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Externally blown flap impingement parametersThe performance of two externally blown flap (EBF) wind tunnel models was compared with an engine exhaust flap impingement correlation parameter. One model was a four engine EBF triple slotted flap transport. Isolated engine wake surveys were conducted to define the wake properties of five separate engine configurations for which performance data were available. The other model was a two engine EBF transport for which the engine wake properties were estimated. The correlation parameter was a function of engine exhaust dynamic pressure at the flap location, area of engine exhaust flap impingement, total exhaust area at the flap location, and engine thrust. The distribution of dynamic pressure for the first model was measured; however, the distribution for the second model was assumed to be uniform.
Document ID
19780016110
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hoad, D. R.
(Army Air Mobility Research and Development Lab. Hampton, VA, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1976
Publication Information
Publication: NASA. Langley Res. Center Powered-Lift Aerodyn. and Acoustics
Subject Category
Aerodynamics
Accession Number
78N24053
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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