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Large scale wind tunnel investigation of a semispan wing equipped with an externally-blown jet flapA wind tunnel investigation was made of the aerodynamic characteristics of a 14.5 foot semispan, externally-blown jet flap model. The model was equipped with a single 30-inch diameter, ducted fan with a 1.03 pressure ratio. The effects of flap size, fan vertical location, and wing sweep on the longitudinal aerodynamic characteristics were studied.
Document ID
19720004253
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Falarski, M. D. (NASA Ames Research Center Moffett Field, CA, United States)
Aiken, T. N. (NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
July 1, 1971
Subject Category
Aerodynamics
Report/Patent Number
NASA-TM-X-62079
Report Number: NASA-TM-X-62079
Accession Number
72N11902
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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