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On the calculation of supersonic, separating, and reattaching flowsA method is developed for solving the laminar and turbulent compressible boundary-layer equations for separating and reattaching flows. Results of this method are compared with experimental data for two laminar and three turbulent boundary-layer, shock-wave interactions. Several Navier-Stokes solutions were obtained for each of the laminar boundary-layer, shock-wave interactions considered. Comparison of these solutions indicates a first-order sensitivity in C sub f to the computational mesh selected in both the viscous and inviscid portions of the flow.
Document ID
19760002926
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Murphy, J. D. (NASA Ames Research Center Moffett Field, CA, United States)
Presley, L. L. (NASA Ames Research Center Moffett Field, CA, United States)
Rose, W. C. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1975
Publication Information
Publication: Aerodynamic Analyses Requiring Advanced Computers, Pt. 1
Subject Category
Aerodynamics
Accession Number
76N10014
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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