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Potential flow solution for a STOL wing propulsion systemPotential flow solution for STOL wing propulsion system presenting flow fields, pressure distribution, and lift coefficient for externally blown flap, high-lift configuration
Document ID
19710020298
Acquisition Source
Legacy CDMS
Document Type
Other - NASA Technical Note (TN)
Authors
Albers, J. A. (NASA Lewis Research Center Cleveland, OH, United States)
Potter, M. C. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
NASA-TN-D-6394
E-6132
Accession Number
71N29774
Funding Number(s)
CONTRACT_GRANT: 721-03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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