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A system for aerodynamic design and analysis of supersonic aircraft. Part 1: General description and theoretical developmentAn integrated system of computer programs was developed for the design and analysis of supersonic configurations. The system uses linearized theory methods for the calculation of surface pressures and supersonic area rule concepts in combination with linearized theory for calculation of aerodynamic force coefficients.
Document ID
19810006455
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Middleton, W. D. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Lundry, J. L. (Boeing Commercial Airplane Co. Seattle, WA, United States)
Date Acquired
September 4, 2013
Publication Date
December 1, 1980
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-3351
D6-41840-1
Report Number: NASA-CR-3351
Report Number: D6-41840-1
Accession Number
81N14970
Funding Number(s)
CONTRACT_GRANT: NAS1-15534
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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