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NASA NTRS · 19670039745

Boundary layer transition at hypersonic Mach numbers.

Henderson, A., Jr.·Maddalon, D. V.

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Abstract

Transition from laminar to turbulent boundary layer flow at hypersonic Mach numbers, noting measurement techniques

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TRANSITION POINT TURBULENT FLOW REYNOLDS NUMBER HYPERSONIC SPEED LAMINAR BOUNDARY LAYER

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Henderson, A., Jr., Maddalon, D. V.. 1967-01-01. Boundary layer transition at hypersonic Mach numbers.. https://ntrs.nasa.gov/citations/19670039745

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