Blunt Trailing Edge Cooling Effects at Supersonic Regime
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit ; 2009 ; Denver , Colorado
01.01.2009
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Analysis of Blunt Trailing Edge Airfoils
AIAA | 2003
|Experimental investigation of base pressure on blunt-trailing-edge wings at supersonic velocities
Engineering Index Backfile | 1952
|