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Starting phenomena for hypersonic inlets with thick turbulent boundary layers at Mach 6

T. J. Goldberg, J. N. Hefner

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Abstract

Starting phenomena of two-dimensional hypersonic inlets with turbulent intake boundary layers at free stream Mach 6

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Starting phenomena of two-dimensional hypersonic inlets with turbulent intake boundary layers at free stream Mach 6

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OpenAlex reports 32 citations for this work. Citation counts describe recorded attention and do not establish research quality.

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Available abstract

Starting phenomena of two-dimensional hypersonic inlets with turbulent intake boundary layers at free stream Mach 6

Key concepts: Mach number, Hypersonic speed, Boundary layer, Turbulence, Aerospace engineering, Mechanics, Boundary (topology), Meteorology

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