Fig. 1.

Method for finding sonic points. Solutions are presented in terms of Mach number M (=v/a) vs log r plot. Θpin = 7.162 × 10−2 for all iterations. Panel a: iterations to obtain inner sonic point rci (black circle) and panel b: iterations to obtain outer sonic point rco (black star). Various branches plotted are multivalued branches (MB; green dashed-dot), transonic (TS; red dashed), and supersonic (SB; blue dashed-dot). Respective Θeins are mentioned inside the panels. Panel c: full set of transonic solutions. Global accretion solution (red solid) through rco and accretion solution through rci (red, dashed) is plotted. Equatorial global wind (through rco) and non-global wind (through rci) are represented using red dotted curve. The accretion disc flow parameters used are λ = 2.5, E = 1.000045, Ṁ = 0.001 ṀEdd, and MBH = 10 M⊙.
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