From: A sharp-interface immersed boundary method for simulating high-speed compressible inviscid flows
Case | Flow variables | Exact | Present |
---|---|---|---|
Ma1 = 3.0 | Ma2 | 2.255 | 2.255 |
p2/p1 | 2.822 | 2.821 | |
T2/T1 | 1.388 | 1.388 | |
Shock-angle | 32.24 ° | 32.21 ° | |
Ma1 = 5.0 | Ma2 | 3.504 | 3.504 |
p2/p1 | 4.781 | 4.781 | |
T2/T1 | 1.736 | 1.736 | |
Shock-angle | 24.32 ° | 24.31 ° |