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The structure of shock wave-boundary layer interactions in transonic flowThe structure of transonic shock wave-boundary layer interactions is studied using asymptotic analyses, for an oblique shock impinging on a flat plate boundary layer. Solutions for unseparated laminar and turbulent boundary layers are reviewed, and incipient separation of a turbulent boundary layer is considered.
Document ID
19760044886
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Adamson, T. C., Jr. (Michigan, University Ann Arbor, Mich., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1976
Subject Category
Aerodynamics
Meeting Information
Meeting: Symposium Transsonicum II
Location: Goettingen
Start Date: September 8, 1975
End Date: September 13, 1975
Accession Number
76A27852
Funding Number(s)
CONTRACT_GRANT: NGR-23-005-523
Distribution Limits
Public
Copyright
Other

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