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Large-scale wind-tunnel investigation of the noise characteristics of a semispan wing equipped with an externally blown jet flapA wind tunnel investigation was made of the noise characteristics of a 4.42 m(14.5 foot) semispan, externally-blown jet flap model. The model was equipped with a single 76.2 cm(30 inch) diameter, ducted fan with a 1.03 pressure ratio. The effects of flap size, fan vertical location, and forward speed on the noise characteristics were studied. The data from the investigation is presented in the form of tabulated one-third octave band frequency spectrums and perceived noise levels for each test condition.
Document ID
19720016361
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Falarski, M. D.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
August 6, 2013
Publication Date
May 1, 1972
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-62154
Report Number: NASA-TM-X-62154
Accession Number
72N24011
Funding Number(s)
PROJECT: RTOP 760-72-01-05-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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