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The Interaction of an Oblique Shock Wave with a Laminar Boundary LayerThe results of some experimental and theoretical studies of the interaction of oblique shock waves with laminar boundary layers are presented. Detailed measurements of pressure distribution, shear distribution, and velocity profiles were made during the interaction of oblique shock waves with laminar boundary layers on a flat plate. From these measurements a model was derived to predict the pressure levels characteristic of separation and the length of the separated region.
Document ID
19980231989
Acquisition Source
Headquarters
Document Type
Other - NASA Memorandum (MEMO)
Authors
Hakkinen, R. J. (Massachusetts Inst. of Tech. Cambridge, MA United States)
Greber, I. (Massachusetts Inst. of Tech. Cambridge, MA United States)
Trilling, L. (Massachusetts Inst. of Tech. Cambridge, MA United States)
Abarbanel, S. S. (Massachusetts Inst. of Tech. Cambridge, MA United States)
Date Acquired
September 6, 2013
Publication Date
March 1, 1959
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
NASA-MEMO-2-18-59W
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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