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Development and applications of supersonic unsteady consistent aerodynamics for intering parallel wings: Programmer's manualThe computer program written in support of the problem to determine aerodynamic influence coefficients on parallel interfering wings is described. The information is geared to the programmer. It is sufficient to describe the program logic and the required peripheral storage.
Document ID
19730004564
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Paine, A. A. (Bell Aerospace Co. Buffalo, NY, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1972
Subject Category
Fluid Mechanics
Report/Patent Number
NASA-CR-112185
Report Number: NASA-CR-112185
Accession Number
73N13291
Funding Number(s)
CONTRACT_GRANT: NAS1-10880
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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