Boundary-layer transition on sharp cones at hypersonic Mach numbers.
HENDERSON, A., JR. /NASA, LANGLEY RESEARCH CENTER, AERO-PHYSICS DIV., FLOW ANALYSIS SECTION, HAMPTON, MADDALON, D. V.
AIAA Journal ; 6 , 3 ; 424-431
1968-01-01
8 pages
Article (Journal)
Electronic Resource
English
Mach 6 Boundary-Layer Stability Experiments on Sharp and Blunted Cones
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