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Engine-over-the-wing noise researchAcoustic measurements for large model eingine-over-the-wing (EOW) research configurations having both conventional and powered lift applications were taken for flap positions typical of takeoff and approach and at locations simulating flyover and sideline. The results indicate that the noise is shielded by the wing and redirected above it, making the EOW concept a prime contender for quiet aircraft. The large-scale noise data are in agreement with earlier small-model results. Below the wing, the EOW configuration is about 10 PNdb quieter than the engine-under-the-wing externally-blown-flap for powered lift, and up to 10 db quieter than the nozzle alone at high frequencies for conventional lift applications.
Document ID
19730015343
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Reshotko, M.
(NASA Lewis Research Center Cleveland, OH, United States)
Goodykoontz, J. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Dorsch, R. G.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1973
Subject Category
Aircraft
Report/Patent Number
E-7429
NASA-TM-X-68246
Report Number: E-7429
Report Number: NASA-TM-X-68246
Meeting Information
Meeting: Fluid and Plasma Dyn. Conf.
Location: Palm Springs, CA
Country: United States
Start Date: July 16, 1973
End Date: July 18, 1973
Sponsors: AIAA
Accession Number
73N24070
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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