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Aerodynamics of Supersonic AircraftAn integrated system for the analysis of supersonic configurations consists of an executive driver and eight basic computer programs that build up force coefficients of an selected configuration. System employs modified linearized theory for calculation of surface pressures and employs supersonic-area-rule concepts in combination with linearized theory for calculation of aerodynamic force coefficients.
Document ID
19810000199
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Tech Brief
Authors
Middleton, W. D. (The Boeing Co.)
Lundry, J. L. (The Boeing Co.)
Coleman, R. G. (The Boeing Co.)
Date Acquired
August 11, 2013
Publication Date
November 1, 1982
Publication Information
Publication: NASA Tech Briefs
Volume: 6
Issue: 2
ISSN: 0145-319X
Subject Category
Mechanics
Report/Patent Number
LAR-12857
Report Number: LAR-12857
ISSN: 0145-319X
Accession Number
81B10199
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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