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benchmarks/5eq_rk3_weno3_hllc
2D_axisym_shockwatercavity Expand file tree Collapse file tree 4 files changed +4
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lines changed Original file line number Diff line number Diff line change 8181c_w = math .sqrt (gamw * (p0w + piw ) / rho0w )
8282
8383# Shock Mach number of interest. Note that the post-shock properties can be defined in terms of either
84- # Min or psOp0a. Just comment/uncomment appropriatelly
84+ # Min or psOp0a. Just comment/uncomment appropriately
8585Min = 2.4
8686
8787## Pos to pre shock ratios - AIR
Original file line number Diff line number Diff line change 5959c_w = math .sqrt (gamw * (p0w + piw ) / rho0w )
6060
6161# 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
6363Min = 2.146
6464
6565## Pos to pre shock ratios - AIR
Original file line number Diff line number Diff line change 5959c_w = math .sqrt (gamw * (p0w + piw ) / rho0w )
6060
6161# 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
6363Min = 2.4
6464
6565## Pos to pre shock ratios - AIR
Original file line number Diff line number Diff line change 5959c_w = math .sqrt (gamw * (p0w + piw ) / rho0w )
6060
6161# 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
6363Min = 2.4
6464
6565## Pos to pre shock ratios - AIR
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