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Interactive Graphics Analysis for Aircraft DesignProgram uses higher-order far field drag minimization. Computer program WDES WDEM preliminary aerodynamic design tool for one or two interacting, subsonic lifting surfaces. Subcritical wing design code employs higher-order far-field drag minimization technique. Linearized aerodynamic theory used. Program written in FORTRAN IV.
Document ID
19830000194
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Townsend, J. C.
Date Acquired
August 11, 2013
Publication Date
October 1, 1983
Publication Information
Publication: NASA Tech Briefs
Volume: 7
Issue: 4
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12951
Accession Number
83B10194
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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