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This article has an erratum: [https://doi.org/10.1051/0004-6361/202142575e]


Issue
A&A
Volume 659, March 2022
Article Number A36
Number of page(s) 26
Section Interstellar and circumstellar matter
DOI https://doi.org/10.1051/0004-6361/202142575
Published online 02 March 2022

© ESO 2022

1 Introduction

H II regions are created by the ionizing radiation of massive stars. Extreme ultra-violet (EUV) photons with energies >13.6 eV photoionize hydrogen in the surrounding medium, and a “bubble” of hot ionized gas (T >8000 K) expands around the star (Strömgren 1939), at a supersonic sound speed, into the cool (T ~10–20 K) molecular cloud. During this expansion, a layer of dust and gas is formed between the ionization front and the preceding shock. Though the propagation of the expanding H II region is initially spherical and many H II regions indeed look circular or bipolar (Churchwell et al. 2006; Deharveng et al. 2010; Anderson et al. 2014), suggesting a 3D bubble structure, more evolved H II regions can have more irregular shapes. This depends on the distribution of the ionizing sources, the initial structures in the embedding gas, and the evolutionary state. Similarly, the structure of the parental molecular cloud can also be nonuniform. Beaumont & Williams (2010) found, based on 12CO (3 →2) maps, that the molecular gas distribution of many H II regions with a circular shape forms ring-like structures around H II region bubbles with a deficit of CO emission along the line-of-sight (LOS) toward the bubble center. This suggests that the clouds are “flat”, that is sheet-like, with one dimension thinner than the other two. Anderson et al. (2010) and Kirsanova et al. (2019) support this scenario for the prototypical H II region bubble RCW 120, based on dust continuum and CO line observations. However, special attention has to be given to self-absorption effects in optically thick low- to mid-J CO lines because concentrations of cold dense material in front of a warm emitting cloud can mimic a CO deficit.

It has been discovered recently that many circular H II regions are associated with expanding shells seen in ionized carbon (Pabst et al. 2019, 2020; Tiwari et al. 2021; Luisi et al. 2021), based on [C II] 158 μm fine-structure line observations with the Stratospheric Observatory for Infrared Astronomy (SOFIA). This important cooling line arises mostly in the atomic-to-molecular transition layer between the H II region and the dense molecular cloud, where a warm (T ≳90 K) photodissociation region (PDR, Hollenbach & Tielens 1999) is formed. For RCW 120, it was shown that the 3D C+ bubble is driven by the stellar wind of the central star and has a significant impact on the star-formation efficiency in the embedding cloud (Luisi et al. 2021). A spherical distribution of warm dust inside the H II region, but a more clumpy structure in the associated molecular cloud, was reported by Marsh & Whitworth (2019) based on Herschel data.

We here present a study of [C II], CO, and H I line emission in the RCW 120 region, complementary to the study presented in Luisi et al. (2021). The [C II] 158 μm line was observed in the context of the SOFIA Legacy Program FEEDBACK1 (Schneider et al. 2020). Maps of 12CO and 13CO (3 →2) emission were obtained with the Atacama Pathfinder Experiment (APEX) telescope. In addition, there is a wealth of archival data on this source at various wavelengths we employ to support the interpretation of our data. Particularly important are high angular resolution (~2′) H I 21 cm line emission data from the Southern Galactic Plane Survey (SGPS, McClure-Griffiths et al. 2005).

The objectives of this paper are to determine the physical properties of the different gas components that are responsible for emission and absorption in the CO, [C II], and H I lines, and to develop a geometrical model for the RCW 120 region. We show that self-absorption features in [C II] and H I are observed at velocities of the bulk emission of the cloud which suggests a physical connection. We argue that the observed large quantities of cold C+ arise from a cool H I halo around the molecular cloud associated with RCW 120. This representation may then serve as a template forexplaining the emission properties in other bubble H II regions.

The H II region RCW 120 has a diameter of 4.5 pc and is excited by a single O6-8V/III star (Martins et al. 2010) at a distance of 1.7 kpc (Kuhn et al. 2019). Figure 1 displays the larger environment of RCW 120 in various tracers (dust, H I, and CO). We observe that there is less atomic and molecular material in the northwestern part of the region and that the H I emission envelops the dense molecular cloud, which is outlined by the dust column density contours. The lower panels of Fig. 1 show the molecular cloud velocity components that are associated with RCW 120, a blue-shifted velocity cloud (v = −37 to − 20 km s-1) and a red-shifted one (v = −20 to 10 km s-1) that are proposed to be in collision (Torii et al. 2015). The most prominent feature in RCW 120 is a ring of dense dust and molecular gas from the red-shifted velocity cloud. Many massive condensations along the ring structure were identified in (sub)-millimeter continuum emission by Zavagno et al. (2007); Deharveng et al. (2009); Anderson et al. (2012). Notable is “condensation 1” (Zavagno et al. 2010) in the southern arc of CO emission, that hosts a Class 0 young stellar object (YSO), driving a CO outflow (Figueira et al. 2020).

The paper is organized as follows. Section 2 gives an overview of the observational data we make use of. Section 3 briefly discusses the [C II], CO, and H I emission distributions and Sect. 4 presents an analysis of the self-absorption effects in [C II], CO (3 →2) and H I. This analysis uses the two-layer multicomponent model for [C II] and CO, first introduced by Guevara et al. (2020) and applied in Bonne et al. (2020). To run the model for an entire spectral cube in CO, we employ a Gaussian Mixture Model, which is an unsupervised machine learning approach to cluster spectra along common properties (Brunton & Kutz 2019). We then constrain the geometry of RCW 120 using SimLine (Ossenkopf et al. 2001) on the CO and [C II] data. H I self-absorption (HISA) is quantified with improved methods for HISA studies. In Sect. 5, we discuss our results and draw a general picture for the possible formation and evolution of H II regions associated with flat molecular clouds. Section 6 summarizes our findings.

2 Observations

2.1 SOFIA

The [C II] line at 1.9 THz was observed during one flight from Christchurch, New Zealand, on 10 June 2019, and during one flight from Tahiti, French Polynesia, on 12 August 2021. The map from the 2019 run covers 75% of the total planned area and is presented in Luisi et al. (2021), the missing part was obtained in the 2021 southern deployment in Tahiti, though with slightly less integration time (see below). For both runs, the heterodyne receiver upGREAT2 onboard SOFIA was used. The target area was split into four squared “tiles” in which each tile has a length of 435.6″ = 7.26′ and is covered four times, two times in RA-direction and two times in Dec-direction. The first two coverages are performed with the array rotated 19° on the sky. The second two coverages are then shifted by 36″ to fill up the gaps of the [OI] map, which was observed in parallel but will not be discussed here. All tiles were covered in the array-on-the-fly mapping mode. During the Tahiti campaign, the last missing northwestern tile was covered two times in RA-direction but only one time in Dec-direction. This results in a slightly lower signal-to-noise ratio.

The half-power beam width at 1.9 THz is 14.1″. As backend, a Fast Fourier Transform Spectrometer (FFTS) with 4 GHz instantaneous bandwidth was employed (Klein et al. 2012). The velocity resolved spectra are resampled to a velocity resolution of 0.2 km s-1. We convolved the [C II] spectra with a Gaussian function to 20″ resolution to increase the S/N and to better compare to the APEX CO (3 →2) data at an original resolution of18″ (and convolved to 20″). The [C II] spectra are presented on a main beam brightness temperature scale Tmb, using an average main beam efficiency of ηmb = 0.65. The forward efficiency is ηf = 0.97. From the spectra, a first order baseline and a set of principle components were removed that were determined from a Principal Component Analysis (PCA) of the spectra from the OFF-position measurements (emission free background). The components originate from the instrument and/or atmosphere (Buchbender et al., in prep.). Systematic variations in the spectra, originating from these instrumental effects, are subtracted in this way from the ON-position spectra (see Tiwari et al. 2021 for more information). The central position of the final map is located at RA(2000) = 17h 12m03.65s and Dec(2000) = −38°30′28.43″. As emission-free reference position, we used RA(2000) = 17h10m41s, Dec(2000) = −37°44′04″.

thumbnail Fig. 1

An overview of RCW 120. Top left: false color image of RCW 120 in Herschel fluxes at 70 μm (blue), 160 μm (green), and 250 μm (red). The H II bubble of RCW 120 stands out prominently. Top right: H I line integrated (v = −20 to 10 km s−1) emission from the SGPS survey (McClure-Griffiths et al. 2005) with contours of Herschel dust column density overlaid (levels Av = 15 to 50 in increments of five). The Herschel data were observed within the HiGAL program (Molinari et al. 2010) and the column density map was produced using the PPMAP method (Marsh et al. 2017). The position where we show an individual spectrum (Fig. 6) is indicated by a blue triangle and the off-position we used for the HISA analysis is marked with a gray triangle. The white and gray squares outline the spectra map displayed in Fig. D.1 and the star symbol indicates the exciting star of RCW 120. Bottom left and right: line integrated 12CO (1 →0) intensity maps of RCW 120 between − 37 to − 20 km s−1 and − 20 to 10 km s−1, respectively. The CO data were taken with the MOPRA telescope and have a resolution of 30″ (Torii et al. 2015).

thumbnail Fig. 2

Velocity integrated maps of [C II] and CO (3 →2) emission in RCW 120 between − 20 and 10 km s-1. Left panel: line integrated [C II] intensity map. The contours outline the regions extracted with a dendrogram based approach (Rosolowsky et al. 2008; Robitaille et al. 2019), explained in Sect. 4.1. Middle and right panel: line integrated 12CO (3 →2) and 13CO (3 →2) intensity maps, respectively. The contours give the line integrated [C II] intensity levels 60, 100, 140, 180, 220 K km s-1, ranging from black to light gray. The two gray lines indicate cuts displaying the line intensities in Fig. 3. The diagonal line has an angle of 25° with respectto the horizontal line. The exciting O6-8V/III type star CD-38 11636 is marked with a star symbol.

2.2 APEX

RCW 120 was mapped on September 21, 2019 in good weather conditions (precipitable water vapor, pwv = 0.5–0.7 mm). The lines observed were 12CO (3 →2) at 345.796 GHz and 13CO (3 →2) at 330.588 GHz, using the LAsMA array on the APEX3 telescope (Güsten et al. 2006). LAsMA is a 7-pixel single polarization heterodyne array receiver that allows simultaneous observations of the two isotopomers in the upper (12CO) and lower (13CO) side-band of the receiver, respectively. The array is arranged in a hexagonal configuration around a central pixel with a spacing of about two beam widths (θmb = 18.2″ at 345.8 GHz) between the pixels. It uses a K mirror as de-rotator. The backends are advanced Fast Fourier Transform Spectrometers (Klein et al. 2012) with a bandwidth of 2 ×4 GHz and a native spectral resolution of 61 kHz. The mapping was done in total power on-the-fly mode using a clean reference position at RA(2000) = 17h10m41s, Dec(2000) = −37°44′04″ (same as for [C II]). The mapped region of 15′ × 15′ was split into 2 × 2 tiles. Each tile was scanned in both RA and Dec with a spacing of 9″ (oversampling to 6″ in scanning direction), resulting in a uniformly sampled map with high fidelity. All spectra are calibrated in main beam brightness temperatures Tmb with a main-beam efficiency ηmb = 0.68 at 345.8 GHz. The observed spectra are convolved with a Gaussian function to 20″ resolution on a grid with a pixel size of 5″. The spectra are resampled to a velocity resolution of 0.2 km s-1.

2.3 H I data

We make use of H I 21 cm hyperfine emission line data and continuum at 1.4 GHz from the Southern Galactic Plane Survey (SGPS), described in detail in McClure-Griffiths et al. (2005). In particular, we use the combined images fromthe Australia Telescope Compact Array and the Parkes Radio Telescope with an angular resolution of ~2′. The spectral cube at an angular resolution of ~150″ was resampled to the same grid as the [C II] and CO (3 →2) data with a pixel size of 5″. The velocity resolution is 0.8 km s−1 and the total velocity range covered is −200 to 150 km s−1.

thumbnail Fig. 3

Position-intensity diagram along two cuts. The positions of both cuts are indicated by the gray lines crossing the ionizing star (central position) in Fig. 2, negative distances are to the east and northeast. The upper panel shows the intensity along the horizontal line and the lower one the intensity along the diagonal cut (25°). The [C II] and 12CO and 13CO (3 →2) intensities are indicated by a blue, orange, and green curve, respectively.

3 Results

3.1 [C II] and CO emission distributions

Maps of line integrated emission of [C II], 12CO and 13CO (3 →2) over a velocity range of − 20 to 10 km s−1 are displayed in Fig. 2. This is the velocity range of the red-shifted cloud that is clearly associated with the RCW 120 H II region (Fig. 1). Comparing the spatial distribution of [C II] and CO, we find that the molecular ring, traced by CO, is somewhat larger and envelopes the [C II] structure. This is demonstrated in Fig. 3, which shows the integrated intensity (between − 20 to 10 km s−1) of [C II] and CO along a horizontal and a diagonal cut through the star (indicated by the two gray lines in Fig. 2). There is a strong drop in emission towards the center of H II region compared to the ring. In 12CO the intensity ratio is ~5–10, in 13CO ≳ 10 and in [C II] ~3–5. In addition, the [C II] emission peaks at slightly smaller radii than CO. This indicates a typical PDR layer structure with the [C II] emitting layer closer to the exciting source than the molecular gas.

Figure 4 shows channel maps of [C II] and CO emission between − 12 and − 2 km s−1. We intentionally leave out the higher-velocity ranges (− 30 to − 12 km s−1 and − 2 to 6 km s−1, respectively)that reveal an expanding bubble in C+ (but not in CO), since this feature is discussed in Luisi et al. (2021). We here focus on the bulk emission of the cloud. All tracers show a ring-like structure around the central H II region in all channels between −12 and −2 km s−1. The ring stands out particularly at the systemic velocity of RCW 120 at −7.5 km s−1. However, there are subtle differences between the CO and [C II] emission distributions. The [C II] ring is rather smooth, with a narrow opening to the east and a larger one to the northwest, but the emission drops sharply going outwards. The CO emission is more fragmented, clearly visible in the middle panel of Fig. 4, and no coherent ring-like structure is visible, but rather a succession of dense clumps along the ring. Similar to the [C II] emitting gas, characterizing mainly the PDR, we also find the same opening to the northwest, but it extends further out than observed in the [C II] line. Close to the systemic velocity of the cloud around − 7.5 km s-1 we observe a lack of CO emission following a tube-like structure extending diagonally from the southwest to the northeast. As we show in Sect. 4.4, this feature is due to self-absorption and indicates that a substantial fraction of emission is absorbed by cold foreground material. The 13CO (3 →2) emission mostly reflects the ring structure and is tracing the dense clumps discovered in dust continuum (Zavagno et al. 2007; Deharveng et al. 2009; Figueira et al. 2017). In addition, in the 13CO channel maps (Fig. 4, bottom panel) we detect two lanes of emission at velocity ~ −7.5 km s−1 across the H II region. These lanes are clearly in the foreground because they are visible in Hα emission as dark features in front of RCW 120 (Figueira et al. 2017; Luisi et al. 2021) and they are also present in 12CO where they are optically thick and extend beyond the southwestern rim of RCW 120. All CO (3 →2) emission features are similar to the ones seen in lower-J CO lines, reported in Anderson et al. (2015) and Kirsanova et al. (2019).

We note that the ionizing star CD − 38°11636 is shifted ~ 110″ southward with respect to the geometrical center of RCW 120. As discussed in Luisi et al. (2021), the stellar wind of the star drives a fast (~15 km s−1) expanding bubble in [C II]. Luisi et al. (2021) report that there is no sign of this expanding shell in the CO (3 →2) data. Likewise, this expansion is also not present in CO (1 →0) and (2 →1) observations(Anderson et al. 2015; Kirsanova et al. 2019).

thumbnail Fig. 4

Channel maps of [C II], 12CO (3 →2) and 13CO (3 →2) emission between −12 and −2 km s−1 integrated insteps of 1 km s−1. Top panel: [C II] line emission. Middle panel: 12CO (3 →2) line emission. Bottom panel: 13CO (3 →2) line emission.

thumbnail Fig. 5

The three top panels show the line integrated 12CO, 13CO (3 →2) and [C II] emission (from left to right, v = −20 to 10 km s−1). The black square in each panel indicates the area where spectra of these lines are shown in the box below. 12CO and 13CO are indicated in black and blue, respectively, the [C II] spectra in red. We note that there is no scaling for any of the lines. The x- and y-axis for the spectra are shown in the top right panel. The spatial offsets are given in arcmin in all panels, the (0,0) position refers to RA(2000) = 17h12m03.65s, DEC(2000) = −38°30′28.4″ (see upper panels). All spectra were smoothed to an angular resolution of 30″ and are displayed in a grid of 30″. This cutout includes the clump with condensation 1 (Zavagno et al. 2007), indicated by a dashed circle, with its prominent outflow source at offsets ~1.5′,−1′.

3.2 [C II], CO, and H I spectra

3.2.1 [C II] and CO spectra

Figure 5 shows as an example CO and [C II] spectra from the area around condensation 1, the brightest emission region in RCW 120 in these tracers. The most prominent feature in the [C II] spectra (red in Fig. 5) is the very extended, high-velocity blue wing in the northwestern area of the box (RA-offset 2′ to 3′, Dec-offsets 0 to −2′) which is missing in 12CO (black spectra). This is the signature of the expanding [C II] shell discussed in Luisi et al. (2021). On the other hand, high-velocity red- and blue-shifted 12CO emission is found at spectra around 1.5′,−1.5′, the peak position of 12CO emission in condensation 1. This is a protostellar CO outflow, recently reported in Figueira et al. (2020). The 12CO spectra show a deep dip in the line shape over several velocity channels around −8 km s−1 where 13CO (blue spectra) has its peak emission. This is the classical picture of an optically thick 12CO line that is self-absorbed. The [C II] line is less affected by optical depth effects in this area of RCW 120, but shows clear self-absorption features, mostly in the form of “flat-top” spectra, i.e. broad absorption over several velocity channels (~ −7 km s−1 to −9 km s−1) at many positions in- and outside of the ring. The complicated line shapes in CO and [C II] indicate a complex spatial structure of the emitting gas components with cooler material in front of the bulk emission of the cloud along the LOS.

3.2.2 [C II] and H I spectra

The phase transition from warm neutral gas to cold neutral and finally molecular gas creates typical correlations between 12CO emission and H I self-absorption (Wang et al. 2020). Figure 6 displays an overlay of [C II], 13CO (3 →2) and H I emission at a representative position, where a prominent dip in emission in the H I line is visible over a large velocity range of −6 to −11 km s−1, centering at the bulk emission of the cloud at ~ −7.5 km s−1. The bulk emission is well-traced by the optically thin 13CO (3 →2) line that has a Gaussian shape. In contrast, the [C II] line is not Gaussian but also shows self-absorption in the form of a “flat-top” spectrum in the same velocity range as the H I self-absorption. We note that the [C II] and 13CO spectra for this plot are on a resolution of 30″ while the resolution of the H I line is ~2′. In Appendix D, we display overlays of [C II] and H I spectra both at ~2′ resolution in order to demonstrate that the H I broad self-absorption around −7.5 km s−1 persist across the whole area observed in [C II] and that there is little variation in the line profile. In the next section, we perform a quantitative analysis of the line emission in order to assess the amount of self-absorption in [C II], CO, and H I.

thumbnail Fig. 6

Overlay between [C II] (red), H I (black), and 13CO (3 →2) (blue) spectra at position (0,2′), indicated in Fig. 1. The H I data have an angular resolution of ~2′, the other spectra have a resolution of 30″. This position is a typical example of the line shapes in RCW 120; larger spectral line maps are given in Figs. 5 and D.1.

4 Analysis

In the following, we start with a determination of the optical depths of the 12CO and [C II] lines along the PDR ring of emission in RCW 120 (Sect. 4.1). We then apply (Sect. 4.2) a two-layer multicomponent model (Guevara et al. 2020) and present the results for the [C II] emission. To solve the radiative transfer equation for the CO data, we need to find a set of initial conditions that satisfies each spectrum of the spectral cube. This is done by clustering the spectral cube via a Gaussian Mixture Model (Sect. 4.3), which allows us to focus on groups of spectra (i.e., clusters) and initializes the radiative transfer equation with fewer, but physically consistent, initial conditions. In Sect. 4.4, we show and discuss the resulting CO synthetic background emission and foreground absorption maps. Next, in Sect. 4.5, we perform SimLine simulations in order to test if RCW 120 is embedded in a spherical molecular cloud. In Sect. 4.6, we present a study of H I self-absorption.

4.1 [C II] and CO optical depth from a one-layer model

The velocity resolved optical depth of 12CO or [12C II] can be determined from the isotopic 12C/13C-brightness temperature ratio with T mb , 12 C (v) T mb , 13 C (v) = 1 e τ(v) τ(v) α, \begin{equation*}\frac{T_{\mathrm{mb, ^{12}C}}(v)}{T_{\mathrm{mb, ^{13}C}}(v)}= \frac{1-\textrm{e}^{-\tau(v)}}{\tau(v)} \alpha,\end{equation*}(1)

assuming that the 13C-isotopologue is optically thin. Here, v is the respective velocity (or channel) and α = 59 ± 10 the local 12C/13C abundance ratio in RCW 120, which is derived from a linear fit, α =6.21(±1.00) ⋅ dGC + 18.71(±7.37), over the carbon isotopic rate of multiple sources in the Galactic plane as a function of distance dGC (in kpc) to the Galactic center (Milam et al. 2005). We assume the same abundance value for ionized and molecular carbon and identical excitation temperatures for all isotopologues (since they have the same collision partners) in the single-layer model.

The large abundance of CO in interstellar molecular clouds results in large optical depths of the main isotope, and in contrast to the less abundant [13C II] hyper-fine emission, the 13CO isotope can also be affected by optical depth effects. In this case, the determined optical depth values from the comparison of both isotopes must be interpreted as a lower limit.

While the [12C II] line is bright in PDR regions such as the one in RCW 120, the [13C II] line is typically faint and requires deep integration at single points (Guevara et al. 2020) or averaging over larger areas. In addition, the [13C II] transition splits into three hyperfine components, with a relative strength of s2→1 = 0.625, s1→0 = 0.25 and s1→1 = 0.125. The three satellites are velocity shifted by Δv2→1 = 11.2 km s-1, Δv1→0 = −65.2 km s-1 and Δv1→1 = 63.2 km s-1 with respect to the [C II] fine structure line (Ossenkopf et al. 2013; Guevara et al. 2020). The strongest hyper-fine structure line lies closest to the main line and is therefore often affected by the wing emission of the [12C II] line. In such a case it is required to fit the red-shifted wing and the satellite simultaneously by a Gaussian profile in order to disentangle the wing component of the [C II] emission from the isotope. Here, we use the conservative assumption that the total intensity in the superposition of both transition lines is dominated by the wing of the main isotope, not the [13C II] line. In this way, we may rather underestimate the [13C II] intensity and thus the optical depth, also providing a lower limit.

The weak intensity and splitting of the [13C II] hyper-fine transition into three lines result in a small signal-to-noise ratio in each pixel and thus do not allow one to spatially resolve the isotope emission. Thus, we average emission over arcmin2 large regions with a dendogram based approach (Rosolowsky et al. 2008; Robitaille et al. 2019). Dendrograms allow for a hierarchical structure analysis of spectral data cubes and thus provide a quantitative way to determine the most prominent extended structures in RCW 120 and local bright structure within those. The determined areas are indicated by contours in the [C II] map (left panel) in Fig. 2. The black contour outlines the entire PDR and bulk of the [C II] emission from RCW 120. The blue, green and red contours split the emission into the three brightest regions: the southwestern PDR with condensation 1, that includes a protostellar outflow, the southeastern PDR with condensation 2 (Zavagno et al. 2007), and the northeastern PDR, respectively. The corresponding averaged spectra of [12C II] and [13C II] and 12CO and 13CO (3 →2) emission originating from these regions are shown in Fig. 7 (left and right, respectively). The dark colored spectra represent the main 12C line and the light colors show the 13C isotope emission. The [13C II] line is averaged over all three hyper-fine transitions (weighted by the relative strength of each satellite) and multiplied by the local carbon abundance ratio of 59. The CO averaged spectra are shown on the original intensity scale without multiplying by the abundance ratio. The velocity dependent optical depth is indicated by the black data points with error bars, which are determined by Δτ=| τ 2 (1+τ) e τ 1 | \sqrt{\frac{ α 2 T_{\mathrm{^13C}}^2σ^2_{\mathrm{^12C}}+ α 2 T_{\mathrm{^12C}}^2σ^2_{\mathrm{^13C}}+Δ α 2 T_{\mathrm{^13C}}^2T_{\mathrm{^12C}}^2  }{ α 4 T_{\mathrm{^13C}}^4}}, \begin{equation*}\Delta \tau = \left| \frac{\tau^2}{(1+\tau)\textrm{e}^{-\tau}-1} \right| \sqrt{\frac{\alpha^2 T_{\mathrm{^{13}C}}^2 \sigma^2_{\mathrm{^{12}C}} + \alpha^2T_{\mathrm{^{12}C}}^2 \sigma^2_{\mathrm{^{13}C}} + \Delta\alpha^2 T_{\mathrm{^{13}C}}^2 T_{\mathrm{^{12}C}}^2}{\alpha^4 T_{\mathrm{^{13}C}}^4}},\end{equation*}(2)

with σ the root mean square (rms) of the brightness temperature of each respective isotope (see Appendix B for the derivation of this equation).

All [C II] spectra show a double peak structure followed by a blue-shifted tail but the scaled up [13C II] line overshoots the [C II] emission and peaks where we observe the dip in the [C II] spectrum, indicating strong self-absorption. We emphasize that the velocity range of the overshoot is not restricted to the bulk emission of the cloud at − 7.5 km s−1 but covers the whole velocity range between ~−10 to −6 km s−1. The optical depth effects in [C II] thus cover a broad distribution in velocity, resulting in “flat-top” spectra and a pronounced dip at − 7.5 km s−1. Both features are also well visible in the individual spectra (Sect. 3.2). The velocity resolved optical depth is above unity for all spectra and peaks at the [C II] absorption dip. The averaged optical depth varies along the ring between τ[C II] ~ 3–4.

It is known that the rotational transitions of 12CO often suffer from self-absorption effects, due to the high abundance of the 12CO molecule (Castets et al. 1990). The absorption effects in RCW 120 are strong enough to be clearly visible in the channel maps around the systemic velocity of the molecular cloud − 7.5 km s-1, see Fig. 4. We observe that most of the emission originating from the southwestern PDR is absorbed. This leads to a visual impression of missing emission along a lane extending diagonally from the inner ring towards the southwestern ring. To determine the strength of the self-absorption we compare the 12CO with the less abundant 13CO line, assuming all emission comes from a single layer.

Similar to the [C II] line, the 12CO (3 →2) line also shows in Fig. 7 a double peak structure for all average spectra with a blue- and red-shifted tail. The most prominent red-shifted emission is found for the southwestern PDR region, most likely due to the internal outflow source. A comparison to the 13CO (3 →2) line clearly reveals that the apparent double peak structure is due to optical depth effects, since the isotope shows a single peak at the location of the emission dip. However, the line-dip is somewhat blue-shifted with respect to the 13CO (3 →2) peak. This is especially visible in the southwestern PDR. A possible explanation is that the observed blue shift of the optical depth maximum with respect to the peak emission is caused by a momentum transfer of the expanding [C II] bubble into the surrounding molecular cloud. The mechanical impact of the expanding bubble could lead to an accumulation of blue-shifted material along the line of sight and thus a higher optical depths for some velocity channels. We note that the 12CO optical depth is overall very high, up to a few 10s at the bulk emission velocity, but this is a consequence of the assumption of the single layer model. These unrealistically high values show that it is required to use a two-layer model where different excitation temperatures are considered. Only with this approach, presented in the next section, it is possible to model self-absorption effects, suchas dips, due to a colder foreground material, which is intrinsically not possible with a single-layer model.

thumbnail Fig. 7

Averaged spectra of the structures along the ring of RCW 120, sorted by the regions indicated in Fig. 2 (ring, southwestern PDR, southeastern PDR and northeastern PDR). Left panels: averaged [12C II] and scaled up [13C II] emission by the local abundance 12C/13C-ratio of 59. Right panels: averaged 12CO and 13CO (3 →2) emission. The black data points with error bars indicate the velocity resolved optical depth.

4.2 Two-layer multicomponent model

4.2.1 An introduction to the model

In the following, we use a generalized version of the model introduced by Guevara et al. (2020) which solves the radiative transfer equation for two gas layers with multiple velocity components that is also adequate for optically thick lines. By assuming a background (bg) layer with a higher excitation temperature than the foreground (fg), T ex, i bg > T ex, i fg $T_{\mathrm{ex},i_{\mathrm{bg}}} > T_{\mathrm{ex},i_{\mathrm{fg}}}$, the background is responsible for the bulk emission of the cloud, while the foreground layer, providing mainly absorption, is located in front of the bulk emission. The observed brightness temperature then calculates as T mb (v)= [ J ν ( T ex,bg )( 1 e i bg τ i bg (v) ) ] e i fg τ i fg (v) + J ν ( T ex,fg )( 1 e i fg τ i fg (v) ), \begin{equation*}\begin{split}T_{\mathrm{mb}}(v) = & \left[\mathcal{J}_{\nu}(T_{\mathrm{ex},\mathrm{bg}}) \, \left(1-\textrm{e}^{-\sum_{i_{\mathrm{bg}}}\tau_{i_{\mathrm{bg}}}(v)}\right) \right] \textrm{e}^{-\sum_{i_{\mathrm{fg}}} \tau_{i_{\mathrm{fg}}}(v)} \\& + \mathcal{J}_{\nu}(T_{\mathrm{ex},\mathrm{fg}}) \, \left(1-\textrm{e}^{-\sum_{i_{\mathrm{fg}}}\tau_{i_{\mathrm{fg}}}(v)}\right), \\\end{split} \end{equation*}(3)

with the sum over ibg,fg components located either in the background or foreground, respectively. The foreground components can be associated with the emitting cloud but they also can be unrelated foreground material. Associated foreground is naturally formed through a decreasing temperature gradient along the line of sight when a background PDR layer around an H II region is connected with a foreground molecular cloud. Because the absorption dip of the more abundant 12C isotope is always close to the systemic velocity of RCW 120, see Fig. 7, we can safely assume that the origin of the cold absorbing components is not an unrelated cloud along the line of sight. In addition, the geometry of RCW 120 with a hot, central H II region, followed by a warm PDR layer and then a cool molecular cloud already suggests a gas temperature gradient. In the following we refer to the absorption by the foreground components as self-absorption. We perform the model fit on both isotopic lines simultaneously, thus the combined line shape is given by: Φ i (v)= ϕ i (v)+ FF s FF ϕ i (vΔ v FF ), \begin{equation*}\Phi_i(v) = \phi_i(v) + \sum_{\mathrm{F\to F\prime}}s_{\mathrm{F\to F\prime}}\phi_i(v-\Delta v_{\mathrm{F\to F\prime}}),\end{equation*}(4)

where Δ v FF $\Delta v_{\mathrm{F\to F\prime}}$ is the line velocity offset from the main isotope and s FF $s_{\mathrm{F\to F\prime}}$ the relative intensity of each line (1 for 13CO and see above for [13C II]). The line profile of each component ϕi(v) is a normalized Gaussian profile: ϕ i (v)= 2 ln2 w i π e 4ln2  ( v v 0,i w i ) 2 , \begin{equation*}\phi_i(v)=\frac{2\sqrt{\ln 2}}{w_i\sqrt{\pi}}\textrm{e}^{-4\ln 2~\left(\frac{v-v_{0,i}}{w_i}\right)^2},\end{equation*}(5)

with v0,i being the central (LSR) velocity and wi the line’s width (FWHM) of the component i. The factor 4ln2 stems from the usage of the FWHM wi instead of the standard deviation σi. The equivalent brightness temperature of a black body emission at a temperature Tex is J ν ( T ex,i )= T 0 e T 0 / T ex,i 1 , \begin{equation*}\mathcal{J}_{\nu}(T_{\mathrm{ex},i}) = \frac{T_0}{e^{T_0/T_{\mathrm{ex},i}}-1},\end{equation*}(6)

with the equivalent temperature of the transition T0 = kB and ν the transition frequency. Each component of the model is characterized by four quantities: excitation temperature, optical depth, position (LSR velocity), and width (FWHM). The position of the component in velocity space and line width are confined by the observed line. The excitation temperature and optical depth are not independent from each other. The excitation temperature can only be read from the line intensity in case of high optical depths. We therefore first constrain a suitable excitation temperature from the observed data, which then leaves only the optical depth as a free parameter.

Assuming that the warm background is partly shining through the cold layer lying in front of it, we can determine the background excitation temperature around the emission peak main beam temperature Tp,mb by: T ex = T 0 ln ( T 0 T p,mb ( 1 e τ p )+1 ) 1 , \begin{equation*}T_{\mathrm{ex}} = T_0\ln\left(\frac{T_0}{T_{\mathrm{p,mb}}}\left(1-\textrm{e}^{-\tau_{\mathrm{p}}}\right)+1\right)^{-1},\end{equation*}(7)

using the optical depth τp determined through Eq. (1).

4.2.2 Two-layer fit of the [C II] ring

We can determine the [C II] optical depth for each component of the emitting background as a function of the excitation temperature Tex and column density N[C II] (Guevara et al. 2020) τ [C\scriptsizeII],i (v)= Φ i (v) g u g l c 3 8π ν 3 A ul N [C\scriptsizeII],i 1 e T 0 T ex,i 1+ g u g l e T 0 T ex,i , \begin{equation*}\tau_{\mathrm{[C{\scriptsize\,II}]}, i}(v)=\Phi_i(v)\frac{g_u}{g_l}\frac{c^3}{8\pi \nu^3}A_{ul} N_{[\mathrm{C{\scriptsize\,II}}], i}\frac{1-\textrm{e}^{-\frac{T_0}{T_{\mathrm{ex},i}}}}{1+\frac{g_u}{g_l}\textrm{e}^{-\frac{T_0}{T_{\mathrm{ex},i}}}},\end{equation*}(8)

with ν = 1900.5369 GHz the rest frequency of the [C II] fine structure line, Aul = 2.3 × 10−6 s-1 the Einstein coefficient for spontaneous emission (Wiese & Fuhr 2007), T0 = kB = 91.25 K the equivalent temperature of the upper level, and the statistical weights of the [C II] transition energy levels gu = 4 and gl = 2. The maximum excitation temperature along the ring in RCW 120, i.e., the background layer, is determined with Eq. (7) to be Tex = 50–70 K.

For the foreground layer, we constrain the lower and upper limits of the excitation temperature of [C II]. The lower limit is derived from the [C II] energy balance. We consider here the case without excess radiative heating, this means the energy input for the ionized carbon gas is provided only by the standard interstellar radiation field and cosmic ray (CR) ionization. In a diffuse optically thin gas the [C II] line emissivity can be computed by (Ossenkopf et al. 2013): nnn\beginaligned ϵ dv &= h A ul c 3 8π k B ν 3 × N [C\scriptsizeII] × g u e T 0 T ex g l + g u e T 0 T ex nnn&=2.3× 10 28 J sr × N [C\scriptsizeII] ×E( T ex ),\endaligned \begin{equation*}\begin{aligned}\int \epsilon\,\mathrm{d}v &= \frac{hA_{ul}c^3}{8\pi k_{\mathrm{B}} \nu^3}\times N_{\mathrm{[C{\scriptsize\,II}]}} \times \frac{g_u\textrm{e}^{\frac{-T_0}{T_{\mathrm{ex}}}}}{g_l+g_u\textrm{e}^{\frac{-T_0}{T_{\mathrm{ex}}}}}\\&= 2.3\times10^{-28} \frac{\mathrm{J}}{\mathrm{sr}} \times N_{\mathrm{[C{\scriptsize\,II}]}} \times E({T_{\mathrm{ex}}}),\end{aligned}\end{equation*}(9)

where we abbreviate the excitation-temperature dependent ratio as E(Tex) and ϵ is the heating efficiency. The total [C II] cooling is Λ [C\scriptsizeII] = 4π ϵ dvdΩ=2.9× 10 27 W× N [C\scriptsizeII] ×E( T ex ) \begin{equation*}\Lambda_{\mathrm{[C{\scriptsize\,II}]}} = \int_{4\pi}\int \epsilon\,\mathrm{d}v\,\mathrm{d}\Omega = 2.9\times10^{-27}\,\mathrm{W}\times N_{\mathrm{[C{\scriptsize\,II}]}} \times E({T_{\mathrm{ex}}})\end{equation*}(10)

and the heating of the cold diffuse cloud is given by the ambient UV field and the CR ionization. The energy density ϱUV for an uv field4 of χ =1 is 6.8 × 10−21 J cm-3. It is absorbed mainly by interstellar dust providing an UV optical depth of τUV ~ 3Av∕1.08. In a column with Av = 1 the energy heating of dust and gas is thus: F UV =( 1 e τ UV( A v =1) ) ϱ UV,χ=1 c=1.9× 10 6 W m 2 . \begin{equation*}F_{\mathrm{UV}} =\left(1-\textrm{e}^{-\tau_{\mathrm{UV}(A_{\textrm{v}} = 1)}}\right)\varrho_{\mathrm{UV, \chi=1}} c = 1.9\times10^{-6}\mathrm{\frac{W}{m^2}}.\end{equation*}(11)

With a typical gas heating efficiency ε = 0.01 (Okada et al. 2013), and the gas column density of N H, A v =1 =1.9× 10 21 cm -2 $N_{\mathrm{H}, A_{\textrm{v}} = 1}=1.9\times10^{21}\,\mathrm{cm^{-2}}$ for an Av = 1 we can translate this into a heating rate per hydrogen; and with the carbon to hydrogen ratio C∕H = 1.6 × 10−4 (Sofia et al. 2004) we obtain a [C II] heating rate of: Γ UV =ε F UV N H, A v =1 ×C/H × N [C\scriptsizeII] =6.3× 10 30 W× N [C\scriptsizeII] . \begin{equation*}\Gamma_{\mathrm{UV}} = \varepsilon \frac{F_{\mathrm{UV}}}{N_{\mathrm{H}, A_{\textrm{v}} = 1} \times \mathrm{C/H}} \times N_{\mathrm{[C{\scriptsize\,II}]}} = 6.3\times10^{-30}\,\mathrm{W} \times N_{\mathrm{[C{\scriptsize\,II}]}}.\end{equation*}(12)

The CR heating rate is given by the CR heating per ionization Q ~ 10 eV (Glassgold et al. 2012) and the CR ionization rate ηH ≈ 2 × 10−16 s-1 (Indriolo et al. 2015). Dividing by the C/H-ratio gives the CR [C II] heating rate: Γ CR = Q× η H C/H × N [C\scriptsizeII] =2× 10 30 W× N [C\scriptsizeII] , \begin{equation*}\Gamma_{\mathrm{CR}} = \frac{Q \times \eta_{\mathrm{H}}}{\mathrm{C/H}} \times N_{\mathrm{[C{\scriptsize\,II}]}} = 2\times 10^{-30}\,\mathrm{W} \times N_{\mathrm{[C{\scriptsize\,II}]}},\end{equation*}(13)

resulting in a total heating of the diffuse [C II]: Γ [C\scriptsizeII] = Γ UV + Γ CR =8.3× 10 30 W× N [C\scriptsizeII] . \begin{equation*}\Gamma_{\mathrm{[C{\scriptsize\,II}]}} = \Gamma_{\mathrm{UV}} + \Gamma_{\mathrm{CR}} = 8.3 \times 10^{-30}\mathrm{W} \times N_{\mathrm{[C{\scriptsize\,II}]}}.\end{equation*}(14)

Energy balance between [C II] cooling (Eq. (10)) and [C II] heating (Eq. (14)) then provides the limit for the [C II]excitation temperature in case of low radiation fields: nnn\beginalignedE( T ex )=0.003= g u e T 0 T ex g l + g u e T 0 T ex \\ T ex = T 0 ln( 2 E 2 ) =14K.\endaligned \begin{equation*}\begin{aligned}E({T_{\mathrm{ex}}}) = 0.003 = \frac{g_u\textrm{e}^{\frac{-T_0}{T_{\mathrm{ex}}}}}{g_l+g_u\textrm{e}^{\frac{-T_0}{T_{\mathrm{ex}}}}}\\\Rightarrow T_{\mathrm{ex}} = \frac{T_0}{\ln\left(\frac{2}{E} -2\right)} = 14\,\mathrm{K}.\end{aligned}\end{equation*}(15)

[C II] as the main cooling line in diffuse material cannot get colder. This is the foundation of the phase separation in the neutral interstellar medium as derived already by Field et al. (1969), just with updated numbers. The CR ionization rate from Indriolo et al. (2015) is probably a lower limit; a factor 10 higher rate for example leads to an excitation temperature of 17 K. We thus take for simplicity in the following 15 K as the minimum excitation temperature for our foreground layer.

In order to find an upper limit for the C+ excitation temperature of the foreground layer, we use the information from an independent estimate of the hydrogen column density for the foreground which is given by optical absorption measurements towards the ionized gas bubble of the H II region in Zavagno et al. (2007). They derived a visual extinction of Av ~ 4.36, corresponding to a hydrogen column density of 8.15 × 1021 cm−2 that in turn translates into a C+ column density of 1.3 × 1018 cm−2. From Fig. A.1, we derive then that such a value for the C+ column density is only achieved for a C+ excitation temperature of ~30 K for the foreground. Significantly higher foreground C+ excitation temperatures Tex, [C II] are thus excluded. In the case of emission lines with strong absorption dips, as observed by Guevara et al. (2020) it is possible to derive an upper limit for the excitation temperature from the depth of the absorption dip. Eventually, at temperatures much below the upper level energy of 91.25 K, the derived gas parameters depend only weakly on the exact foreground excitation temperature(Guevara et al. 2020).

The results of the two-layer multicomponent model are displayed in Fig. 8. The red spectra in each subfigure represent the observed averaged [C II] emission in the RCW 120 PDR ring (top left), the northeastern PDR (top right), the southwestern PDR (bottom left), and the southeastern PDR (bottom right), respectively. The green line shows the model fit result, which always provides a very good match to the data, as demonstrated by the fit residuals (gray data points in the left lower panel in each subfigure). The upper right panel of each subfigure shows the background components in dark blue that sum up to the overall synthetic background. The difference in intensity between this synthetic background spectrum and the observed spectrum (in red) shows how much emission is absorbed and thus missing in the integrated intensity map. The absorbing cold foreground components are shown in the right lower panel by the pink curve. It becomes obvious that there is significant absorption, since the synthetic spectra are a factor 2 higher than the observed ones.

Table 1 summarizes the values for [C II] column density N[C II] and hydrogen column density NH = N H\scriptsizeI  +2 N H 2 ${N}_{\textrm{{H{\scriptsize\,I~}}}} + 2 {N}_{\textrm{H}_2}$, mass, and luminosity for the background- and foreground layers. The C+ excitation temperature for the background varies between ~50 and 70 K depending on the region (see Tables in Appendix C.1). For the foreground, we use the lower (15 K) and upper (30 K) limits of the C+ excitation temperature.

From Table 1, it becomes obvious that the background [C II] column density N[C II],bg is typically 3–5 × 1018 cm-2, which corresponds to a hydrogen column density of 2–3 × 1022 cm-2. We anticipate that the C+ emission background emission arises from PDR surfaces of dense, molecular clumps in the UV-illuminated ring of RCW 120 with a total mass of ~2000 M. In this case, H2 molecules are the primary collision partner of C+. We focus here on the emission of the ring but we note that there is little variation in the values for C+ and hydrogen column density for the different regions in RCW 120 (individually listed in the table). In Luisi et al. (2021), we extracted ~100 clumps from the 12CO (3 →2) data and derived typical clump densities of a few 104 cm−3, radii between 0.3 and 1 pc, and a total mass of 2500 M. From the C+ column densities, assuming a density of a few 104 cm−3 (Luisi et al. 2021), we roughly estimate a thickness of the C+ surface layer as a sum over these clumps of ~0.1−0.2 pc. This is consistent with C+ in a thin surface layer around the clumps but potentially several of these clumps along the line of sight in the beam. This calculation, however, ignores beam and volume filling factors, but shows that the PDR surface origin of the C+ emission in the ring is a reasonable approach. It is remarkable that the luminosity in the [C II] line per cloud mass is quite uniform with a typical ratio of L[C II],bgMH,bg ≈ 0.18 LM and a maximum of 0.27 for the SW PDR. This means that in the bright background PDRs we have a typical mass to single-line luminosity conversion factor of 0.2 LM.

The foreground C+ column density N[C II],fg is typically a factor 3 lower, the corresponding hydrogen column densities are of the order of 2–7 × 1021 cm-2 (depending on T[C II],fg = 15 K or 30 K). However, there is significant mass concentrated in this foreground component, summing up to 344 M (or 685 M) in the PDR ring area. The nature of the foreground gas is a priori unknown, but we assume that it constitutes an extended, low-density, cool atomic envelope. To settle this issue, we study the H I emission and absorption properties in Sect. 4.6 and come back to this point in the discussion in Sect. 5.

Table 1

Physical properties of the emitting and absorbing layers along the ring of RCW 120 from [C II] using a foreground excitation temperature of 15 K and 30 K, respectively.

thumbnail Fig. 8

Two-layer multicomponent model results for the four regions extracted with the Dendogram technique. The left top subfigure is a template for all regions: The observed averaged [C II] spectrum is indicated in the left upper panel in red and the green curve on top is the resulting model fit. In the left middle panel, the temperature axis range is smaller so that the weak [13C II] satellitesaround the main isotope line are clearly visible. The left lower panel shows residuals of the fit in gray and the two horizontal orange lines indicate the 3σ level. In theright top panel the red spectrum once more displays the observed [C II] emission and the dark blue lines show the single Gaussian components. The light blue line is the superposition of all synthetic background components. The dashed orange line indicates the velocity resolved optical depth (values on the right axis). The right lower panel shows the pink single foreground Gaussian components and the violet line indicates the superposition of all the synthetic foreground components. The dashed orange line illustrates again the velocity resolved optical depth.

4.3 Clustering of CO spectra

4.3.1 The Gaussian mixture model

In contrast to the [C II] data, the signal-to-noise ratio is sufficiently high in both CO isotopes at most positions of the map to run the two-layer multicomponent model for every spectrum of the entire CO data cube. The model requires an initial guess (number of components, velocity, line width, excitation temperature and optical depth) as an input to converge towards a physically meaningful solution. While the selection of reasonable initial guesses is a simple exercise for a single spectrum, doing so for thousands of spectra requires an unreasonable amount of time. We thus need a different approach here leveraging the fact that the shape of each spectrum in a data cube is not random, but is confined by the local physical conditions. The idea is to apply identical initial guesses for similar spectra. To do so, we first need to group all spectra into clusters in which each cluster represents a typical spectrum assembled by similar spectra. In a second step, the average cluster spectrum is fed into the two-layer multicomponent model and fitted. The values from those fits are then used as initial guesses for all spectra of the corresponding cluster.

We employ a Gaussian Mixture Model (GMM), which groups similar objects by linear combinations of multidimensional Gaussian distributions. This is an unsupervised task and the GMM employed in this study is one of the possible options chosen among many others (Brunton & Kutz 2019). A GMM is a probabilistic approach to clustering and has been proven to be a robust methodology in a variety of real world problems, for example by Jones et al. (2019). Treating each cluster as Gaussians allows for decomposing the whole dataset as a linear combination of Gaussians; it is then a convenient and simple choice which allows for an inexpensive and robust algorithm. Different initialization may result in somewhat different clusters. However, the GMM is only used here as a preprocessing step for the two-layer multicomponent model and we verified that small differences in the identified clusters do not alter our conclusions.

Let S be a set of n spectra. Each spectrum sS is defined as a vector of temperature values depending on the velocity v. Given a number of channels D in velocity space (hereafter feature space) a spectrum s is therefore a D-dimensional point.

A GMM aims at describing the probability distribution of the data set P(s), as a weighted, linear combination of multiple Gaussian distributions N(s $\mathcal{N}(\bm{s}$): P(s)= c ϕ c  N(s; μ c , Σ c ), \begin{equation*}P(\bm{s}) = \sum_{c} \bm{\phi}_{c} ~ \mathcal{N}(\bm{s}; \bm{\mu}_{c}, \Sigma_{c}),\end{equation*}(16)

in which the multidimensional Gaussian distribution is defined as N(s; μ c , Σ c )= exp( 1 2 (s μ c ) T Σ c 1 (s μ c )) (2π) D | Σ c | , \begin{equation*}\mathcal{N}(\bm{s}; \bm{\mu}_{c}, \Sigma_{c}) = \frac{\exp{(-\frac{1}{2}(\bm{s} - \bm{\mu}_{c})^{T}}\Sigma_{c}^{-1}(\bm{s} - \bm{\mu}_{c}))}{\sqrt{(2\pi)^{D} |\Sigma_{c}|}},\end{equation*}(17)

with mean μc, covariance matrix Σc and weight ϕc. The probability of cluster c is P(c) = ϕc and the normalization is given as c ϕ c =1, \begin{equation*}\sum_{c} \bm{\phi}_{c} = 1,\end{equation*}(18)

μc is a D-dimensional vector and Σc is a matrix of size D × D.

The GMM starts with a random guess for the k clusters to discover and it solves an Expectation-Maximization (EM) algorithm (Dempster et al. 1977) to converge to an optimal solution. The EM algorithm iteratively updates the mean μc and covariance matrix Σc of each cluster c in order to maximize the following measure of likelihood: logP(S)= i n log( c k ϕ c  N(s; μ c , Σ c )), \begin{equation*}\log P(\bm{S}) = \sum_{i}^{n} \log (\sum_{c}^{k} \bm{\phi}_{c} ~ \mathcal{N}(\bm{s}; \bm{\mu}_{c}, \Sigma_{c})),\end{equation*}(19)

The EM algorithm always guarantees convergence to a local optimum. While we can simply provide a list of spectra to the GMM algorithm without further doing, we remove the dimensions dominated by noise. A dimension of the feature space is removed when the rms of this dimension is lower than 3 σ cube $3\,\langle\sigma\rangle_{\mathrm{cube}}$, with σ cube $\langle\sigma\rangle_{\mathrm{cube}}$ the average rms of the spectral cube. Furthermore, we scale the intensity of each spectra by T = T mb T mb,min T mb,max T mb,min , \begin{equation*}T\prime = \frac{T_{\mathrm{mb}} - T_{\mathrm{mb, min}}}{T_{\mathrm{mb, max}} - T_{\mathrm{mb, min}}},\end{equation*}(20)

so that the temperature range of every spectra is confined between 0 and 1. This forces the GMM to cluster the spectra based on the line shape regardless of the intensity. The amplitude of each spectrum is proportional to the column density (or optical depth) which has a unique solution for a given excitation temperature. However, the shape of the spectra determines the amount of Gaussian components, which is not found by the model itself but is a model input parameter.

4.3.2 Bayesian information criterion

To select an appropriate number of clusters k we employ the Bayesian information criterion (BIC), a useful statistical test for model selection (Schwarz 1978). Given the total number of spectra n and clusters k, the BIC is defined as: nnn\beginalignedBIC(k) &=N(k)log(n)2L(k);N(k) &=k1+k D+ k D(D1) 2 .\endaligned \begin{equation*}\begin{aligned}\mathrm{BIC}(k) &= N(k) \log(n) - 2\mathcal{L}(k);\\N(k) &= k - 1 + k~D + \frac{k~D(D-1)}{2}.\end{aligned}\end{equation*}(21)

We note that L $\mathcal{L}$ is a measure of likelihood (see Eq. (19)) and D is the dimensionality of the feature space.

Over a range of candidate numbers K = (k1, k2, …), we choose the k = ki which minimizes the BIC. This allows to select the simplest model (i.e., fewest parameter) and avoids model-overfitting. Since the GMM startsin an initial random state, which affects the final outcome to some extend, we calculate the BIC for each ki multiple times (100 times), following the procedure in Jones et al. (2019). Finally, the mean BIC value and the standard deviation is derived for each ki.

We apply the GMM on the molecular carbon isotope 13CO (3 →2) since it is not strongly affected by foreground absorption effects which “artificially” change the spectral shape, i.e., dips in the spectrum. In addition, the 13CO emission does not show high-velocity wings. The determined BIC for the 13CO (3 →2) data cube isshown in Fig. 9. The black dots represent the mean BIC value and the error bars the standard deviation (which is small and thus almost not visible in the plot). We reach the minimum value at k = 5, implying that the 3D data cube can be clustered into five different regions. The average spectra of each cluster, along with their locations, are shown in Fig. 10. The strong ring emission is shown by the orange cluster 2 and the corresponding averaged spectrum of the ring is indicated by the orange spectrum in the upper panel of Fig. 10. Clusters 1 and 5 surround cluster 2 as shown in the lower panel of Fig. 10. The superposition of their average spectra almost coincides with the average spectrum of cluster 2. All three clusters form the emission by the ring in RCW 120 as indicated by the contours. The velocity shift between clusters 1 and 5 indicate that even the dense ring has a complex velocity structure. Cluster 3 (green) is mainly visible in the two lanes at the center of the bubble and around the ring. The two lanes are also visible in Hα in absorption and thus are located at the nearside of the region. Finally, cluster 4 (red) mainly shows the weak CO emission from the inner part of the bubble.

thumbnail Fig. 9

Bayesian information criterion. The black points represent the mean BIC value for each cluster ki of the 13CO spectral cube. The error bars (which are very small and thus almost not visible) show the standard deviation. A parabolic fit is also shown (see blue line) visualizing the trend of the data points.

thumbnail Fig. 10

GMM clusters. Top panel: the average spectra of the clusters are plotted in different colors. Bottom panel: the corresponding cluster locations, adopting the same color scheme, are shown. The integrated 13CO (3 →2) emission is indicated by the contours.

4.4 Physical properties of the CO (3 →2) emission

4.4.1 Average CO spectra

Similar to the [C II] spectra we fit the radiative transfer Eq. (3) for multiple components distributed between two layers to the observed CO (3 →2) spectra. The optical depth as a function of column density and excitation temperature is given by (Mangum & Shirley 2015): τ CO,i (v)= ϕ i (v) N CO,i 8 π 3 μ 2 J u 3hc ( k B T ex,i hB + 1 3 ) 1 e T u T ex,i ( e T 0 T ex,i 1 ), \begin{equation*}\tau_{\mathrm{CO}, i}(v) = \phi_i(v)N_{\mathrm{CO}, i}\frac{8\pi^{3}\mu^2J_u}{3hc} \left(\frac{k_{\mathrm{B}} T_{\mathrm{ex},i}}{hB}+\frac{1}{3} \right)^{-1}e^{\frac{-T_u}{T_{\mathrm{ex},i}}}\left(e^{\frac{T_0}{T_{\mathrm{ex},i}}}-1 \right),\end{equation*}(22)

with the dipole moment μ, the upper J-level Ju, the rotational constant B and the temperature of the upper level Tu, which can be approximated as: T u = hB J u ( J u +1) k B . \begin{equation*}T_u = \frac{hBJ_u(J_u+1)}{k_{\mathrm{B}}}.\end{equation*}(23)

The average (over the PDR ring) excitation temperature of the warm emitting background is determined with Eq. (7) to be ~40 K. This value is the same value as in Luisi et al. (2021). For the cold absorbing foreground, we assume a temperature of 6 K as a typical value for cold molecular clouds. We note that for larger foreground temperatures the model fit goodness decreases drastically unable to reproduce the observed CO (3 →2) lines. The assumptions of constant excitation temperature for all velocity components in the background and foreground, respectively, is justified: for the background, the velocity components that contribute the most to the emission are the ones around the bulk emission of the cloud (around −7.5 km s−1) and thus all arise from the same volume of gas. The foreground velocity components are slightly more scattered in velocity, but here, the assumption that we have uniform conditions in the cold gas phase is straightforward and justified.

To determine the emitting background layer, we fit the less abundant isotopologue 13CO (3 →2) with the model first. The corresponding 12CO (3 →2) emitting layer is then determined by scaling up the 13CO column density with the carbon abundance ratio. However, there are components which are only visible in the main isotope but lost in the noise of the weaker 13CO (3 →2). These background components are added in the second step. Finally, the model fit is used on both molecular CO lines simultaneously, including the foreground layer, while the previously determined background layer is fixed. This simultaneous fit ensures that the additional background components are only visible in the main isotope and that the determined absorbing foreground is only affecting the 12CO (3 →2) line.

The two-layer multicomponent fit for the averaged spectra is shown in Fig. 11 and the physical properties for each cluster in Table 2. The left column in Fig. 11 displays the spatial cluster location, the middle and right columns show the 13CO (3 →2) and 12CO (3 →2) model fits, respectively. Similar to the findings for the ionized carbon, the emitting background layer is overshooting the observed main isotope line significantly. This requires a cold absorbing foreground which absorbs a significant amount of the 12CO line. The optical depths for 12CO for the background emission are still high (Table 2), but more of the order of a few and not of a few 10s like in the single-layer model. The background column density of the molecular gas is of the order of 1–10 × 1021 cm−2. The molecular ring surrounding the H II region is described by cluster 1,2 and 5, which gives a total mass of ~ 2200 M for the emitting background and ~670 M for the cold absorbing foreground. This is a lower limit, since we do not see the material behind the warm emitting layer.

While the numbers of components varies for the emitting background (see tables in Appendix C.2), we find that the foreground is best described by three components: a component approximately located at the systemic velocity of RCW 120 around −7.5 km s−1 and a blue-shifted and red-shifted component. The absorbing component at the systemic velocity can be attributed to a temperaturegradient between the observer and the warm emitting ring, formed due to the decreasing stellar radiation with distance from the ionizing star. However, the two additional velocity-shifted components suggest a more complex geometry and dynamics than the simple assumption of a spherical molecular cloud enveloping the ionizing star. We already assumed from the opacity calculations for the single layer model (Sect. 4.1) that dynamics play an important role in understanding the CO emission features and we propose the following scenario: Luisi et al. (2021) reported a fast (~15 km s−1) expanding [C II] bubble that impacts the surrounding molecular cloud. The expanding bubble drives a shock wave into the surrounding gas, sweeping it up into a shell. The inside of this shell is ionized and separated from the warm atomic gas in the PDR by the ionization front. For a large enough column, the PDR layers further away from the UV source will become molecular and this molecular gas would move at the velocity of the shell. There is no communication between the gas in front of the shock front and behind it. The momentum transfer occurs in the shock front associated with the outer boundary of the shell. However, the red-shifted component cannot be simply attributed to the red-shifted expanding shell, since a possible absorbing layer would be located at the rear side of the region where absorption features can not be detected. Thus, a red-shifted component with respect to the systemic velocity indicates an inflow of cold molecular material towards RCW 120.

thumbnail Fig. 11

Two-layer multicomponent model fit to the average spectra of each cluster determined by the GMM. Left column: the black contours indicate the spatial location of the clusters. Area that is located outside the clusters is dark shaded. Following the middle and right columns: 13CO and 12CO (3 →2) model fits. All other parameters are as shown in Fig. 8. The red spectra in the upper left panelsindicate the observed CO lines and the green curve is the resulting model fit. In the panel below, the gray data points show the fit residual and the two horizontal orange lines indicate the 3σ level. In the upper right panels, the dark blue lines show the single Gaussian components and the light blue line the superposition of all synthetic background components. In the lower right panels, the pink line displays the single foreground Gaussian components and the magenta line shows the superposition of all synthetic foreground components. The dashed orange line indicates the velocity resolved optical depth.

Table 2

Physical properties of the emitting and absorbing layers along the ring of RCW 120 from CO (3 →2).

4.4.2 Entire spectral CO cube

In the following, we use the model fits of the average spectra as an input for the entire spectral cube to resolve the spatial distribution of the two layers. Like for the average cluster spectra we first fit the 13CO (3 →2) data cube with the two-layer multicomponent model assuming weak foreground absorption. The resulting model fit is scaled up by the local carbon abundance ratio to determine the 12CO (3 →2) emitting background layer. However, for the full cube we need to take into account that the noise in each pixel is much higher than for the average cluster spectra. Simply using the number of background components determined from the averaged spectra might lead to “over-fitting”, thus assuming more background components than visible in a single spectrum can result in fitting of noise fluctuations which scaled up by the carbon abundance ratio are visible as artifacts in the resulting synthetic map. We thus perform the model fit in a sequential way: the model fit to each pixel is started with the strongest background component, afterwards the goodness of the model fit is tested. If the reduced chi-squared is approximately χ R 2 ~1 $\chi_{\mathrm{R}}^2 \sim 1$, no further background component is added. Otherwise the sequential model fit is continued.

The resulting synthetic 12CO (3 →2) map of the emitting background layer is shown in the left panel of Fig. 12. Even though the map is derived from the observed 13CO (3 →2) spectral cube, the map reveals a different spatial distribution because the 12CO line is optically thick. In order to reveal the “real” 12CO distribution (unaffected by optical depth effects), we determine the 12CO column density using Eq. (22) and show channel maps of this synthetic column density in the top panel of Fig. 13. The velocity resolved 12CO column density of the warm emitting layer now has a similar spatial distribution as the 13CO (3 →2) emission (compare to Fig. 4).

In a second step, we determine the spatial distribution of the cold absorbing foreground layer. We run the two-layer multicomponent model on both CO isotopologues simultaneously and use the previously determined background cube as input. Again, possible additional background components (only visible in 12CO (3 →2)) and the foreground components, derived from the averaging spectra of the clusters, are added iteratively until the model fit goodness is sufficient.

The resulting emission map of the cold foreground layer is shown in the middle panel of Fig. 12. In contrast to the warm emitting background, the ring-like structure characteristic for RCW 120 is barely visible. Moreover, we observe an almost homogeneous emission pattern. However, we learned from the analysis of the background map that the true distribution of the molecular gas is better revealed in the column density channel maps, which are shown in Fig. 13. Between the velocity range of − 12 to − 9 km s−1, we observe a rather homogeneous density distribution with a slight increase towards the inner ring. At velocities between − 9 to − 6 km s−1, thus close to the systemic velocity of RCW 120, we find an increased foreground correlating with the absorption features visible in the 12CO (3 →2) channel maps in Fig. 4.

However, the observed increase of foreground material toward the center of the H II region does not have a significant impact on the observed molecular deficit. The CO column density for the background and foreground layer along two cuts through the ionizing star are shown in the right panel of Fig. 12. The column density of the cold absorbing layer is indicated by the green curve, which shows little variation along the cuts and has a low contributionto the overall column density. Thus, most of the molecular column density is found in the dense PDR ring.

For velocities red-shifted from the systemic velocity of the cloud, the ring-like structure emerges in the foreground column density. This may suggest some inflow, i.e., the ring is still accumulating mass which then serves as a reservoir for further star-formation. Figueira et al. (2017) reported an over-density of compact sources in the ring with respect to the whole molecular cloud. A total of at least 35 compact, prestellar sources were found. We note that the red-shifted feature is only visible in the 12CO maps that were extracted using both molecular isotopes in order to disentangle self-absorption effects from kinematic features.

thumbnail Fig. 12

Line integrated 12CO (3 →2) synthetic maps and cuts. Left panel: spatial distribution of the warm background emitting layer. Middle panel: spatial distribution of the cold foreground absorbing layer. Right panel: position-intensity diagram along the two cuts indicated by the gray lines crossing the ionizing star. The upper panel shows the horizontal cut and the lower panel shows the diagonal cut. The orange curve is showing the column density of the emitting background layer, the green curve shows the column number density of the absorbing foreground layer and the blue curve indicates the combined column density of both layers.

thumbnail Fig. 13

Velocity resolved 12CO column density maps of the warm emitting background layer (top) and the cold absorbing foreground layer (bottom).

thumbnail Fig. 14

Geometrical effects of a spherical shell. Left panel: visualization of the radial profile that would provide the projected column number density distribution in the central panel along a cut through the bubble center. Right panel: dependence of the apparent shell width (red) and the limbbrightening factor (black) on the geometric shell width. The observed [C II] and CO (3 → 2) shell widths and limb brightening factors are overplotted. The error bars indicate the variation of both quantities along the observed ring.

4.5 Geometric modeling of RCW 120

For star-formation embedded in the parental molecular cloud we expect that the produced H II region expands isotropically as long as the surrounding medium is isotropic on the size scale of the H II region. By focusing here on [C II] and CO (3 →2) emission, tracing only the warm gas around the H II region, we characterize the structure and velocity in the direct vicinity of the H II region unaffected by the geometry of the molecular cloud on larger scales. In case of a spherically symmetric expanding H II region inside a molecular cloud one would indeed expect to observe a ring-like intensity structure like in RCW 120 due to limb brightening at the edge of the bubble. However, in the following we show that the parameters of the observed structure are inconsistent with a spherically symmetric configuration.

A simple estimate is possible based on purely geometric arguments. The intensity profiles in Fig. 3 show a width of the bright rim of about 0.7–0.8 pc (FWHM) for CO (3 →2) and 13CO (3 →2). In [C II] it is somewhat narrower (0.4–0.6 pc). The intensity contrast between the rim peak and the inner part of the bubble is 5–10 in CO (3 →2), above 10 in 13CO (3 →2) and between 3 and 5 in [C II]. If we assume the most simple configuration of a spherical shell, the actual width of the shell will affect both the apparent width and the intensity contrast between shell center and rim. A thinner shell will allow for a stronger limb brightening providing a higher intensity contrast, but it will also lead to a narrower apparent shell width. This is illustrated in Fig. 14. The left and central panels show the geometry and projected column for an example shell with a width of 0.7 pc. The limb brightening from the LOS integration provides a maximum contrast between rim and center of a factor of 2.7. Such a setup would provide approximately the observed rim width, but a too low contrast compared to the observed values. The right panel visualizes the outcome of a parameter scan when changing the shell width. The black line shows the resulting intensity contrast, the red line the apparent rim width. For comparison we added the observed ranges for CO (3 → 2) and [C II]. The error bars indicate the variations of both quantities along the ring. One sees that for [C II] a shell width of about 0.6 pc could provide a marginal fit to both the rim width and the intensity contrast while for 12CO (3 →2) both numbers are mutually exclusive. We find a strong discrepancy between the observed 12CO (3 →2) limb brightening factor and the observed shell width. This discrepancy is even stronger for the molecular isotope 13CO (3 →2), where we detect a limb brightening factor of larger than >10 for a shell with of about ~ 0.7 pc. Of course, the simple homogeneous shell is a nonrealistic over-simplification, but as one can build any radial distribution from a series of such shells, it is obvious that other radial profiles typically only worsen the discrepancy as they will have an even lower contrast ratio compared to the shell in this geometric example.

For optically thin lines, that basically provide a LOS integration, the data are therefore incompatible with a spherical structure. However, one might ask whether LOS absorption may provide the observed contrast ratio enhancement. To answer this question we ran full radiative transfer computations using SimLine (Ossenkopf et al. 2001). We did not try to perform a detailed χ2 -fit for best cloud parameters but we only show the fundamental radiative transfer effects for an example of parameters that are in rough agreement with the overall geometry. Results are shown in Fig. 15. The upper panel displays an experiment based on the simple geometry discussed above using gas temperatures from Sect. 4.2. A homogeneous shell with a thickness of 0.7 pc, a density of 103 cm−3, and a kinetic temperature of 80 K is surrounded by a shell with the lower kinetic temperature of 15 K. The C+ abundance in that outer shell is varied to create a variable level of absorption. In the low optical depth case we recover an intensity distribution similar to the geometric picture from Fig. 14, however, with a lower limb brightening compared tothe idealized geometric integration. Adding surrounding material with an increasing optical depth actually worsens the situation by absorbing relatively more from the bright rim than in the center of the configuration. The marginal match for the [C II] data in Fig. 14 therefore vanishes if one uses full radiative transfer computations. To show that this conclusion is not limited to the artificial two-shell setup, the lower plot uses a continuous density and temperature structure with power law profiles for temperature and density. The thin shell is mimicked by a very steep radial density decrease with a power of −8. The temperature drops from 80 K with a radial exponent of −2. Here, we visualize the CO (3 →2) lines5. The picture confirms the same behaviour; an increasing optical depth lowers the contrast between rim and center in all cases instead of increasing it. Radiative transfer cannot solve the contradiction found in Fig. 14, it rather worsens it. The same holds when including a velocity field for the expansion of the bubble. It tends to increase the absorption in the rim while decreasing it in the center. All of our SimLine experiments with more realistic parameters for RCW 120 in a spherically symmetric configuration lead to line predictions that deviated even more strongly from the observed lines than in the simple geometric picture described above.

We conclude that the large limb brightening factor for a ring of the observed thickness cannot be explained by a spherical symmetric geometry, but it requires rather a torus-like structure surrounding the expanding H II region. The warm molecular emission must come from a primordially flat structure forming the ring, excluding an isotropic configuration. Even though we detect an expanding bubble in the velocity resolved [C II] spectra (Luisi et al. 2021), we find that the observed [C II] limb brightening factor is not compatible with the observed shell width. The [C II] emission must also originate, at least partially, from the surface of the molecular torus forming a PDR (see also Sect. 4.2.2). The observed 2D ring structure is a superposition of the expanding shell and the torus surrounding the H II region.

thumbnail Fig. 15

Modeled intensities from the radiative transfer in a spherically symmetric bubble. Top panel: modeled [C II] intensity for simple shell geometries (Fig. 14) for various optical depths of surrounding cold material. Bottom panel: modeled 12CO and 13CO (3 →2) intensities for a slightly more realistic configuration with a continuous density and temperature gradient. The modeled intensities are determined by solving the radiative transfer equations with SimLine (Ossenkopf et al. 2001).

thumbnail Fig. 16

Observed and scaled H I spectra. The blue curve shows the averaged H I emission from the PDR ring area observed in [C II]. The orange spectrum is the Off-position (without an absorption dip) thatis indicated in Fig. 1. The red spectrum is the same spectrum, scaled up by afactor of 1.2 in order to match the wing emission of the average On-spectrum between −20 and 20 km s−1. The green curve displays a Gaussian fit to the scaled up Off-position.

4.6 Hydrogen self-absorption

The presentation of the H I spectra in Sect. 3.2.2 revealed that H I self-absorption (HISA) is found at the same velocities where [C II] and CO (3 →2) show self-absorption features (broad self-absorption across a velocity range of around −6 to −11 km s−1 and a strong dip at ~ − 7.5 km s−1). From the [C II] self-absorption analysis (Sect. 4.2.2), we derived that substantial column densities of cold foreground material must be responsible for the absorption. In the following, we assess if cold, atomic gas can be this gas component.

Figure 16 shows in blue the H I spectrum averaged over the PDR ring where we have reliable values of the [C II] column density (Table 1). As in the single spectra, we observe a dip in the spectrum near the systemic velocity of RCW 120. To quantitatively determine the absorption we first need to determine the strength of the warm background emission. Todo so we assume that the cold absorbing hydrogen cloud is a local feature compared to the extended background emission, similar as it was done in Wang et al. (2020). An appropriate Off-position, free of HISA, needs to be close enough to the source to be exposed to the same background radiation, but far enough to be free of absorption features. The orange spectrum in Fig. 16 was selected as a reasonable Off-position (centered at RA(2000) = 17h12m21.6s, Dec(2000) = −38°00′35.9″, see Fig. 1) and represents an average over an area three times the beam size π (1503/2) 2 arcsec 2 $\pi(150\cdot3/2)^2\,\mathrm{arcsec^2}$. However, the H I emission outside RCW 120 is not homogeneous but shows some variation in intensity. Therefore, we tested different approaches to deal with the resulting uncertainty. We scaled up the Off-spectrum by a factor of 1.2, so that the wings of the Off-spectrum, in the range of [−20, 20] km s−1 match the wings of the blue On-spectrum. The resulting spectrum is shown in red in Fig. 16. The shape of the Off-spectrum also shows some variation and a small dip at −9 km s−1 might indicate that the spectrum is not completely free of HISA. Thus we also performed a single Gaussian component fit to the scaled spectrum (green curve in Fig. 16). In the following we use the parameters for position, width and intensity of this Gaussian for the calculations but will propagate the uncertainties from the insufficient knowledge on the Off-spectrum in the discussion.

The velocity resolved intensity difference between the On- and Off-spectra Ton-off(v) = Ton(v) − Toff(v) can be written as a function of the HISA optical depth τHISA(v) and temperature THISA, describing the excitation temperature of the absorbing H I material, (Wang et al. 2020): T on-off (v)=( T HISA p T off (v) T cont )(1 e τ HISA (v) ), \begin{equation*}T_{\mathrm{on-off}}(v) = (T_{\mathrm{HISA}}-pT_{\mathrm{off}}(v)-T_{\mathrm{cont}})\cdot(1-\textrm{e}^{-\tau_{\mathrm{HISA}}(v)}),\end{equation*}(24)

with the background continuum temperature Tcont and the dimensionless parameter p: p= T bg ( 1 e τ fg ) T off , \begin{equation*}p = \frac{T_{\mathrm{bg}}\left(1-\textrm{e}^{-\tau_{\mathrm{fg}}}\right)}{T_{\mathrm{off}}},\end{equation*}(25)

which is defined between [0, 1] and accounts for possible foreground emission. A value of p = 1 means that there is no foreground emission; for p = 0, there is no background emission (see also Wang et al. 2020, for a more detailed derivation and discussion of the equations). In the following we assume p = 1, thus all emission originates from the warm background. The main background is the overall warm Galactic H I emission background (Jackson et al. 2002; Li & Goldsmith 2003). The continuum temperature is derived from the SGPS continuum map at 1.4 GHz and displayed in the top right panel of Fig. 17. For a given HISA temperature we can determine the velocity resolved optical depth τ HISA (v)=ln( 1 T on-off (v) T HISA T off (v) T cont ) \begin{equation*}\tau_{\mathrm{HISA}}(v) = -\ln\left(1-\frac{T_{\mathrm{on-off}}(v)}{T_{\mathrm{HISA}} -T_{\mathrm{off}}(v)-T_{\mathrm{cont}}} \right)\end{equation*}(26)

and then the HISA column density (Wilson et al. 2009): N HISA cm -2 =1.8224× 10 18 T HISA K τ HISA (v)d( v km s -1 ). \begin{equation*}\frac{N_{\mathrm{HISA}}}{\mathrm{cm^{-2}}} = 1.8224\times 10^{18}\frac{T_{\mathrm{HISA}}}{\mathrm{K}}\int\tau_{\mathrm{HISA}}(v)\,\textrm{d}\left(\frac{v}{\mathrm{km\,s^{-1}}} \right).\end{equation*}(27)

Apart from the background intensity, the HISA temperature is another uncertainty factor, since we cannot determine it independently from the optical depth. An upper limit for the possible HISA temperature can be derived from Eq. (26) for τHISA: T HISA,max = T on,min + T cont , \begin{equation*}T_{\mathrm{HISA,max}} = T_{\mathrm{on, min}} + T_{\mathrm{cont}},\end{equation*}(28)

with the absorption dip minimum temperature Ton,min. The upper limit HISA temperature distribution is shown in the lower left panel of Fig. 17 which varies between 60 K and 100 K. Simply using Ton,min is not feasible, since it would result in infinitely large column densities. Thus, we subtract the rms from the On-position ΔTon: T HISA,max = T HISA,max Δ T on . \begin{equation*}T\prime_{\mathrm{HISA,max}} = T_{\mathrm{HISA,max}} - \Delta T_{\mathrm{on}}.\end{equation*}(29)

The derived column density becomes very temperature sensitive close to THISA,max and thus sensitive to the noise level as illustrated in Fig. 18. The determined HISA column density distribution is shown in the lower right panel of Fig. 17, the values range between 3–6 × 1021 cm-2. Even though the column density variations are small, they lead to the formation of filamentary structures in the cold absorbing hydrogen layer. However, these structures need to be treated with caution because the map gridding is very high, matching the resolution of the [C II] and CO maps used in this work, with respect to the low resolution of the H I data (~2′).

Channel maps of the velocity resolved HISA column density are shown in Fig. 19. Similar to the cold molecular material most of the observed HISA mass is found at blue-shifted velocities or at the systemic velocity ~ − 7.5 km s−1. We emphasize again that though the filamentary structures are real, they are artificially enhanced because of the high gridding. Interestingly, we observe a weak ring-like structure, similar to the CO- and [C II] ring emission around the bubble, starting at velocities around − 7 km s−1 and then continuing to red-shifted velocities. This may be an indication of a possible inflow of atomic gas on the molecular torus, as already tentatively seen in CO (Sect. 4.4.2).

thumbnail Fig. 17

HISA properties. Top left: line integrated H I emission between −20 to 10 km s−1. Top right: continuum temperature map from 1.4 GHz emission. Lower left: upper limit of HISA temperature. Lower right: HISAcolumn density distribution. The contours give the line integrated [C II] intensity levels 60, 100, 140, 180, 220 K km s−1, ranging from black to light gray.

thumbnail Fig. 18

Column densities of absorbing H I. The orange, red and green curves show the HISA column density as a function of temperature for the Off-position, the scaled up version, and the Gaussian fit, respectively (see Fig. 16).

5 Discussion

5.1 The nature of the [C II] absorbing foreground layer

In Sect. 4.2.2, we found a layer of gas that is absorbing a significant amount of emission in [C II]. Similar to the findings of Guevara et al. (2020), who reported for various sources that there is a substantial column density of gas located in a cold [C II] foreground layer which is atomic or molecular or a mixture of both.

We can now quantitatively investigate the hypothesis that the layer of cold C+ is the same material that produces the HISA, this means that the [C II] absorption occurs in atomic gas with HISA temperature. If C+ is mixed with atomic hydrogen, we can compute the relation between HISA temperature, the [C II] excitation temperatureand the density of the gas. Together with the known column density of the foreground layer this turns into alength of the absorbing column. Figure 20 shows the excitation temperature Tex, [C II] of [C II], as a function of the density in the atomic gas, assuming that C+ is only excited through collisions with atomic hydrogen (collisional cross sections from Barinovs et al. 2005). The black dotted line indicates Tex, [C II] = 30 K, our upper limit, the curves were calculated for THISA between 60 K and 90 K. The HISA temperature has a small influence on the density for the temperature regime of low Tex, [C II]. The relation allows us to discuss reasonable limits for Tex, [C II]. Using an average of HISA temperature of 80 K and Tex, [C II] = 30 K, we obtain a density of 500 cm−3 for the HISA layer and thus a LOS extent of ~5 pc. A somewhat smaller [C II] excitation temperature of ~20 K results in a density of ~ 120 cm−3 and a larger extent of ~12 pc for the HISA cloud. Even lower excitation temperatures can be excluded because they would result in a required length of the absorbing column that exceeds the size of the configuration by a large factor being highly unlikely for associated gas.

Figure 21, which will be discussed in more detail in the next subsection, qualitatively shows the layering of the H II region bubble, the PDR ring, the molecular cloud and the enveloping H I layer. Though due to the uncertainties we cannot further narrow down the values for the extent of the H I layer, we demonstrate that the derived LOS extent of the H I cloud is reasonable with respect to the diameter of the H II region bubble (4.5 pc) and the larger molecular cloud (~10 pc). We note that Kirsanova et al. (2019) also concluded that there is a foreground absorbing cloud. However, they estimated a gas density n= n HI +2 n H 2 $n = n_{\textrm{{HI}}} + 2n_{\textrm{H}_2}$ of 50 cm−3 and a LOS extend of 1 pc of the cloud, much lower than what we obtain.

Summarizing, we think that in the case of RCW120 a large fraction of the C+ absorbing foreground material is atomic. It is known since long that H I halos exist around molecular clouds (Burton et al. 1978; Williams & Maddalena 1996; Lee et al. 2012; Motte et al. 2014; Imara & Burkhart 2016; Wang et al. 2020) and RCW 120 is not an exception (see Fig. 1 and Torii et al. 2015). Detecting HISA features, however, is not always evident. Jackson et al. (2002) stated that several criteria must be satisfied. First, the molecular cloud must be enveloped by a significant amount of cold H I with a high enough opacity (τHI ≥ 1), and second, there must be sufficient background emission from warm H I. These requirements are fulfilled in RCW 120. We assume that the carbon in the atomic cloud is ionized mostly by cosmic rays because even though UV radiation and X-rays “leak” through punctures in the PDR ring (Luisi et al. 2021), the UV field is fast attenuated with distance d by a factor 1/d2. This is an assumption, however, we cannot investigate with the current data set.

5.2 Flat molecular clouds around H II region bubbles and a possible scenario of the RCW 120 region

Beaumont & Williams (2010) presented observations in the CO (3 →2) transition line of 43 H II bubbles identified by the Spitzer Space Telescope. They reported a deficit in CO emission towards the center of the observed rings, proposing that the associated molecular cloud must be “flat” and not spherical. We made the same observation for RCW 120 and showed quantitatively (Sects. 4.4 and 4.5) that this CO deficit is not due to self-absorption effects, that could mimic missing emission, but a real shortfall of emission. In addition, we proposed that CO self-absorption at red-shifted velocities could “hide” high-velocity gas that is falling on the dense molecular ring and similarly, at blue-shifted velocities, could prevent to detect expansion features in the molecular gas (no signs of expanding CO bubbles were found in the CO data that was not corrected for self-absorption). The density of this molecular gas is probably low, because high-velocity emission, i.e. infalling gas or an expanding molecular ring was not detected in 13CO, which is not affected by self-absorption. However, these conclusions are tentative and need further comparative studies of [C II], CO, and H I in other H II region bubbles.

In Figs. 21 and 22, we portray the RCW 120 star-forming region and speculate about its formation and evolution. We propose that we see RCW 120 in a stage of evolution in which a massive star formed inside a collapsing filament and the current H II region now bursts out of the remaining, nonfilamentary, but “flat” cloud structure. The velocity resolved [C II] spectra shown in Luisi et al. (2021) revealed an expanding C+ bubble that swept up the surrounding material to a structure that is visible in the plane of the sky as a ring. The expanding bubble powered by stellar wind (Luisi et al. 2021), transfers momentum into the surrounding molecular cloud. The compression of the ambient molecular cloud was confirmed by observations of asymmetric column density profiles (Zavagno et al. 2020) and double-peak features in the column density probability distribution functions (Tremblin et al. 2014). This compression continues even after the bubble bursts out of the filament/sheet, in contrast to a pressure driven H II region. The accumulation and compression of the ambient molecular clouds triggers additional star formation along the ring in RCW 120 (Deharveng et al. 2009; Figueira et al. 2017). Thus, missing young stellar objects (YSOs) along the line of sight towards the interior of the ring are an additional hint that the surrounding molecular cloud has a sheet-like geometry (Anderson et al. 2015). A longitudinally collapsing filament (Schneider et al. 2010) additionally compresses the molecular gas and may have built up the prominent ridge seen in the south of RCW 120 (the north part is no longer visible because the H II region created a hole in the structure). In general it is observed that the geometry of molecular clouds is flattened or filament-like (e.g., Bally et al. 1989; de Geus et al. 1990; Heiles & Troland 2003; Molinari et al. 2010; André et al. 2010). Though there are different views of how dense structures are forming (quasi-static vs. dynamic scenarios), our proposed scenarios fit in both cases. In the quasi-static view, a collapsing cloud would first contract along its shortest axis towards a sheet-like geometry and then further collapse to a filament-like shape (Lin et al. 1965). Since the free fall time of an elongated cloud is much larger than the one of a spherical configuration (Toalá et al. 2012; Pon et al. 2012), clumps inside a sheet or filament will collapse faster than the global molecular cloud, leading to star formation inside sheet-like molecular clouds. In turbulent, magneto-hydrodynamic simulations (e.g., Audit & Hennebelle 2005; Banerjee et al. 2009; Vázquez-Semadeni et al. 2006), sheets and filaments form naturally through gas compression in colliding atomic flows.

However, it is important to note that such a finding might be strongly biased towards sheet-like geometries. Ring-like structures are more likely to be observed originating from sheet-like molecular clouds due to the enhanced contrast between the emission from the surrounding torus and the inner ring. Potential bubbles embedded in molecular clouds sufficiently extended (the extension of the molecular cloud in all three dimensions is much larger than the H II region) are more difficult to detect. The larger column density along the line of sight of an H II region embedded in a molecular cloud increases the optical depth and thus reduces the contrast between the limb brightening shell and the interior of the H II region. Moreover, magnetic pressure will act against the compression perpendicular to the magnetic field lines reducing the accumulation and compression at the ring and will distort the geometry of the H II region (Krumholz et al. 2007).

thumbnail Fig. 19

Channel maps of velocity resolved HISA column density.

thumbnail Fig. 20

Hydrogen density in the absorbing foreground layer (x-axis) and C+ excitation temperature (y-axis) as a function of the HISA temperature.

thumbnail Fig. 21

Cartoon of the RCW 120 region where the observer is located on the right and sees a circular shaped H II region in yellow (which is a 3D bubble in reality), and an expanding C+ shell (red), surrounded by a molecular ring that is fragmented into clumps (blue). The sketch represents a ‘cut’, there is also molecular material in front of the H II region, this becomes clearer in Fig. 22. CO emission arises from the clump interiors and [C II] from the UV-illuminated clump surfaces and the expanding C+ bubble. UV-radiation and X-rays leak into the surrounding molecular cloud and into the enveloping H I cloud (green). This H I layer is our HISA cloud in which carbon is mostly ionized by cosmic rays. The Galactic background (green arrows on the left) is responsible for warm H I.

thumbnail Fig. 22

3D visualization of the RCW120 region to show the oblate geometry of the molecular cloud. The observers perspective is from the right and the line integrated [C II] map is projected on the left side. The spherical H II region (red) is surrounded by the flat, low-density cloud (green). The clumpy PDR (golden clumps) and the expanding C+ bubble (purple) are found in the interface region between H II region and molecular cloud.

6 Summary

We studied the RCW 120 H II region bubble and its associated molecular and atomic cloud, employing data from the SOFIA FEEDBACK [C II] 158 μm legacy program, APEX 12CO and 13CO (3 →2) data, and the Southern Galactic Plane H I 21 cm survey. We analyzed self-absorption and optical depth in these lines and proposed a physical and geometrical model for the RCW 120 region.

  • We determined optical depth effects along the ring of RCW 120 for [C II] and CO (3 →2), employing information from [13C II] and 13CO (3 →2) data. We observe large [C II] optical depth and strong self-absorption in the [C II] line in the velocity range ~ − 12 to ~ − 4 km s−1 with a pronounced dip at −7.5 km s−1, the systemic velocity of the cloud. To disentangle the weak [13C II] hyperfine-transition from the noise floor we averaged over square arcmin large regions along the ring using dendrograms (Rosolowsky et al. 2008). In a second step we solved the radiative transfer equations for multiple velocity components distributed between two layers. This analysis revealed a cold [C II] layer, corresponding to a hydrogen column density of 3–7 × 1021 cm−2, hiding a substantial amount of column number density, which would be otherwise undetected.

  • The H I spectral lines also show self-absorption (HISA) in the same velocity range as [C II]. We performed a nonstandard HISA study and obtained similar H I column densities as the ones from [C II] for the absorbing foreground layer. We thus propose that the large column of cold C+ in RCW 120 arises from a cool, low-density (<500 cm−3) atomic envelope around the region. The size of this HISA cloud is ~5 pc (the exact values depend on the HISA temperature and C+ excitation temperature). The carbon in this cool phase can only be ionized by cosmic rays, and UV-radiation and X-rays that leak through the punctured ring.

  • We observe a deficit of CO (3 →2) emission along the LOS towards the H II region bubble. 12CO has large optical depths and shows self-absorption at the bulk velocity (−7.5 km s−1) of the molecular cloud. We solve the radiative transfer equation for two layers for the entire CO (3 →2) spectral cube and demonstrate that the CO deficit is real and not mimicked by self-absorption. To find initial model parameters for the entire data cube, we group the spectra of the cube using the Gaussian mixture model, an unsupervised machine learning approach to cluster multidimensional data. In a second step we solve the radiative transfer equations for the average spectra of each cluster.

  • The CO analysis revealed that red-shifted gas (with respect to the systemic velocity of ~ − 7.5 km s−1) of RCW 120 is located close to the molecular ring, suggesting that the ring is still accreting material. Blue-shifted gas, that is not detectable without correction for self-absorption, indicates gas motion towards us and may thus signify an expanding molecular ring that was so far undetected.

  • We propose that RCW 120 could be a template for the evolution and geometry of H II regions that expand from inside an initially filamentary or sheet-like structure. We speculate that the filament might have experienced a longitudinal collapse while a massive star was forming inside the filament. The expanding H II region and the collapse accumulated more mass in the H II region/molecular cloud interface and formed a molecular shell that fragmented into clumps and star-forming cores. The expanding H II region is currently bursting out of the sheet/filament and no filamentary structure remains. While the expansion of pressure driven H II region eventually halts, the momentum transfer from the stellar wind will continue the expansion as observed in other sources (Pabst et al. 2019; Tiwari et al. 2021; Luisi et al. 2021), including RCW 120. This scenario is still highly speculative and needs further studies of bubbles in the key line tracers [C II], CO, and H I.

Acknowledgements

This study was based on observations made with the NASA/DLR Stratospheric Observatory for Infrared Astronomy (SOFIA). SOFIA is jointly operated by the Universities Space Research Association Inc. (USRA), under NASA contract NNA17BF53C, and the Deutsches SOFIA Institut (DSI), under DLR contract 50 OK 0901 to the University of Stuttgart. upGREAT is a development by the MPI für Radioastronomie and the KOSMA/Universität zu Köln, in cooperation with the DLR Institut für Optische Sensorsysteme. Financial support for the SOFIA Legacy Program, FEEDBACK, at the University of Maryland was provided by NASA through award SOF070077 issued by USRA. The FEEDBACK project is supported by the BMWI via DLR, Projekt Number 50 OR 1916 (FEEDBACK) and Projekt Number 50 OR 1714 (MOBS - MOdellierung von Beobachtungsdaten SOFIA). N.S., R.S., and L.B. acknowledge support by the Agence National de Recherche (ANR/France) and the Deutsche Forschungsgemeinschaft (DFG/Germany) through the project “GENESIS” (ANR-16-CE92-0035-01/DFG1591/2-1). A.Z. thanks the support of the Institut Universitaire de France. The Australia Telescope Compact Array is part of the Australia Telescope National Facility (grid.421683.a) which is funded by the Australian Government for operation as a National Facility managed by CSIRO. The Parkes radio telescope is part of the Australia Telescope National Facility (grid.421683.a) which is funded by the Australian Government for operation asa National Facility managed by CSIRO. This work was supported by the Collaborative Research Centre 956, subprojects A4, C6 and C1, funded by the Deutsche Forschungsgemeinschaft (DFG), project ID 184018867.

Appendix A Derivation of physical properties

A.1 Cold absorbing [C II] excitation temperature range

We derived the physical properties of the cold absorbing [C II] foreground in front of RCW 120 in Sec. 4.2.2 employing the two-layer multicomponent model (Guevara et al. 2020). The column number density is hereby a function of the optical depth and excitation temperature. Thus, for a chosen excitation temperature the optical depth is the remaining model parameter. To constrain the possible foreground excitation temperature we derived the lower limit from the [C II] energy balance to Tex~ 15K. The upper temperature limit was calculated to Tex ~ 30K from the hydrogen column density derived from the optical absorption measurements towards the ionized gas bubble of the H II region in Zavagno et al. (2007). We note that also the model fit goodness drastically decreases for temperatures above 30 K. The resulting cold foreground [C II] column density variation of N[C II] as a function of excitation temperature is shown in Fig. A.1.

thumbnail Fig. A.1

The [C II] column density of the cool foreground layer in the PDR ring as a function of the excitation temperature.

A.2 Mass and luminosity determinations

The two-layer model applied on the [C II] and CO data gives us the synthetic background and foreground column density and corresponding line intensity. Using the output we can derive further physical parameter such as mass and luminosity. The [C II] column density is converted into a mass of neutral gas by applying the hydrogen to carbon ratio C∕H = 1.6 ⋅ 10−4 (Sofia et al. 2004): M H = N [C\scriptsizeII] C/H m H A , \begin{equation*}M_{\mathrm{H}}=\frac{N_{\mathrm{[C{\scriptsize\,II}]}}}{\mathrm{C/H}}m_{\mathrm{H}}A~,\end{equation*}(A.1)

with the size A of the target area and the hydrogen mass mH. In a similar fashion we derive the total molecular gas mass using the column density determined from the 13CO (3-2) transition. M H 2 = N CO CO/H 2 m H 2 A , \begin{equation*}M_{\mathrm{H_2}}=\frac{N_{\mathrm{CO}}}{\mathrm{CO/H_2}}m_{\mathrm{H_2}}A~,\end{equation*}(A.2)

with the molecular hydrogen mass m H 2 $m_{\mathrm{H_2}}$ and CO∕H2 = 8.5 ⋅ 10−5 as conversion factor (Tielens 2010).

The integrated line intensity I [K km s-1] can be converted to the surface brightness F [W m−2 sr−1]: F=2 k B I ( ν c ) 3 \begin{equation*}F = 2k_{\mathrm{B}} I\left(\frac{\nu}{c}\right)^3\end{equation*}(A.3)

and multiplying this intensity with 4πA gives the luminosity L of the region.

Appendix B Optical depth error

In Sect. 4.1 we derived the velocity resolved optical depth along the torus in RCW 120 for [C II] and CO (3 →2) assuming a homogeneous medium. The optical depth itself is determined by comparing the observed intensities of the two isotopes. However, equation 1 is not analytically solvable, which makes the calculation of the corresponding error not trivial. To do so we first introduce a new variable y which is simply: y= \frac{T_{\mathrm{^12C}}}{αT_{\mathrm{ ^13C}} }= 1 e τ τ  . \begin{equation*}y = \frac{T_{\mathrm{^{12}C}}}{\alpha T_{\mathrm{^{13}C}}}= \frac{1-e^{-\tau}}{\tau}~.\end{equation*}(B.1)

The error of our new variable y can now be derived from error propagation of the observed intensity errors σ_{\mathrm{^12C}} $\sigma_{\mathrm{^{12}C}}$ and σ_{\mathrm{^13C}} $\sigma_{\mathrm{^{13}C}}$ of both isotopes and Δα the uncertainty of the local 12C/13C abundance ratio: nn\beginalignedΔy=& \sqrt{\left| \fracy{T_{\mathrm{^12C}}} \right|^2σ^2_{\mathrm{^12C}}+ \left| \fracy{T_{\mathrm{^13C}}} \right|^2σ^2_{\mathrm{^13C}}+ | y α | 2 Δα }=& \sqrt{\frac{ α 2 T_{\mathrm{^13C}}^2σ^2_{\mathrm{^12C}}+ α 2 T_{\mathrm{^12C}}^2σ^2_{\mathrm{^13C}}+Δ α 2 T_{\mathrm{^13C}}^2T_{\mathrm{^12C}}^2  }{ α 4 T_{\mathrm{^13C}}^4}}\endaligned \begin{equation*}\begin{aligned}\Delta y =& \sqrt{\left| \frac{\partial y}{\partial T_{\mathrm{^{12}C}}} \right|^2 \sigma^2_{\mathrm{^{12}C}} + \left| \frac{\partial y}{\partial T_{\mathrm{^{13}C}}} \right|^2 \sigma^2_{\mathrm{^{13}C}} + \left| \frac{\partial y}{\partial \alpha} \right|^2 \Delta\alpha}\\=& \sqrt{\frac{\alpha^2 T_{\mathrm{^{13}C}}^2 \sigma^2_{\mathrm{^{12}C}} + \alpha^2T_{\mathrm{^{12}C}}^2 \sigma^2_{\mathrm{^{13}C}} + \Delta\alpha^2 T_{\mathrm{^{13}C}}^2 T_{\mathrm{^{12}C}}^2}{\alpha^4 T_{\mathrm{^{13}C}}^4}}\end{aligned}\end{equation*}(B.2)

on the other hand we can determine the error of y by error propagation of the optical depth error: nn\beginalignedΔy=& | y τ | 2 Δ τ 2 = &| y τ |Δτ= &| (1+τ) e τ 1 τ 2 |Δτ .\endaligned \begin{equation*}\begin{aligned}\Delta y =& \sqrt{\left| \frac{\partial y}{\partial \tau} \right|^2 \Delta\tau^2} = & \left| \frac{\partial y}{\partial \tau} \right| \Delta\tau = & \left| \frac{(1+\tau)e^{-\tau} -1}{\tau^2} \right| \Delta\tau~.\end{aligned}\end{equation*}(B.3)

Combination of eq. B.2 and eq. B.3 finally gives us an expression for the optical depth error: Δτ=| τ 2 (1+τ) e τ 1 | \sqrt{\frac{ α 2 T_{\mathrm{^13C}}^2σ^2_{\mathrm{^12C}}+ α 2 T_{\mathrm{^12C}}^2σ^2_{\mathrm{^13C}}+Δ α 2 T_{\mathrm{^13C}}^2T_{\mathrm{^12C}}^2  }{ α 4 T_{\mathrm{^13C}}^4}} . \begin{equation*}\Delta \tau = \left| \frac{\tau^2}{(1+\tau)e^{-\tau}-1} \right| \sqrt{\frac{\alpha^2 T_{\mathrm{^{13}C}}^2 \sigma^2_{\mathrm{^{12}C}} + \alpha^2T_{\mathrm{^{12}C}}^2 \sigma^2_{\mathrm{^{13}C}} + \Delta\alpha^2 T_{\mathrm{^{13}C}}^2 T_{\mathrm{^{12}C}}^2}{\alpha^4 T_{\mathrm{^{13}C}}^4}}~.\end{equation*}(B.4)

Appendix C Two-layer multicomponent fit parameter

C.1 [C II] fit parameter

Tables C.1 to C.8 give the resulting fitting parameter of the two-layer multicomponent model fit for the [C II] spectra along the ring/torus in RCW 120. We sort the results by the areas identified with Dendograms which are basically the brightest PDR regions of the ring. The tables are ordered by region and give the values for the background and foreground velocity components for the foreground [C II] excitation temperatures 15 K and 30 K.

C.2 CO fit parameter

Tables C.9 to C.13 give the fitting results of the two-layer multicomponent model fit for 12CO average spectra. The tables are ordered by the clusters identified with the GMM method and give the values for the background and foreground velocity components for the CO excitation temperatures 40 K for the background and 6 K for the foreground.

Table C.1

Two-layer multicomponent fit results of the RCW 120 PDR with Tex,fg = 15 K

Table C.2

Two-layer multicomponent fit results of the southwestern PDR with Tex,fg = 15 K

Table C.3

Two-layer multicomponent fit results of the southeastern PDR with Tex,fg = 15 K

Table C.4

Two-layer multicomponent fit results of the northeastern PDR with Tex,fg = 15 K

Table C.5

Two-layer multicomponent fit results of the RCW 120 PDR with Tex,fg = 30 K

Table C.6

Two-layer multicomponent fit results of the southwestern PDR with Tex,fg = 30 K

Table C.7

Two-layer multicomponent fit results of the southeastern PDR with Tex,fg = 30 K

Table C.8

Two-layer multicomponent fit results of the northeastern PDR with Tex,fg = 30 K

Table C.9

Two-layer multicomponent fit results of Cluster 1

Table C.10

Two-layer multicomponent fit results of Cluster 2

Table C.11

Two-layer multicomponent fit results of Cluster 3

Table C.12

Two-layer multicomponent fit results of Cluster 4

Table C.13

Two-layer multicomponent fit results of Cluster 5

Appendix D H I and [C II] spectra

Figure D.1 displays an overlay between H I and [C II] spectra at the same angular resolution of ~2′.

thumbnail Fig. D.1

Overlay between H I (black) and [C II] (red) spectra at an angular resolution of 2′ in a grid of 2′. The PDR ring of RCW 120 is indicated with a dashed black circle and the O star with a black star symbol. The velocity and temperature ranges are given in the upper caption. This plot is intended to show qualitatively that thereis a systematic H I depression at velocities around the bulk emission velocity of the cloud at − 8 km s−1. The [C II] line shows self-absorption at that velocity (and flat-top spectra) which is not so prominent in this display because the spectra are smoothed to 2′ resolution.

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2

German Receiver for Astronomy at Terahertz. (up)GREAT (Risacher et al. 2018) is a development by the MPI für Radioastronomie and the KOSMA Universität zu Köln, in cooperation with the MPI für Sonnensystemforschung and the DLR Institut für Planetenforschung.

3

APEX, the Atacama Pathfinder Experiment is a collaboration between the Max-Planck-Institut für Radioastronomie, Onsala Space Observatory (OSO), and the European Southern Observatory (ESO).

4

The Habing field Go relates to the Draine field χ by χ = 1.71 Go where Go is the mean interstellar radiation field from Habing (1968); Draine (1978).

5

The setup ignores that for CO the shell is somewhat larger and the inner temperature somewhat cooler than for [C II] (see Sect. 4.4) but rather tries to allow for a direct comparison with the two-shell setup in the upper panel of Fig. 15.

All Tables

Table 1

Physical properties of the emitting and absorbing layers along the ring of RCW 120 from [C II] using a foreground excitation temperature of 15 K and 30 K, respectively.

Table 2

Physical properties of the emitting and absorbing layers along the ring of RCW 120 from CO (3 →2).

Table C.1

Two-layer multicomponent fit results of the RCW 120 PDR with Tex,fg = 15 K

Table C.2

Two-layer multicomponent fit results of the southwestern PDR with Tex,fg = 15 K

Table C.3

Two-layer multicomponent fit results of the southeastern PDR with Tex,fg = 15 K

Table C.4

Two-layer multicomponent fit results of the northeastern PDR with Tex,fg = 15 K

Table C.5

Two-layer multicomponent fit results of the RCW 120 PDR with Tex,fg = 30 K

Table C.6

Two-layer multicomponent fit results of the southwestern PDR with Tex,fg = 30 K

Table C.7

Two-layer multicomponent fit results of the southeastern PDR with Tex,fg = 30 K

Table C.8

Two-layer multicomponent fit results of the northeastern PDR with Tex,fg = 30 K

Table C.9

Two-layer multicomponent fit results of Cluster 1

Table C.10

Two-layer multicomponent fit results of Cluster 2

Table C.11

Two-layer multicomponent fit results of Cluster 3

Table C.12

Two-layer multicomponent fit results of Cluster 4

Table C.13

Two-layer multicomponent fit results of Cluster 5

All Figures

thumbnail Fig. 1

An overview of RCW 120. Top left: false color image of RCW 120 in Herschel fluxes at 70 μm (blue), 160 μm (green), and 250 μm (red). The H II bubble of RCW 120 stands out prominently. Top right: H I line integrated (v = −20 to 10 km s−1) emission from the SGPS survey (McClure-Griffiths et al. 2005) with contours of Herschel dust column density overlaid (levels Av = 15 to 50 in increments of five). The Herschel data were observed within the HiGAL program (Molinari et al. 2010) and the column density map was produced using the PPMAP method (Marsh et al. 2017). The position where we show an individual spectrum (Fig. 6) is indicated by a blue triangle and the off-position we used for the HISA analysis is marked with a gray triangle. The white and gray squares outline the spectra map displayed in Fig. D.1 and the star symbol indicates the exciting star of RCW 120. Bottom left and right: line integrated 12CO (1 →0) intensity maps of RCW 120 between − 37 to − 20 km s−1 and − 20 to 10 km s−1, respectively. The CO data were taken with the MOPRA telescope and have a resolution of 30″ (Torii et al. 2015).

In the text
thumbnail Fig. 2

Velocity integrated maps of [C II] and CO (3 →2) emission in RCW 120 between − 20 and 10 km s-1. Left panel: line integrated [C II] intensity map. The contours outline the regions extracted with a dendrogram based approach (Rosolowsky et al. 2008; Robitaille et al. 2019), explained in Sect. 4.1. Middle and right panel: line integrated 12CO (3 →2) and 13CO (3 →2) intensity maps, respectively. The contours give the line integrated [C II] intensity levels 60, 100, 140, 180, 220 K km s-1, ranging from black to light gray. The two gray lines indicate cuts displaying the line intensities in Fig. 3. The diagonal line has an angle of 25° with respectto the horizontal line. The exciting O6-8V/III type star CD-38 11636 is marked with a star symbol.

In the text
thumbnail Fig. 3

Position-intensity diagram along two cuts. The positions of both cuts are indicated by the gray lines crossing the ionizing star (central position) in Fig. 2, negative distances are to the east and northeast. The upper panel shows the intensity along the horizontal line and the lower one the intensity along the diagonal cut (25°). The [C II] and 12CO and 13CO (3 →2) intensities are indicated by a blue, orange, and green curve, respectively.

In the text
thumbnail Fig. 4

Channel maps of [C II], 12CO (3 →2) and 13CO (3 →2) emission between −12 and −2 km s−1 integrated insteps of 1 km s−1. Top panel: [C II] line emission. Middle panel: 12CO (3 →2) line emission. Bottom panel: 13CO (3 →2) line emission.

In the text
thumbnail Fig. 5

The three top panels show the line integrated 12CO, 13CO (3 →2) and [C II] emission (from left to right, v = −20 to 10 km s−1). The black square in each panel indicates the area where spectra of these lines are shown in the box below. 12CO and 13CO are indicated in black and blue, respectively, the [C II] spectra in red. We note that there is no scaling for any of the lines. The x- and y-axis for the spectra are shown in the top right panel. The spatial offsets are given in arcmin in all panels, the (0,0) position refers to RA(2000) = 17h12m03.65s, DEC(2000) = −38°30′28.4″ (see upper panels). All spectra were smoothed to an angular resolution of 30″ and are displayed in a grid of 30″. This cutout includes the clump with condensation 1 (Zavagno et al. 2007), indicated by a dashed circle, with its prominent outflow source at offsets ~1.5′,−1′.

In the text
thumbnail Fig. 6

Overlay between [C II] (red), H I (black), and 13CO (3 →2) (blue) spectra at position (0,2′), indicated in Fig. 1. The H I data have an angular resolution of ~2′, the other spectra have a resolution of 30″. This position is a typical example of the line shapes in RCW 120; larger spectral line maps are given in Figs. 5 and D.1.

In the text
thumbnail Fig. 7

Averaged spectra of the structures along the ring of RCW 120, sorted by the regions indicated in Fig. 2 (ring, southwestern PDR, southeastern PDR and northeastern PDR). Left panels: averaged [12C II] and scaled up [13C II] emission by the local abundance 12C/13C-ratio of 59. Right panels: averaged 12CO and 13CO (3 →2) emission. The black data points with error bars indicate the velocity resolved optical depth.

In the text
thumbnail Fig. 8

Two-layer multicomponent model results for the four regions extracted with the Dendogram technique. The left top subfigure is a template for all regions: The observed averaged [C II] spectrum is indicated in the left upper panel in red and the green curve on top is the resulting model fit. In the left middle panel, the temperature axis range is smaller so that the weak [13C II] satellitesaround the main isotope line are clearly visible. The left lower panel shows residuals of the fit in gray and the two horizontal orange lines indicate the 3σ level. In theright top panel the red spectrum once more displays the observed [C II] emission and the dark blue lines show the single Gaussian components. The light blue line is the superposition of all synthetic background components. The dashed orange line indicates the velocity resolved optical depth (values on the right axis). The right lower panel shows the pink single foreground Gaussian components and the violet line indicates the superposition of all the synthetic foreground components. The dashed orange line illustrates again the velocity resolved optical depth.

In the text
thumbnail Fig. 9

Bayesian information criterion. The black points represent the mean BIC value for each cluster ki of the 13CO spectral cube. The error bars (which are very small and thus almost not visible) show the standard deviation. A parabolic fit is also shown (see blue line) visualizing the trend of the data points.

In the text
thumbnail Fig. 10

GMM clusters. Top panel: the average spectra of the clusters are plotted in different colors. Bottom panel: the corresponding cluster locations, adopting the same color scheme, are shown. The integrated 13CO (3 →2) emission is indicated by the contours.

In the text
thumbnail Fig. 11

Two-layer multicomponent model fit to the average spectra of each cluster determined by the GMM. Left column: the black contours indicate the spatial location of the clusters. Area that is located outside the clusters is dark shaded. Following the middle and right columns: 13CO and 12CO (3 →2) model fits. All other parameters are as shown in Fig. 8. The red spectra in the upper left panelsindicate the observed CO lines and the green curve is the resulting model fit. In the panel below, the gray data points show the fit residual and the two horizontal orange lines indicate the 3σ level. In the upper right panels, the dark blue lines show the single Gaussian components and the light blue line the superposition of all synthetic background components. In the lower right panels, the pink line displays the single foreground Gaussian components and the magenta line shows the superposition of all synthetic foreground components. The dashed orange line indicates the velocity resolved optical depth.

In the text
thumbnail Fig. 12

Line integrated 12CO (3 →2) synthetic maps and cuts. Left panel: spatial distribution of the warm background emitting layer. Middle panel: spatial distribution of the cold foreground absorbing layer. Right panel: position-intensity diagram along the two cuts indicated by the gray lines crossing the ionizing star. The upper panel shows the horizontal cut and the lower panel shows the diagonal cut. The orange curve is showing the column density of the emitting background layer, the green curve shows the column number density of the absorbing foreground layer and the blue curve indicates the combined column density of both layers.

In the text
thumbnail Fig. 13

Velocity resolved 12CO column density maps of the warm emitting background layer (top) and the cold absorbing foreground layer (bottom).

In the text
thumbnail Fig. 14

Geometrical effects of a spherical shell. Left panel: visualization of the radial profile that would provide the projected column number density distribution in the central panel along a cut through the bubble center. Right panel: dependence of the apparent shell width (red) and the limbbrightening factor (black) on the geometric shell width. The observed [C II] and CO (3 → 2) shell widths and limb brightening factors are overplotted. The error bars indicate the variation of both quantities along the observed ring.

In the text
thumbnail Fig. 15

Modeled intensities from the radiative transfer in a spherically symmetric bubble. Top panel: modeled [C II] intensity for simple shell geometries (Fig. 14) for various optical depths of surrounding cold material. Bottom panel: modeled 12CO and 13CO (3 →2) intensities for a slightly more realistic configuration with a continuous density and temperature gradient. The modeled intensities are determined by solving the radiative transfer equations with SimLine (Ossenkopf et al. 2001).

In the text
thumbnail Fig. 16

Observed and scaled H I spectra. The blue curve shows the averaged H I emission from the PDR ring area observed in [C II]. The orange spectrum is the Off-position (without an absorption dip) thatis indicated in Fig. 1. The red spectrum is the same spectrum, scaled up by afactor of 1.2 in order to match the wing emission of the average On-spectrum between −20 and 20 km s−1. The green curve displays a Gaussian fit to the scaled up Off-position.

In the text
thumbnail Fig. 17

HISA properties. Top left: line integrated H I emission between −20 to 10 km s−1. Top right: continuum temperature map from 1.4 GHz emission. Lower left: upper limit of HISA temperature. Lower right: HISAcolumn density distribution. The contours give the line integrated [C II] intensity levels 60, 100, 140, 180, 220 K km s−1, ranging from black to light gray.

In the text
thumbnail Fig. 18

Column densities of absorbing H I. The orange, red and green curves show the HISA column density as a function of temperature for the Off-position, the scaled up version, and the Gaussian fit, respectively (see Fig. 16).

In the text
thumbnail Fig. 19

Channel maps of velocity resolved HISA column density.

In the text
thumbnail Fig. 20

Hydrogen density in the absorbing foreground layer (x-axis) and C+ excitation temperature (y-axis) as a function of the HISA temperature.

In the text
thumbnail Fig. 21

Cartoon of the RCW 120 region where the observer is located on the right and sees a circular shaped H II region in yellow (which is a 3D bubble in reality), and an expanding C+ shell (red), surrounded by a molecular ring that is fragmented into clumps (blue). The sketch represents a ‘cut’, there is also molecular material in front of the H II region, this becomes clearer in Fig. 22. CO emission arises from the clump interiors and [C II] from the UV-illuminated clump surfaces and the expanding C+ bubble. UV-radiation and X-rays leak into the surrounding molecular cloud and into the enveloping H I cloud (green). This H I layer is our HISA cloud in which carbon is mostly ionized by cosmic rays. The Galactic background (green arrows on the left) is responsible for warm H I.

In the text
thumbnail Fig. 22

3D visualization of the RCW120 region to show the oblate geometry of the molecular cloud. The observers perspective is from the right and the line integrated [C II] map is projected on the left side. The spherical H II region (red) is surrounded by the flat, low-density cloud (green). The clumpy PDR (golden clumps) and the expanding C+ bubble (purple) are found in the interface region between H II region and molecular cloud.

In the text
thumbnail Fig. A.1

The [C II] column density of the cool foreground layer in the PDR ring as a function of the excitation temperature.

In the text
thumbnail Fig. D.1

Overlay between H I (black) and [C II] (red) spectra at an angular resolution of 2′ in a grid of 2′. The PDR ring of RCW 120 is indicated with a dashed black circle and the O star with a black star symbol. The velocity and temperature ranges are given in the upper caption. This plot is intended to show qualitatively that thereis a systematic H I depression at velocities around the bulk emission velocity of the cloud at − 8 km s−1. The [C II] line shows self-absorption at that velocity (and flat-top spectra) which is not so prominent in this display because the spectra are smoothed to 2′ resolution.

In the text

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