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Shock wave-turbulent boundary layer interactions in transonic flow (1976)

Messiter, A. F. ; Adamson, T. C., Jr.

In: CASI

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Publication Date: 2019-06-27

Description: The method of matched asymptotic expansions is used in analyzing the structure of the interaction region formed when a shock wave impinges on a turbulent flat plate boundary layer in transonic flow. Solutions in outer regions, governed by inviscid flow equations, lead to relations for the wall pressure distribution. Solutions in the inner regions, governed by equations in which Reynolds and/or viscous stresses are included, lead to a relation for the wall shear stress. Solutions for the wall pressure distribution are reviewed for both oblique and normal incoming shock waves. Solutions for the wall shear stress are discussed.

Keywords: AERODYNAMICS

Type: NASA. Langley Res. Center Advan. in Eng. Sci., Vol. 4; p 1425-1435

Format: application/pdf

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