Free Access
Issue
A&A
Volume 593, September 2016
Article Number L14
Number of page(s) 7
Section Letters
DOI https://doi.org/10.1051/0004-6361/201629442
Published online 22 September 2016

© ESO, 2016

1. Introduction

High-mass stars, multiple systems, and clusters are born from the gravitational collapse of massive, dense clumps (compact structures with M ≥ 100M, and n(H2) ≥ 104 cm-3) inside large molecular clouds. Stars more massive than 8 M are expected to form either through direct accretion of material in massive cores within the clump that does not fragment further (e.g. McKee & Tan 2003; Tan et al. 2013), or as a result of a dynamical evolution where several low-mass seeds competitively accrete matter in a highly fragmented clump (Bonnell et al. 2004). In the latter scenario, each clump forms multiple massive stars and many lower mass stars: the unlucky losers in the competitive accretion competition. There is still vigorous debate on which of these scenarios is more likely to occur, and fragmentation appears to be particularly important in this debate. Theoretical models and simulations show that the number, the mass, and the spatial distribution of the fragments depend strongly on which of the main competitors of gravity is dominant. The main physical mechanisms that oppose gravity during collapse are intrinsic turbulence, radiation feedback, and magnetic pressure (e.g. Krumholz 2006; Hennebelle et al. 2011). Feedback from nascent protostellar objects through outflows, winds, and/or expansion of ionised regions (especially from newly born massive objects) can be important in relatively evolved stages (Bate 2009), but even then seems to be of only secondary importance (Palau et al. 2013).

In a purely gravo-turbulent scenario, the collapsing clump should fragment into many cores, the number of which is comparable to the total mass divided by the Jeans mass (Dobbs et al. 2005); on the other hand, fragmentation can be suppressed by temperature enhancement that is due to the gravitational energy radiated away from the densest portion of the clump that collapses first (Krumholz 2006), or by magnetic support (Hennebelle et al. 2011). Commerçon et al. (2011) have shown that models with strong magnetic support predict fragments more massive and less numerous than those predicted by the models with weak magnetic support. The crucial parameter in their 3D simulations is μ = (M/ Φ)/(M/ Φ)crit, where (M/ Φ) is the ratio between total mass and magnetic flux, and the critical value (M/ Φ)crit, that is, the ratio at which gravity is balanced by the magnetic field (thus, for (M/ Φ)crit> 1 the magnetic field cannot prevent gravitational collapse), is given by theory (Mouschovias & Spitzer 1976). The outcome of the simulations also depends on other initial global parameters of the clump, such as gas temperature, angular momentum, total mass, and average volume density. Once these parameters are fixed, however, the final population of cores shows a strong variation with μ.

Studies of the fragmentation level in massive clumps at the earliest stages of the gravitational collapse remain limited so far. These investigations are challenging for several reasons: pristine, massive clumps are rare and typically located at distances larger than 1 kpc, hence reaching the linear resolution required for a consistent comparison with the simulations (about 1000 AU) requires observations with sub-arcsecond angular resolution. Furthermore, the low mass of the fragments expected in the simulations (fractions of M) requires extremely high sensitivities. In general, the few studies performed so far with sub-arcsecond angular resolution, or close to ~ 1′′, reveal either low fragmentation (e.g. Palau et al. 2013; Longmore et al. 2011), or many fragments that are too massive, however, to be consistent with the gravo-turbulent scenario (Bontemps et al. 2010; Zhang et al. 2015). Furthermore, comparisons with models that assume the actual physical conditions (temperature, turbulence) of the collapsing parent clump have not been published yet.

In this letter, we report on the population of fragments derived in the image of the dust thermal continuum emission at ~ 278 GHz obtained with the Atacama Large Millimeter Array (ALMA) towards the source IRAS 16061–5048c1, hereafter I16061c1, a massive (M ~ 280M, Beltrán et al. 2006; Giannetti et al. 2013) and dense (column density of H2, N(H2) ~ 1.6 × 1023 cm-2) molecular clump located at 3.6 kpc (Fontani et al. 2005). The clump was detected at 1.2 mm at low angular resolution with the Swedish-ESO Submillimeter Telescope (SEST, panel A of Fig. 1, Beltrán et al. 2006), and found to be not blended with nearby millimeter clumps, which allows a clear identification of the fragments. Its high mass and column density make it a potential site for the formation of massive stars and rich clusters, according to observational findings (Kauffmann & Pillai 2010; Lopez-Sepulcre et al. 2010). The clump was classified as an infrared dark cloud because it was undetected in the images of the Midcourse Space Experiment (MSX) infrared satellite, although more sensitive images of the Spitzer satellite revealed infrared emission at a wavelength of 24 μm (panel A in Fig. 1). Nevertheless, several observational results indicate that the possibly embedded star formation activity is at a very early stage (Sanchez-Monge et al. 2013). In particular, the depletion factor of CO (ratio between expected and observed abundance of CO) is 12. This provides strong evidence for the chemical youth of the clump, because the cause of depletion factors of CO larger than unity is the freeze-out of this molecule onto dust grains, a mechanism efficient only in cold and dense pre-stellar and young protostellar cores (Caselli et al. 1999; Emprechtinger et al. 2009; Fontani et al. 2012). The observations and data reduction procedures are presented in Sect. 2. Our results are shown in Sect. 3 and discussed in Sect. 4.

thumbnail Fig. 1

Panel A): dust continuum emission map (dashed contours) obtained with the SEST telescope with an angular resolution of 24′′ at 1.2 mm towards I16061c1 (Beltrán et al. 2006). The map is superimposed on the Spitzer-MIPS image at 24 μm (in units of MJy/sr). The circle indicates the ALMA primary beam at 278 GHz (~ 24′′). Panel B): enlargement of the rectangular region indicated in panel A), showing the contour map of the thermal dust continuum emission at frequency 278 GHz detected with ALMA, in flux density units. The first contour level and the spacing between two adjacent contours both correspond to the 3σ rms of the image (0.54 mJy/beam). The cross marks the phase centre. The ellipse in the bottom left corner shows the synthesized beam, and corresponds to 0.36′′×0.18′′ (Position Angle = 86°). The numbers indicate the twelve identified fragments (see Sect. 3). Panel C): simulations of the thermal dust emission at 278 GHz predicted by the models of Commerçon et al. (2011), which reproduce the gravitational collapse of a 300 M clump in case of strong magnetic support (μ = 2), obtained at time t2 (see text), projected on a plane perpendicular to the direction of the magnetic field. Panel D): same as panel C) for the case μ = 200 (weak magnetic support). Panel E): synthetic ALMA images of the models presented in panel C). The contours correspond to 0.54, 1.2, 2, 5, 10, 30, and 50 mJy/beam. Panel F) same as panel E) for the case μ = 200 at time t200 (weak magnetic support).

2. Observations and data reduction

Observations of I16061c1 with the ALMA array were performed during June, 2015. The array was in configuration C36-6, with maximum baseline of 1091 m. The phase centre was at RA (J2000): 16h10m06.′′61 and Dec (J2000): −50°50′29′′. The total integration time on source was ~ 18 min. The precipitable water vapour during observations was ~ 1.8 mm. Bandpass and phases were calibrated by observing J14274206 and J16175848, respectively. The absolute flux scale was set through observations of Titan and Ceres. From Beltrán et al. (2006), we know that the total flux measured with the single-dish in an area corresponding to the ALMA primary beam at the observing frequency (24′′) is ~ 2.3 Jy, while the total flux measured with ALMA in the same area is 0.63 Jy. This means that we recover ~ 30% of the total flux. The remaining ~ 70% is likely contained in an extended envelope that is resolved out. Continuum was extracted by averaging in frequency the line-free channels. The total bandwidth used is ~ 1703 MHz. Calibration and imaging was performed with the CASA1 software (McMullin et al. 2007), and the final images were analysed following standard procedures with the software MAPPING of the GILDAS2 package. The angular resolution of the final image is ~ 0.25′′ (i.e. ~ 900 AU at the source distance). We were sensitive to point-like fragments of 0.06 M. Together with the continuum, we detected several lines, among which N2H+(3–2). These data will be presented and discussed in a forthcoming paper. In this letter, we only use the N2H+ (32) line to derive the virial masses, as we show in Sect. 3.

3. Results

The ALMA map of the dust thermal continuum emission is shown in Fig. 1B: we have detected several dense condensations distributed in a filamentary-like structure extended east-west, surrounded by fainter extended emission. This structure has been decomposed into twelve fragments (Fig. 1B). The fragments were identified following these criteria: (1) peak intensity greater than five times the noise level; (2) two partially overlapping fragments are considered separately if they are separate at their half-peak intensity level. The minimum threshold of five times the noise was adopted because some peaks at the edge of the primary beam are comparable to about four to five times the noise level. We decided to use these criteria and decompose the map into cores by eye instead of using decomposition algorithms (such as Clumpfind) because small changes in their input parameters could lead to large changes in the number of identified clumps (Pineda et al. 2009). The main physical properties of the fragments derived from the continuum map, that is, integrated and peak flux, size, and gas mass, and the methods used to derive them, are described in Appendix A. The derived parameters are listed in Table A.1. The mean mass of the fragments is 4.4 M, with a lowest value of 0.7 M and a highest value of ~ 9M. The diameters (undeconvolved for the beam) range from 0.011 to 0.032 pc, with a mean value of 0.025 pc.

To investigate the stability of the fragments, we calculated the virial masses Mvir, that is, the masses required for the cores to be in virial equilibrium, from the line widths observed in N2H+ (32). As stated in Sect. 2, we here used this molecular transition only for the purpose to derive the level of turbulence (the key ingredient of the models, together with the magnetic support) of the dense gas out of which the fragments are formed. The approach used to derive Mvir is described in Appendix A and the values obtained are reported in Table A.1. The average ratio between Mvir and M computed from the continuum emission is about 0.4, indicating that the gravity dominates, according to other ALMA studies of fragmentation (Zhang et al. 2015). However, the uncertainties due to the dust mass opacity coefficient (see Eq. (A.1)) can be of a factor 23, hence it is difficult to conclude that the fragments are unstable. Moreover, the formula of the virial mass we used does not consider the magnetic support. Because this latter is expected to be relevant, it is likely that the fragments are closer to virial equilibrium and would not tend to fragment further. If one assumes, for instance, the value of 0.27 mG measured by Pillai et al. (2015) in another infrared-dark cloud, the ratio between virial mass and gas mass would become about 1, and the fragments would be marginally stable. A similar conclusion is given in Tan et al. (2013), where the dynamics of four infrared-dark clouds similar to I16061c1 is studied.

4. Discussion and conclusion

We have simulated the gravitational collapse of I16061c1 through 3D numerical simulations following Commerçon et al. (2011), adopting a mass, temperature, average density, and level of turbulence of the parent clump very similar to those measured (Beltrán et al. 2006; Giannetti et al. 2013). In particular, the Mach number setting the initial turbulence was derived from the line width of C18O (32) by Fontani et al. (2012). Because these observations were obtained with angular resolution of ~ 24′′ and the critical density of the line (~ 5 × 104 cm-3, Fontani et al. 2005) is comparable to the average density of the clump as a whole (Beltrán et al. 2006), the C18O line width represents a reasonable estimate of the intrinsic turbulence of the parent clump. The models were run for μ = 2 (strongly magnetised case) and μ = 200 (weakly magnetised case). Then, we post-processed the simulations data and computed the dust emission maps at 278 GHz: the final maps obtained in flux density units at the distance of the source were imaged with the CASA software to reproduce synthetic images with the same observational parameters as those of the observations. A detailed description of the parameters used for the numerical simulations, of the resulting maps, and how they were post-processed is given in Appendix B. Further descriptions of the models can also be found in Commerçon et al. (2011). To investigate possible effects of geometry, we imaged the outcome of the simulations projected on three planes: (x, y), (x, z), and (y, z), where x is the direction of the initial magnetic field. As an example, in Figs. 1C and D we show the results for the cases of strong and weak magnetic support, respectively, projected on the (y, z) plane, that is, on a direction perpendicular to the magnetic field. The synthetic images obtained with CASA are shown in panels E and F. All the planes for μ = 2 and μ = 200 are shown in Appendix B, in Figs. B.1 and B.2, respectively. An important result of the simulations (see Fig. B.3 in Appendix B) is that the total flux seen by the interferometer in the μ = 2 case decreases until about 35 × 103 yr and then goes through a minimum and gradually starts to increase. In the μ = 200 case, by contrast, the decrease is not reversed. We conclude from this that in the μ = 2 case, the fragments continue to accrete material and eventually will reach the total flux observed in the ALMA image. Thus, in the μ = 2 case we analysed the synthetic images produced at the time at which the total flux in the fragments matches the observed value within an uncertainty of about 10% (the calibration uncertainty on the flux density, see the ALMA Technical Handbook3), while for the μ = 200 case we analysed the synthetic images obtained at the end of the simulations. This corresponds to two different times: t2 = 48 500 yr after the birth of the first protostar for μ = 2; t200 = 59 500 yr after the birth of the first protostar for μ = 200.

thumbnail Fig. 2

Top panels: histograms showing the distribution of the peak fluxes (Fpeak) of the fragments identified in the ALMA image of I16061c1 (black), and in the synthetic images for μ = 2 (green, left) and μ = 200 (blue, right). Bottom panels: empirical cumulative distribution function (ECDF) of the quantities plotted in the top panels. The black line corresponds to the ALMA data; the green and blue lines indicate the strong and weak field cases, respectively, projected on the three planes. In all panels, the different line style indicates the projection plane: solid = (x, y); dot-dashed = (x, z); dashed = (y, z). The vertical dotted line corresponds to 0.8 mJy, which is approximately five times the rms noise level in both the real and synthetic maps. Note that the μ = 2 model spans the observations, while the μ = 200 model is strongly biased towards fragments with masses lower than those observed.

The synthetic maps with μ = 200 show more fragments with lower peak fluxes, and the overall structure is more chaotic and never filamentary, independently of the projection plane. The fragments were identified and their properties in the synthetic images derived following the same criteria and procedures as those used for the ALMA data. Therefore, any systematic error introduced by the assumptions made (e.g. the assumed dust temperature, gas-to-dust ratio, dust grain emissivity) are the same in the real and synthetic images and consequently do not affect the comparison. The statistical properties of the synthetic core populations are summarised in Table B.1 of Appendix B. We also compared the cumulative distribution of the peak fluxes of the fragments in the observed and synthetic images. The results are shown in Fig. 2. The case with μ = 200 has lower peak values for the whole populations, while one or two fragments have a higher peak value than the maximum observed. The μ = 2 case has a broader distribution of values. Overall, the ALMA map shows a narrower distribution of peak fluxes, with a deficit of very weak and very strong peaks, which in turn are present in the two synthetic images. However, the μ = 2 model roughly spans the observations, while the μ = 200 model is heavily biased below the data. In addition, a non-parametric statistical test (Anderson-Darling test) implies that all the μ = 200 cases can be excluded as being drawn from the same parent distribution as the observed values with a confidence level exceeding 99.8%. The μ = 2 case is less obvious because two projections could be excluded at a 9899% confidence level, while the third projection, (y, z), with a null hypothesis probability of ~ 90% cannot be excluded at the 2σ level. The deficit of very strong and very weak peaks in the real image may be due to a difference between the μ values assumed in the simulations and the real one, or to some other unknown (or doubtful) initial assumption such as the density profile or the homogeneous temperature of the collapsing clump.

Based on the overall morphologies shown in Fig. 1 (and in Figs. B.1 and B.2) and on the statistical properties of the fragments reported in Fig. 2, the model that better reproduces the

data clearly is the one with μ = 2. Hence, with these new ALMA observations, compared with realistic 3D simulations that assume as initial conditions the properties of the parent clump, we demonstrate that the fragmentation due to self-gravity is dominated by the magnetic support, based on the evidence that (1) the overall morphology of the fragmenting region is filamentary, and this is predicted only in case of a dominant magnetic support; (2) the observed fragment mass distribution is most easily understood in simulations assuming substantial magnetic support.


1

The Common Astronomy Software Applications (CASA) software can be downloaded at http://casa.nrao.edu

Acknowledgments

This paper makes use of the following ALMA data: ADS/JAO.ALMA.2012.1.00366.S. ALMA is a partnership of ESO (representing its member states), NSF (USA) and NINS (Japan), together with NRC (Canada), NSC and ASIAA (Taiwan), and KASI (Republic of Korea), in cooperation with the Republic of Chile. The Joint ALMA Observatory is operated by ESO, AUI/NRAO and NAOJ We acknowledge the Italian-ARC node for their help in the reduction of the data. We acknowledge partial support from Italian Ministero dell’Istruzione, Università e Ricerca through the grant Progetti Premiali 2012 iALMA (CUP C52I13000140001) and from Gothenburg Centre of Advanced Studies in Science and Technology through the program Origins of habitable planets.

References

  1. Bate, M. R. 2009, MNRAS, 392, 1363 [NASA ADS] [CrossRef] [Google Scholar]
  2. Beltrán, M. T., Brand, J., Cesaroni, R., et al. 2006, A&A, 447, 221 [NASA ADS] [CrossRef] [EDP Sciences] [MathSciNet] [Google Scholar]
  3. Beuther, H., Schilke, P., Sridharan, T. K., et al. 2002, A&A, 566, 945 [Google Scholar]
  4. Bleuler, A., & Teyssier, R. 2014, MNRAS, 445, 4015 [NASA ADS] [CrossRef] [Google Scholar]
  5. Bonnell, I. A., Vine, S. G., & Bate, M. R. 2004, MNRAS, 349, 735 [NASA ADS] [CrossRef] [Google Scholar]
  6. Bontemps, S., Motte, F., Csengeri, T., & Schneider, N. 2010, A&A, 524, A18 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  7. Caselli, P., Walmsley, C. M., Tafalla, M., Dore, L., & Myers, P. 1999, ApJ, 523, L165 [NASA ADS] [CrossRef] [Google Scholar]
  8. Commerçon, B., Hennebelle, P., & Henning, T. 2011, ApJ, 742, L9 [NASA ADS] [CrossRef] [Google Scholar]
  9. Commerçon, B., Launhardt, R., Dullemond, C., & Henning, Th. 2012, A&A, 545, A98 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  10. Commerçon, B., Debout, V., & Teyssier, R. 2014, A&A, 563, A11 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  11. Crutcher, R. M. 2013, ARA&A, 50, 29 [Google Scholar]
  12. Dobbs, C. L., Bonnell, I. A., & Clark, P. C. 2005, MNRAS, 360, 2 [NASA ADS] [CrossRef] [MathSciNet] [Google Scholar]
  13. Emprechtinger, M., Caselli, P., Volgenau, N. H., Stutzki, J., & Wiedner, M.C. 2009, A&A, 493, 89 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  14. Fontani, F., Beltrán, M. T., Brand, J., et al. 2005, A&A, 432, 921 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  15. Fontani, F., Giannetti, A., Beltrán, M. T., et al. 2012, MNRAS, 423, 2342 [NASA ADS] [CrossRef] [Google Scholar]
  16. Fromang, S., Hennebelle, P., & Teyssier, R. 2006, A&A, 457, 371 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  17. Giannetti, A., Brand, J., Sanchez-Monge, Á., et al. 2013, A&A, 556, A16 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  18. Hennebelle, P., Commerçon, B., Joos, M., et al. 2011, A&A, 528, A72 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  19. Kauffmann, J., & Pillai, T. 2010, ApJ, 723, L7 [NASA ADS] [CrossRef] [Google Scholar]
  20. Krumholz, M. R. 2006, ApJ, 641, L45 [NASA ADS] [CrossRef] [Google Scholar]
  21. Krumholz, M. R., Klein, R., McKee, C. F., Offner, S. S. R., & Cunningham, A. J. A. 2009, Science, 323, 754 [NASA ADS] [CrossRef] [PubMed] [Google Scholar]
  22. Longmore, S. N., Pillai, T., Keto, E., Zhang, Q., & Qiu, K. 2011, ApJ, 726, L97 [NASA ADS] [CrossRef] [Google Scholar]
  23. Lopez-Sepulcre, A., Cesaroni, R., & Walmsley, C. M. 2010, A&A, 517, A66 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  24. Maret, S., Hily-Blant, P., Pety, J., Bardeau, S., & Reynier, E. 2011, A&A, 526, A47 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  25. McKee, C., & Tan, J. C. 2003, ApJ, 585, 850 [NASA ADS] [CrossRef] [MathSciNet] [Google Scholar]
  26. McMullin, J. P., Waters, B., Schiebel, D., Young, W., & Golap, K. 2007, in Astronomical Data Analysis Software and Systems XVI, eds. R. A. Shaw, F. Hill, & D. J. Bell, ASP Conf. Ser., 376, 127 [Google Scholar]
  27. Mouschovias, T. C., & Spitzer, L. J. 1976 , ApJ, 210, 326 [Google Scholar]
  28. Ossenkopf, V., & Henning, T. 1994, A&A, 291, 943 [NASA ADS] [Google Scholar]
  29. Palau, A., Fuente, A., Girart, J. M., et al. 2013, ApJ, 762, 120 [NASA ADS] [CrossRef] [Google Scholar]
  30. Pillai, T., Kauffmann, J., Tan, J. C., et al. 2015, ApJ, 799, 74 [NASA ADS] [CrossRef] [Google Scholar]
  31. Pineda, J. E., Rosolowsky, E. W., & Goodman, A. A. 2009, ApJ, 699, L134 [NASA ADS] [CrossRef] [Google Scholar]
  32. Sanchez-Monge, Á, Beltrán, M. T., Cesaroni, et al. 2013, A&A, 550, A21 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  33. Tan, J. C., Kong, S., Butler, M. J., Caselli, P., & Fontani, F. 2013, ApJ, 779, 96 [NASA ADS] [CrossRef] [Google Scholar]
  34. Teyssier, R. 2002, A&A, 385, 337 [NASA ADS] [CrossRef] [EDP Sciences] [Google Scholar]
  35. Weiss, A., Hillebrandt, W., Thomas, H.-C., & Ritter, H. 2005, Book review: Cox and Giuli’s Principles of Stellar Structure (Cambridge, UK: Princeton Publishing Associates Ltd) [Google Scholar]
  36. Zhang, Q., Wang, K., Xing, L., & Jiménez-Serra, I. 2015, ApJ, 804, 141 [NASA ADS] [CrossRef] [Google Scholar]

Appendix A: Physical properties of the fragments

Appendix A.1: Derivation of the parameters

  • Integrated flux densities: the integrated flux densities of the fragments, Sν, were obtained from the 3σ rms contour in the continuum image. In the few cases for which the 3σ rms contours of two adjacent fragments are partly overlapping (e.g. fragments 5, 6, and 7 in Fig. 1), the edges between the two have been defined by eye at approximately half of the separation between the peaks. The results are shown in Table A.1.

  • Gas masses: the gas mass of each fragment was calculated from the equation M=gSνd2κνBν(Td),\appendix \setcounter{section}{1} \begin{equation} M=\frac{g S_{\nu} d^2}{\kappa_{\nu}B_{\nu}(T_{\rm d})} , \label{mass_dust} \end{equation}(A.1)where Sν is the integrated flux density, d is the distance to the source, κν is the dust mass opacity coefficient, g is the gas-to-dust ratio (assumed to be 100), and Bν(Td) is the Planck function for a black body of temperature Td. We adopted Td = 25 K, corresponding to the gas temperature derived by Giannetti et al. (2013), assuming coupling between gas and dust (reasonable assumption at the high average density of the clump). The dust mass opacity coefficient was derived from the equation κν = κν0(ν/ν0)β. We assumed β = 2 and κν0 = 0.899 cm-2 gr-1 at ν0 = 230 GHz, according to Ossenkopf & Henning (1994). The highest mass derived is ~ 9M, the lowest is ~ 0.7M (see Table A.1).

  • Size: the size of each fragment was estimated as the diameter of the circle with an area equivalent to that encompassed by the 3σ rms contour level. The results are shown in Table A.1. The ALMA beam size is much smaller than the size of the fragments, so that deconvolution for the beam is irrelevant to derive the source size.

  • Virial masses: the virial masses were derived in this way: first, we extracted the N2H+ (32) spectra from the 3σ rms level of the 12 continuum cores. All the spectra were fitted in an automatic way using a procedure based on the integration of the python module PyMC and the CLASS extension WEEDS (Maret et al. 2011). Then, the virial masses, Mvir, were computed from the formula Mvir=210rΔv2M,\appendix \setcounter{section}{1} \begin{equation} M_{\rm vir} = 210 r \Delta v^{2}~M_\odot , \end{equation}(A.2)where r is the size of the fragment, and Δv is the line width at half maximum of the average N2H+ (3–2) spectrum obtained from the fitting procedure described above. The results are shown in Table A.1.

Table A.1

Peak position (in RA and Dec J2000), integrated flux (inside the 3σ rms contour level), peak flux, diameter, mass, line width at half maximum, and virial mass of the 12 fragments identified in Fig. 1B.

Appendix B: Simulations and synthetic images

Appendix B.1: Methods and initial conditions for the numerical calculations

We performed a set of two radiation-magneto-hydrodynamics calculations that includes the radiative feedback from the accreting protostars. We used the RAMSES code with the grey flux-limited-diffusion approximation for radiative transfer and the ideal magnetohydrodynamics (MHD) for magnetic fields (Commerçon et al. 2012, 2014; Teyssier 2002; Fromang et al. 2006). The initial conditions are similar to those used in Hennebelle et al. (2011) and Commerçon et al. (2011), with slight modifications to match roughly the observed properties of I16061c1. We note that the models presented in this Letter were made with initial conditions very similar to those measured from previous observations in I16061c1to perform an appropriate comparison with observations for this specific source. Our aim was not to fine-tune the initial conditions such that the models best reproduce the observations. We considered an isolated spherical core of mass 300M, radius 0.25 pc, and temperature 20 K. We assumed a Plummer-like initial density profile ρ(r) = ρc/ (1 + (r/r0)2), with ρc = 3.96 × 105 cm-3 and r0 = 0.085 pc, and a factor 10 for the density contrast between the centre and the border of the core. This density profile is suggested by observational findings (Beuther et al. 2002). The initial magnetic field was aligned with the x-axis and its intensity was proportional to the column density through the cloud (Hennebelle et al. 2011). We here investigated two degrees of magnetization, μ = 2, which is close to the values 23 that are observationally inferred (e.g. Crutcher 2012), and μ = 200, which corresponds to a quasi-hydrodynamical case. Last, we applied an initial internal turbulent velocity field to the cores. The velocity field was obtained by imposing a Kolmogorov power spectrum with randomly determined phases (i.e. a ratio 2:1 between the solenoidal and the compressive modes). There is no global rotation of the cloud, meaning that the angular momentum is contained within the initial turbulent motions, which are then amplified by the gravitational collapse. The amplitude of the velocity dispersion was scaled to match a turbulent Mach number of 6.44, in agreement with C18O observations (Fontani et al. 2012). Following Hennebelle et al. (2011, Eq. (2) therein), the virial parameter was αvir ~ 0.72 for μ = 2, and αvir ~ 0.54 for μ = 200 (close to virial equilibrium in both cases). The two calculations, μ = 2 and μ = 200, started with the same initial turbulent velocity field (only one realisation was explored) and turbulence was not maintained during the collapse. Investigation of the effect of different initial turbulent seeds is beyond the scope of this Letter. The computational box had a 2563 resolution, and the grid was refined according to the local Jeans length (at least 8 cells/Jeans length) down to seven levels of refinement (minimum cell size of 13 AU). Below 13 AU, the collapsing gas was described using sub-grid models attached to sink particles, similar to what was done in other studies (Krumholz et al. 2009). We used the sink particle method presented in Bleuler et al. (2014), although with slight modifications on the checks performed for the sink creation. The sink particles accrete the gas that is located in their accretion volumes (sphere of radius ~ 52 AU, 4 cells) and that is Jeans unstable. We considered that half of the mass accreted onto the sink particles becomes stellar material. The luminosity of the protostars was then computed using mass-radius and mass-luminosity empirical relations of main-sequence stars (e.g. Weiss et al. 2005) and was injected within the accretion volume in the computational domain as a source term (e.g. Krumholz et al. 2009). We did not account for accretion luminosity.

Appendix B.2: Outcomes of the numerical calculations

We ran the calculations until they reached a star formation efficiency (SFE) > 20% (where the star formation efficiency corresponds to the ratio between the mass of the gas accreted onto the sink particles and the total mass of the cloud). Again, the choice of the times at which we stopped the calculations was not aimed at best reproducing the observed values. Model μ = 2 is post-processed at time t2 = 48 500 yr after the birth of the first protostar, which is the time at which the total flux in fragments is equal to the observed value (within the uncertainty), and μ = 200 at time t200 = 59 500 yr. At these times, model μ = 2 has formed 38 sink particles (for a total mass of 60 M), while model μ = 200 has formed 119 sink particles (for a total mass of 85 M). Figure B.3 shows the time evolution after the first sink creation of the SFE, the number of sinks, and the total flux at 278 GHz (within a total area of 80 000 AU × 80 000 AU) for the two models. The circles indicate the time at which the simulations are post-processed. We note the increase in the 278 GHz flux with time for μ = 2, which probably reflects the temperature increase caused by the radiation of the sink particles.

Appendix B.3: Production of the synthetic images

We first post-processed the RAMSES calculation results using the radiative transfer code RADMC-3D4 and the interface presented in Commerçon et al. (2012). We produced dust emission maps at 278 GHz (see Figs. B.1 and B.2). We did not account for the stellar luminosities in the synthetic images since the

stellar irradiation is reprocessed in the envelope at millimeter wavelengths. However, we attempted to create models accounting for protostellar luminosities, and found results that do not change significantly at the wavelength considered. The ALMA synthetic images of the numerical simulations were then produced through the CASA software: first, synthetic visibilities were created with the task simobserve, which were then imaged with the task simanalyze. To precisely reproduce the observations, we used the same parameters in the tasks as in the observations: integration time on source of 18 min, precipitable water vapour of about 1.8 mm, array configuration C36-6, start hour angle of 2.4 h (see Sect. 2). The population of fragments in the final synthetic images were derived following the same procedure as described in Sect. 4.

thumbnail Fig. B.1

Top panels: show the thermal dust continuum emission map at frequency 278 GHz predicted by the models of Commerçon et al. (2011), which reproduce the gravitational collapse of a 300 M clump in case of strong magnetic support (μ = 2) at time t2 = 48 500 yr after the birth of the first protostar (see main text for details). In the bottom panels, we show the models after processing in the CASA simulator, adopting the same observational conditions as for the real observations. Units of the colour-scale are Jansky/beam. Contour levels are 0.6, 1, 5, 10, 30, and 50 mJy beam-1 in all bottom panels.

thumbnail Fig. B.2

Same as Fig. B.1 for the case μ = 200 at time t200 = 59 500 yr after the birth of the first protostar (see main text for details).

thumbnail Fig. B.3

From top to bottom: evolution with time of the number of sink particles, of the SFE, and of the total flux emission at 278 GHz (within a total area of 80 000 AU × 80 000 AU) for the two models after the creation of the first sink. The circles indicate the time at which the simulations are post-processed. In the bottom panel, the different lines correspond to the different projection planes as illustrated in the bottom right corner.

Table B.1

Statistical comparison between the fragment population derived from the ALMA image of I16061c1 shown in Fig. 1 and the simulations presented in Figs. B1 and B2 of the Appendix.

All Tables

Table A.1

Peak position (in RA and Dec J2000), integrated flux (inside the 3σ rms contour level), peak flux, diameter, mass, line width at half maximum, and virial mass of the 12 fragments identified in Fig. 1B.

Table B.1

Statistical comparison between the fragment population derived from the ALMA image of I16061c1 shown in Fig. 1 and the simulations presented in Figs. B1 and B2 of the Appendix.

All Figures

thumbnail Fig. 1

Panel A): dust continuum emission map (dashed contours) obtained with the SEST telescope with an angular resolution of 24′′ at 1.2 mm towards I16061c1 (Beltrán et al. 2006). The map is superimposed on the Spitzer-MIPS image at 24 μm (in units of MJy/sr). The circle indicates the ALMA primary beam at 278 GHz (~ 24′′). Panel B): enlargement of the rectangular region indicated in panel A), showing the contour map of the thermal dust continuum emission at frequency 278 GHz detected with ALMA, in flux density units. The first contour level and the spacing between two adjacent contours both correspond to the 3σ rms of the image (0.54 mJy/beam). The cross marks the phase centre. The ellipse in the bottom left corner shows the synthesized beam, and corresponds to 0.36′′×0.18′′ (Position Angle = 86°). The numbers indicate the twelve identified fragments (see Sect. 3). Panel C): simulations of the thermal dust emission at 278 GHz predicted by the models of Commerçon et al. (2011), which reproduce the gravitational collapse of a 300 M clump in case of strong magnetic support (μ = 2), obtained at time t2 (see text), projected on a plane perpendicular to the direction of the magnetic field. Panel D): same as panel C) for the case μ = 200 (weak magnetic support). Panel E): synthetic ALMA images of the models presented in panel C). The contours correspond to 0.54, 1.2, 2, 5, 10, 30, and 50 mJy/beam. Panel F) same as panel E) for the case μ = 200 at time t200 (weak magnetic support).

In the text
thumbnail Fig. 2

Top panels: histograms showing the distribution of the peak fluxes (Fpeak) of the fragments identified in the ALMA image of I16061c1 (black), and in the synthetic images for μ = 2 (green, left) and μ = 200 (blue, right). Bottom panels: empirical cumulative distribution function (ECDF) of the quantities plotted in the top panels. The black line corresponds to the ALMA data; the green and blue lines indicate the strong and weak field cases, respectively, projected on the three planes. In all panels, the different line style indicates the projection plane: solid = (x, y); dot-dashed = (x, z); dashed = (y, z). The vertical dotted line corresponds to 0.8 mJy, which is approximately five times the rms noise level in both the real and synthetic maps. Note that the μ = 2 model spans the observations, while the μ = 200 model is strongly biased towards fragments with masses lower than those observed.

In the text
thumbnail Fig. B.1

Top panels: show the thermal dust continuum emission map at frequency 278 GHz predicted by the models of Commerçon et al. (2011), which reproduce the gravitational collapse of a 300 M clump in case of strong magnetic support (μ = 2) at time t2 = 48 500 yr after the birth of the first protostar (see main text for details). In the bottom panels, we show the models after processing in the CASA simulator, adopting the same observational conditions as for the real observations. Units of the colour-scale are Jansky/beam. Contour levels are 0.6, 1, 5, 10, 30, and 50 mJy beam-1 in all bottom panels.

In the text
thumbnail Fig. B.2

Same as Fig. B.1 for the case μ = 200 at time t200 = 59 500 yr after the birth of the first protostar (see main text for details).

In the text
thumbnail Fig. B.3

From top to bottom: evolution with time of the number of sink particles, of the SFE, and of the total flux emission at 278 GHz (within a total area of 80 000 AU × 80 000 AU) for the two models after the creation of the first sink. The circles indicate the time at which the simulations are post-processed. In the bottom panel, the different lines correspond to the different projection planes as illustrated in the bottom right corner.

In the text

Current usage metrics show cumulative count of Article Views (full-text article views including HTML views, PDF and ePub downloads, according to the available data) and Abstracts Views on Vision4Press platform.

Data correspond to usage on the plateform after 2015. The current usage metrics is available 48-96 hours after online publication and is updated daily on week days.

Initial download of the metrics may take a while.