Transition from laminar to turbulent boundary layer flow on sharp cones hypersonic Mach numbers, noting measurement techniques
Boundary-layer transition on sharp cones at hypersonic Mach numbers.
AEROSPACE SCIENCES MEETING ; 1967 ; NEW YORK, NY
1968-03-01
Miscellaneous
No indication
English
Mach 6 Boundary-Layer Stability Experiments on Sharp and Blunted Cones
Online Contents | 2006
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