Wind Tunnel Test of Gurney Flaps and T-Strips on an NACA 23012 Wing
25th AIAA Applied Aerodynamics Conference
01.01.2007
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Wind Tunnel Test of Gurney Flaps and T-Strips on an NACA 23012 Wing
British Library Conference Proceedings | 2007
|High-speed wind-tunnel tests of NACA 23012 and 23012-64 airfoils
Engineering Index Backfile | 1941
|Wind-tunnel investigation of NACA 23012 airfoil with 30-percent-chord venetian-blind flaps
Engineering Index Backfile | 1942
|