Revisiting the Transonic Similarity Rule: Critical Mach Number Prediction Using Potential Flow Solutions
34th AIAA Applied Aerodynamics Conference
01.01.2016
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2016
|Separated trailing-edge flow at a transonic Mach number
AIAA | 1983
|Separated trailing-edge flow at a transonic Mach number
NTRS | 1983
|Separated trailing-edge flow at a transonic Mach number
AIAA | 1982
|