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Lift induced on a swept wing by a two-dimensional partial-span deflected jet at Mach numbers from 0.20 to 1.30Induced lift characteristics of swept wing-body configuration with partial-span jet in flow at Mach 0.20 to 1.30
Document ID
19710022831
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Capone, F. J. (NASA Langley Research Center Hampton, VA, United States)
Corson, B. W., Jr. (NASA Langley Research Center Hampton, VA, United States)
Putnam, L. E. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
August 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
L-7707
NASA-TM-X-2309
Report Number: L-7707
Report Number: NASA-TM-X-2309
Accession Number
71N32307
Funding Number(s)
CONTRACT_GRANT: 764-74-02-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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