The effect of trailing edge geometry on cavity flow oscillation driven by a supersonic shear layer
The aeronautical journal ; 102 , 1013 ; 129-136
1998
Article (Journal)
Unknown
Effect of Boundary Layer Shear on Trailing Edge Noise
AIAA | 2017
|Effect of trailing-edge thickness on lift at supersonic velocities
Engineering Index Backfile | 1955
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