Skip to main content
Advances in Aerodynamics

Table 5 Flow conditions of the ONERA M6 wing in Ref. [33]

From: Numerical study on the influence of initial ambient temperature on the aerodynamic heating in the tube train system

Mach

Reynolds number

Attack angle

Sideslip angle

0.8395

11.72 × 106

3.06°

0°

Back to article page