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Effects of Interaction Between Normal Shock and Boundary LayerA discussion of the interaction between normal shocks and boundary layers on the basis of experimental evidence obtained in studies of supersonic flows in passages is given. The investigation was made as a result of the inability of the existing normal-shock theory to explain phenomena involving normal shocks that occurred in the presence of boundary layers. Assumptions with regard to the character of the effects of interaction between boundary layer and normal shock are proposed; these assumptions seem to give good agreement with certain experimental results.
Document ID
20140002003
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Donaldson, Coleman duP.
(National Advisory Committee for Aeronautics. Langley Aeronautical Lab. Langley Field, VA, United States)
Date Acquired
March 18, 2014
Publication Date
January 1, 1944
Subject Category
Fluid Mechanics And Thermodynamics
Report/Patent Number
NACA-CB-4A27
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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