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Calculating Wave Drag on an AircraftImproved program based on more-accurate mathematical mode. WDAG2 calculates supersonic zero-lift wave drag of complex aircraft configurations. Incorporates extended capabilities for geometric input to enable use of more-accurate mathematical model. Engineer defines aircraft components as fusiform or non-fusiform by use of traditional parallel contours. Written in FORTRAN IV.
Document ID
19870000471
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Dollyhigh, Samuel M. (NASA Langley Research Center, Hampton, Va.)
Craidon, Charlotte B. (NASA Langley Research Center, Hampton, Va.)
Date Acquired
August 13, 2013
Publication Date
October 1, 1987
Publication Information
Publication: NASA Tech Briefs
Volume: 11
Issue: 9
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
ISSN: 0145-319X
Report Number: LAR-13634
LAR-13634
Accession Number
87B10471
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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