The shock tube as a device for testing transonic airfoils at high Reynolds numbers
10th Aerodynamic Testing Conference ; 1978 ; San Diego , CA , U.S.A.
01.01.1978
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Transonic low-Reynolds number airfoils
AIAA | 1992
|Transonic low Reynolds number airfoils
AIAA | 1991
|