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Pressure distributions on a wing having NACA 4415 airfoil sections with trailing-edge flaps set at 0 deg and 40 degWind tunnel measurements of pressure distributions on wing having NACA 4415 airfoil sections with trailing-edge flaps set at 0 deg and 40 deg
Document ID
19710018601
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Carter, A. W. (NASA Langley Research Center Hampton, VA, United States)
Date Acquired
September 2, 2013
Publication Date
June 1, 1971
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-2225
L-7568
Report Number: NASA-TM-X-2225
Report Number: L-7568
Accession Number
71N28077
Funding Number(s)
CONTRACT_GRANT: 721-01-11-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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