Blunt Trailing Edge Cooling Effects at Supersonic Regime
45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit ; 2009 ; Denver , Colorado
2009-01-01
Conference paper
Electronic Resource
English
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
|