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Flap noise measurements for STOL configurations using external upper surface blowingScreening tests of upper surface blowing on externally blown flaps configurations were conducted. Noise and turning effectiveness data were obtained with small-scale, engine-over-the-wing models. One large model was tested to determine scale effects. Nozzle types included circular, slot, D-shaped, and multilobed. Tests were made with and without flow attachment devices. For STOL applications the particular multilobed mixer and the D-shaped nozzles tested were found to offer little or no noise advantage over the round convergent nozzle. High aspect ratio slot nozzles provided the quietest configurations. In general, upper surface blowing was quieter than lower surface blowing for equivalent EBF models.
Document ID
19730006303
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dorsch, R. G.
(NASA Lewis Research Center Cleveland, OH, United States)
Reshotko, M.
(NASA Lewis Research Center Cleveland, OH, United States)
Olsen, W. A.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-68167
E-7227
Report Number: NASA-TM-X-68167
Report Number: E-7227
Meeting Information
Meeting: Propulsion Joint Specialists Conf.
Location: New Orleans, LA
Country: United States
Start Date: November 29, 1972
End Date: December 1, 1972
Sponsors: AIAA and ASME
Accession Number
73N15030
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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