Effect of surface cooling and roughness on transition for the Shuttle Orbiter
10th Fluid and Plasmadynamics Conference ; 1977 ; Albuquerque , NM , U.S.A.
1977-01-01
Conference paper
Electronic Resource
English
Shuttle Orbiter Experimental Boundary-Layer Transition Results with Isolated Roughness
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|Effect of Isolated Roughness Elements on Boundary-Layer Transition for Shuttle Orbiter
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