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Asymptotic features of shock-wave boundary-layer interactionA semi-implicit method is applied to solve the Navier-Stokes equations numerically and to evaluate the features of the free-interaction phenomenon that occurs when a shock wave impinges on a Blasius boundary layer. Comparisons are made with predictions of the triple-deck theory and experiment. Results include pressure and skin-friction distribution in the free-interaction region for various values of Reynolds number.
Document ID
19800058965
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hussaini, M. Y.
(NASA Ames Research Center Moffett Field, CA, United States)
Baldwin, B. S.
(NASA Ames Research Center Moffett Field, CA, United States)
Maccormack, R. W.
(NASA Ames Research Center Moffett Field, Calif., United States)
Date Acquired
August 10, 2013
Publication Date
August 1, 1980
Publication Information
Publication: AIAA Journal
Volume: 18
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
80A43135
Funding Number(s)
CONTRACT_GRANT: NAS1-14472
CONTRACT_GRANT: NAS1-14101
Distribution Limits
Public
Copyright
Other

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