Tests conducted in 8 × 7-ft supersonic test section of Ames Unitary Plan wind tunnel to determine location of transition on three separate hemispheres having absolute surface roughness values of 50, 580, and 2760 microin.; location determined from shadow-graphs and checked by local temperature-recovery measurements; pertinence to reducing aerodynamic heating of ballistic missiles.
Boundary-layer-transition measurements on hemispheres of various surface roughnesses in wind tunnel at mach numbers from 2.48 to 3.55
NASA -- Memo
National Aeronautics and Space Administration -- Memorandums ; Memo n 12-25-58A
1959
29 pages
Report
English
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