Skip to main content
Advances in Aerodynamics

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

Back to article page