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Advanced-panel pilot codeNumerical research program helps establish "proof-of-concept" for newly developed higher-order panel method applicable to both subsonic and supersonic flows about nearly-arbitrary aircraft configurations. It is intended to solve variety of boundary-value problems in steady-subsonic or supersonic inviscid flow.
Document ID
19790000255
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Bills, G. R. (Boeing Commercial Airplane Co.)
Epton, M. A. (Boeing Commercial Airplane Co.)
Johnson, F. T. (Boeing Commercial Airplane Co.)
Date Acquired
August 10, 2013
Publication Date
December 1, 1979
Publication Information
Publication: NASA Tech Briefs
Volume: 4
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ARC-11278
Report Number: ARC-11278
ISSN: 0145-319X
Accession Number
79B10255
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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