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Validation of CFD for aircraft design: A Boeing viewInformation is given in viewgraph form on computational fluid dynamics (CFD) for aircraft design. Topics covered include CFD validation for advanced systems, cavity flow, transonic flow, separated flow, boundary layer interaction, hypersonic flow, heat transfer, zonal modeling, the mathematical foundation for Navier-Stokes simulation, hypersonic inlets, and the role of wind tunnel tests.
Document ID
19920075818
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Vas, Irwin E. (Boeing Military Airplane Development Wichita, KS, United States)
Forester, C. (Boeing Military Airplane Development Wichita, KS, United States)
Yoshihara, Hideo (Boeing Military Airplane Development Wichita, KS, United States)
Nark, T. (Boeing Military Airplane Development Wichita, KS, United States)
Birch, S. (Boeing Military Airplane Development Wichita, KS, United States)
Bengelink, R. (Boeing Military Airplane Development Wichita, KS, United States)
Rubbert, Paul E. (Boeing Military Airplane Development Wichita, KS, United States)
Lee, Jerry (Boeing Military Airplane Development Wichita, KS, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1987
Publication Information
Publication: NASA. Ames Research Center, NASA CFD Validation Workshop
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
92N70942
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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