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Aerodynamic design and analysis system for supersonic aircraft. Part 1: General description and theoretical developmentAn integrated system of computer programs has been 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. Interactive graphics are optional at the user's request. This part presents a general description of the system and describes the theoretical methods used.
Document ID
19750010113
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 3, 2013
Publication Date
March 1, 1975
Publication Information
Publisher: NASA
Subject Category
Aerodynamics
Report/Patent Number
NSF/RANN/SE/GI-36731X/PR-74-1
NASA-CR-2520
D6-41768
Accession Number
75N18185
Funding Number(s)
CONTRACT_GRANT: NAS1-12052
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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