Docs @ 59d9431

Author: MFC Action

simulation/doxygen_crawl.html

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simulation/m__cbc_8fpp_8f90.html

@@ -323,6 +323,12 @@ <h2 class="memtitle"><span class="permalink"><a href="#a9771aa6ccf00c0970db70784
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+<p>gamma_method = 1: Ref. Section 2.3.1 Formulation of doi:10.7907/ZKW8-ES97.</p>
+<p>gamma_method = 2: c_p / c_v where c_p, c_v are specific heats.</p>
+<p>gamma_method = 1: Ref. Section 2.3.1 Formulation of doi:10.7907/ZKW8-ES97.</p>
+<p>gamma_method = 2: c_p / c_v where c_p, c_v are specific heats.</p>
+<p>gamma_method = 1: Ref. Section 2.3.1 Formulation of doi:10.7907/ZKW8-ES97.</p>
+<p>gamma_method = 2: c_p / c_v where c_p, c_v are specific heats.</p>
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simulation/m__compute__cbc_8fpp_8f90.html

@@ -149,15 +149,15 @@
 <tr class="memitem:a8bc20ac103228a5f5854c78781f9a3cc" id="r_a8bc20ac103228a5f5854c78781f9a3cc"><td class="memItemLeft" align="right" valign="top">subroutine, public&#160;</td><td class="memItemRight" valign="bottom"><a class="el" href="namespacem__compute__cbc.html#a8bc20ac103228a5f5854c78781f9a3cc">m_compute_cbc::s_compute_slip_wall_l</a> (lambda, <a class="el" href="m__rhs_8fpp_8f90.html#a2ac747380de0e6e5e11b01f4137fb75c">l</a>, <a class="el" href="m__rhs_8fpp_8f90.html#a1adc244ddf111bde5ae4e9ecc136e571">rho</a>, c, mf, dalpha_rho_ds, dpres_ds, dvel_ds, dadv_ds)</td></tr>
 <tr class="memdesc:a8bc20ac103228a5f5854c78781f9a3cc"><td class="mdescLeft">&#160;</td><td class="mdescRight">The L variables for the slip wall CBC, see pg. 451 of Thompson (1990). At the slip wall (frictionless wall), the normal component of velocity is zero at all times, while the transverse velocities may be nonzero.  <br /></td></tr>
 <tr class="separator:a8bc20ac103228a5f5854c78781f9a3cc"><td class="memSeparator" colspan="2">&#160;</td></tr>
-<tr class="memitem:a4413e05fc457a989abc1837a3e840fad" id="r_a4413e05fc457a989abc1837a3e840fad"><td class="memItemLeft" align="right" valign="top">subroutine, public&#160;</td><td class="memItemRight" valign="bottom"><a class="el" href="namespacem__compute__cbc.html#a4413e05fc457a989abc1837a3e840fad">m_compute_cbc::s_compute_nonreflecting_subsonic_buffer_l</a> (lambda, <a class="el" href="m__rhs_8fpp_8f90.html#a2ac747380de0e6e5e11b01f4137fb75c">l</a>, <a class="el" href="m__rhs_8fpp_8f90.html#a1adc244ddf111bde5ae4e9ecc136e571">rho</a>, c, mf, dalpha_rho_ds, dpres_ds, dvel_ds, dadv_ds)</td></tr>
-<tr class="memdesc:a4413e05fc457a989abc1837a3e840fad"><td class="mdescLeft">&#160;</td><td class="mdescRight">The L variables for the nonreflecting subsonic buffer CBC see pg. 13 of Thompson (1987). The nonreflecting subsonic buffer reduces the amplitude of any reflections caused by outgoing waves.  <br /></td></tr>
-<tr class="separator:a4413e05fc457a989abc1837a3e840fad"><td class="memSeparator" colspan="2">&#160;</td></tr>
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+<tr class="memdesc:a3ed89568b020fb0ab93a0836cd99ba8e"><td class="mdescLeft">&#160;</td><td class="mdescRight">The L variables for the nonreflecting subsonic buffer CBC see pg. 13 of Thompson (1987). The nonreflecting subsonic buffer reduces the amplitude of any reflections caused by outgoing waves.  <br /></td></tr>
+<tr class="separator:a3ed89568b020fb0ab93a0836cd99ba8e"><td class="memSeparator" colspan="2">&#160;</td></tr>
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-<tr class="memdesc:a1f0ea4a8b8cca03dcb25273ff4671ed1"><td class="mdescLeft">&#160;</td><td class="mdescRight">The L variables for the nonreflecting subsonic outflow CBC see pg. 454 of Thompson (1990). This nonreflecting subsonic CBC presumes an outgoing flow and reduces the amplitude of any reflections caused by outgoing waves.  <br /></td></tr>
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+<tr class="memdesc:aaebbe5603a0b7f154c2b6c1c9bbd0d47"><td class="mdescLeft">&#160;</td><td class="mdescRight">The L variables for the nonreflecting subsonic outflow CBC see pg. 454 of Thompson (1990). This nonreflecting subsonic CBC presumes an outgoing flow and reduces the amplitude of any reflections caused by outgoing waves.  <br /></td></tr>
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+<tr class="memdesc:a645b0d1fb8eb2b0390e9f3ad5fd91ed8"><td class="mdescLeft">&#160;</td><td class="mdescRight">L variables for the supersonic outflow CBC, see pg. 453 of Thompson (1990). For the supersonic outflow CBC, the flow evolution at the boundary is determined completely by the interior data.  <br /></td></tr>
+<tr class="separator:a645b0d1fb8eb2b0390e9f3ad5fd91ed8"><td class="memSeparator" colspan="2">&#160;</td></tr>
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simulation/m__compute__cbc_8fpp_8f90.js

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