Investigation of Multiple-Equilibrium-Points Phenomena in Transonic Flutter of NACA 64A010 Airfoil
AIAA Journal ; 60 , 9 ; 5581-5588
01.09.2022
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Boundary-layer and stalling characteristics of NACA 64a010 airfoil section
Engineering Index Backfile | 1950
|Unsteady pressures on a NACA 64A010 airfoil experimental and theoretical results
Tema Archiv | 1979
|