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Hypersonic CFD applications at NASA Langley using CFL3D and CFL3DEThe CFL3D/CFL3DE CFD codes and the industrial use status of the codes are outlined. Comparison of grid density, pressure, heat transfer, and aerodynamic coefficience are presented. Future plans related to the National Aerospace Plane Program are briefly outlined.
Document ID
19910001561
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Richardson, Pamela F. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1989
Publication Information
Publication: NASA, Ames Research Center, NASA Computational Fluid Dynamics Conference. Volume 2: Sessions 7-12
Subject Category
Aerodynamics
Accession Number
91N10874
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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