Skip to main content

Table 1 Computational conditions

From: Kinetic comparative study on aerodynamic characteristics of hypersonic reentry vehicle from near-continuous flow to free molecular flow

  Ma Re KnHS ρ,kg/m3 T,K Tw,K
Case1 8.0 5.937 2.75 1.11×10−7 56 300
Case2 8.0 59.37 0.275 1.11×10−6 56 300
Case3 8.0 593.7 0.0275 1.11×10−5 56 300
Case4 8.0 5937.0 0.00275 1.11×10−4 56 300