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benchmarks/5eq_rk3_weno3_hllc/case.py

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c_w = math.sqrt(gamw * (p0w + piw) / rho0w)
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# Shock Mach number of interest. Note that the post-shock properties can be defined in terms of either
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# Min or psOp0a. Just comment/uncomment appropriatelly
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# Min or psOp0a. Just comment/uncomment appropriately
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Min = 2.4
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## Pos to pre shock ratios - AIR

examples/2D_axisym_shockwatercavity/case.py

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@@ -59,7 +59,7 @@
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c_w = math.sqrt(gamw * (p0w + piw) / rho0w)
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# Shock Mach number of interest. Note that the post-shock properties can be defined in terms of either
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# Min or psOp0a. Just comment/uncomment appropriatelly
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# Min or psOp0a. Just comment/uncomment appropriately
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Min = 2.146
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## Pos to pre shock ratios - AIR

examples/3D_shockdroplet/case.py

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@@ -59,7 +59,7 @@
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c_w = math.sqrt(gamw * (p0w + piw) / rho0w)
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# Shock Mach number of interest. Note that the post-shock properties can be defined in terms of either
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# Min or psOp0a. Just comment/uncomment appropriatelly
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# Min or psOp0a. Just comment/uncomment appropriately
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Min = 2.4
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## Pos to pre shock ratios - AIR

examples/3D_shockdroplet_muscl/case.py

Lines changed: 1 addition & 1 deletion
Original file line numberDiff line numberDiff line change
@@ -59,7 +59,7 @@
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c_w = math.sqrt(gamw * (p0w + piw) / rho0w)
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# Shock Mach number of interest. Note that the post-shock properties can be defined in terms of either
62-
# Min or psOp0a. Just comment/uncomment appropriatelly
62+
# Min or psOp0a. Just comment/uncomment appropriately
6363
Min = 2.4
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## Pos to pre shock ratios - AIR

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