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Upper-surface-blowing flow-turning performanceJet exhaust flow-turning characteristics were determined for systematic variations in upper-surface blowing exhaust nozzles and trailing-edge flap configuration variables from experimental wind-off (static) flow studies. For conditions with parallel flow exhausting from the nozzle, jet height (as indicated by nozzle exit height) and flap radius were found to be the most important parameters relating to flow turning. Nonparallel flow from the nozzle, as obtained from an internal roof angle and/or side spread angle, had a large favorable effect on flow turning. Comparisons made between static turning results and wind tunnel aerodynamic studies of identical configurations indicated that static flow-turning results can be indicative of wind-on powered lift performance for both good and poor nozzle-flap combinations but, for marginal designs, can lead to overly optimistic assessment of powered lift potential.
Document ID
19780016105
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Sleeman, W. C., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Phelps, A. E., III
(Army Air Mobility R and D Lab. Hampton, Va., United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1976
Publication Information
Publication: Powered-Lift Aerodyn. and Acoustics
Subject Category
Aerodynamics
Accession Number
78N24048
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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