Experimental Study of the Use of Vortex Generators to Reduce Fluctuating Pressure Loads in Shock Wave Turbulent Boundary Layer Interactions
15th Aeroacoustics conference ; 1993 ; Long Beach; CA
1993-01-01
AIAA 93-4335
Separate paper nos 93-4320 to 93-4450 with gaps held only
Conference paper
English
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Reduction of Fluctuating Pressure Loads in Shock-Boundary-Layer Interactions Using Vortex Generators
Online Contents | 1995
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