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Shock-wave boundary layer interactionsPresented is a comprehensive, up-to-date review of the shock-wave boundary-layer interaction problem. A detailed physical description of the phenomena for transonic and supersonic speed regimes is given based on experimental observations, correlations, and theoretical concepts. Approaches for solving the problem are then reviewed in depth. Specifically, these include: global methods developed to predict sudden changes in boundary-layer properties; integral or finite-difference methods developed to predict the continuous evolution of a boundary-layer encountering a pressure field induced by a shock wave; coupling methods to predict entire flow fields; analytical methods such as multi-deck techniques; and finite-difference methods for solving the time-dependent Reynolds-averaged Navier-Stokes equations used to predict the development of entire flow fields. Examples are presented to illustrate the status of the various methods and some discussion is devoted to delineating their advantages and shortcomings. Reference citations for the wide variety of subject material are provided for readers interested in further study.
Document ID
19860019701
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Delery, J.
(Office National d'Etudes et de Recherches Aeronautiques Paris, France)
Marvin, J. G.
(NASA Ames Research Center Moffett Field, Calif., United States)
Reshotko, E.
(Case Western Reserve Univ. Cleveland, Ohio, United States)
Date Acquired
September 5, 2013
Publication Date
February 1, 1986
Publication Information
ISBN: 92-835-1519-6
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AGARD-AG-280
AD-A171302
Accession Number
86N29173
Distribution Limits
Public
Copyright
Other
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