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==Limiting Pressure and Maximum Mass== No matter how you look at the bounded isothermal sphere sequence — whether plotted as a curve in Bonnor's P-V diagram or as a curve in Whitworth's R-P diagram — it is clear that, for a given choice of the sound speed and the mass, there is a value of the pressure above which no equilibrium configuration exists. (Alternatively, for a given sound speed and external pressure, there is a limiting mass above which no equilibrium configuration exists; see below.) The configuration identifying this limiting pressure resides at the position along Bonnor's P-V diagram sequence where <math>~dP_e/dV</math> — or, in Whitworth's discussion, <math>~dP_e/dR</math> — first goes to zero. ===Following Bonnor's Presentation=== As is shown in his equation (3.1), [http://adsabs.harvard.edu/abs/1956MNRAS.116..351B Bonnor (1956)] determined that, at a fixed mass and sound speed, <math>~dP/dV</math> goes to zero when, <div align="center"> <math>~1-\frac{1}{2} e^{\psi} \biggl( \frac{d\psi}{d\xi}\biggr)^2 = 0 \, .</math> </div> In the following figure, the function defined by the left-hand-side of this expression is plotted versus <math>~\ln\xi</math> using [[SSC/Structure/IsothermalSphere#Emden.27s_Numerical_Solution|Emden's (1907) tabulated data]]. As Bonnor noted, the function first crosses zero when <math>~\xi \approx 6.5</math> <math>~(\ln\xi = 1.87)</math>. <div align="center"> <table border="1"> <tr> <td align="center"> [[File:Bonnor1956DPDVplot.jpg|400px|center|Bonnor (1956, MNRAS, 116, 351)]] </td> </tr> </table> </div> An isothermal sphere that is truncated at this location will have a radius, <div align="center"> <math> R = \biggl( \frac{c_s^2}{G\rho_c} \biggr)^{1/2} \frac{6.5}{\sqrt{4\pi}} = 1.83 \biggl( \frac{c_s^2}{G\rho_c} \biggr)^{1/2} \, , </math> </div> which matches equation (3.3) of [http://adsabs.harvard.edu/abs/1956MNRAS.116..351B Bonnor (1956)]; and, drawing on function values provided in [[SSC/Structure/IsothermalSphere#Emden.27s_Numerical_Solution|Emden's (1907) Table 14]], it will have a total mass, <div align="center"> <math>~M_R = \biggl( \frac{c_s^6}{4\pi G^3 \rho_c} \biggr)^{1/2} \biggl[\xi^2 \frac{d\psi}{d\xi} \biggr]_e \approx \biggl( \frac{c_s^6}{G^3 \rho_c} \biggr)^{1/2} \biggl[ \frac{(14.353+17.214)/2}{\sqrt{4\pi}} \biggr] = 4.45 \biggl( \frac{c_s^6}{G^3 \rho_c} \biggr)^{1/2}\, .</math> </div> Dividing this expression for <math>~M_R</math> by the expression for <math>~R</math> gives, <div align="center"> <math> \frac{M_R}{R} = 2.43 \biggl( \frac{c_s^2}{G} \biggr) \, , </math> </div> which matches equation (3.6) of [http://adsabs.harvard.edu/abs/1956MNRAS.116..351B Bonnor (1956)]. In order to maintain an equilibrium structure while truncating the isothermal model at this radius requires applying an external pressure of the following magnitude: <div align="center"> <math>P_e = c_s^2 \rho_c e^{-\psi} \approx c_s^2 \rho_c (0.08493 + 0.05833)/2 = 0.0716~ c_s^2 \rho_c \, ,</math> </div> where, again, numerical values have been drawn from [[SSC/Structure/IsothermalSphere#Emden.27s_Numerical_Solution|Emden's (1907) Table 14]]. <span id="cychenMaryland"> Finally, using this relation to eliminate <math>~\rho_c</math> from the expression for <math>~M_R</math> gives,</span> <div align="center"> <table border="0" cellpadding="5"> <tr> <td align="right"> <math>~M_R</math> </td> <td align="center">=</td> <td align="left"> <math>\biggl( \frac{c_s^8}{G^3 P_e} \biggr)^{1/2}\biggl[ \frac{1}{4\pi}\biggr]^{1/2} \biggl[\xi^2 e^{-\psi/2} \biggl(\frac{d\psi}{d\xi} \biggr) \biggr]_e</math> </td> </tr> <tr> <td align="center" colspan="3"><font color="red">On 3/2/2026, we changed the exponential from (incorrect) <math>e^{+\psi/2}</math> to (correct) <math>e^{-\psi/2}</math>.</font></td> </tr> <tr> <td align="right"> </td> <td align="center"><math>\approx</math></td> <td align="left"> <math> \biggl( \frac{c_s^8}{G^3 P_e} \biggr)^{1/2} \frac{1}{2\pi^{1/2}} \biggl\{ \frac{1}{2} \biggl[ 14.353 (0.08493)^{1/2} + 17.214 (0.05833)^{1/2} \biggr] \biggr\} </math> </td> </tr> <tr> <td align="right"> </td> <td align="center"><math>\approx</math></td> <td align="left"> <math> 1.18 \biggl( \frac{c_s^8}{G^3 P_e} \biggr)^{1/2} \, . </math> </td> </tr> </table> </div> This is the mass upper limit for a stable, pressure-bounded isothermal sphere — the so-called Bonnor-Ebert mass; see, for example, equation (1) of [http://adsabs.harvard.edu/abs/1977ApJ...214..488S Shu (1977)]. [[SSC/Structure/LimitingMasses#Bounded_Isothermal_Sphere_.26_Bonnor-Ebert_Mass|In a separate discussion]], we compare this result to the determinations of other related mass upper-limits. ===Ebert's Corresponding Presentation=== The expression derived by Bonnor for the ratio <math>~M_R/R</math> in the limiting configuration can be inverted to give, <div align="center"> <math> ~R \approx 0.41 \biggl( \frac{G M_R}{c_s^2} \biggr) \, . </math> </div> This matches the expression for the critical radius, <math>~R_\mathrm{kr}</math>, that appears as equation (23) in [http://adsabs.harvard.edu/abs/1955ZA.....37..217E Ebert's (1955) published derivation]. Similarly, the above relation that expresses the Bonnor-Ebert limiting mass in terms of <math>~c_s</math>, <math>~G</math>, and <math>~P_e</math> can be inverted to give, <div align="center"> <math> ~P_e \approx 4\pi (1.18)^2 \biggl( \frac{c_s^8}{4\pi G^3 M_R^2} \biggr) = 17.5 \biggl( \frac{c_s^8}{4\pi G^3 M_R^2} \biggr) \, , </math> </div> which agrees with the limiting pressure that was derived by [http://adsabs.harvard.edu/abs/1955ZA.....37..217E Ebert (1955)] and that is also presented in his equation (23).
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