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Wing-Design Program for Subsonic or Supersonic SpeedsSurface of mildest possible camber generated. WINGDES provides analysis, design capability and is applicable to both subsonic and supersonic flows. Optimization carried out for entire wing or for designated leading- and trailing-edge areas, for design of missionadaptive surfaces. WINGDES written in FORTRAN IV.
Document ID
19860000338
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Carlson, H. W.
(Kentron International, Inc.)
Walkley, K. B.
(Kentron International, Inc.)
Date Acquired
August 12, 2013
Publication Date
July 1, 1986
Publication Information
Publication: NASA Tech Briefs
Volume: 10
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-13315
Accession Number
86B10338
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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