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A numerical solution of the unsteady airfoil with application to the vortex interaction problemNumerical analysis of aerodynamic forces on thin airfoil operating in unsteady potential flow
Document ID
19710006352
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Rudhman, W. E. (Pennsylvania State Univ. University Park, PA, United States)
Date Acquired
August 6, 2013
Publication Date
December 1, 1970
Subject Category
Aerodynamics
Report/Patent Number
NASA-CR-111843
Report Number: NASA-CR-111843
Accession Number
71N15827
Funding Number(s)
CONTRACT_GRANT: NGR-39-009-111
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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