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Acoustic characteristics of a semispan wing equipped with an externally blown jet flap including results at forward speedA wind-tunnel investigation was made of the noise characteristics of a 14.5-ft semispan, externally blown jet flap model. The model was equipped with a single 30-in. 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. With the ducted fan mounted 0.79 or 1.24 diameters below the wing and a flap chord greater than 50 percent, the peak perceived noise level increased 2 to 3 Pndb when the flap was deflected to 90 deg. The jet scrubbing noise increase 3 to 4 db when the flap was deflected 90 deg. Installation of the fan on the wing was responsible for 1 to 2 db of this change. Forward speed did not have a significant effect on the perceived noise level, although it did cause a reduction in the sound pressure levels of the first and second fan harmonics.
Document ID
19730009314
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Falarski, M. D.
(NASA Ames Research Center Moffett Field, CA, United States)
Date Acquired
September 2, 2013
Publication Date
March 1, 1973
Subject Category
Aircraft
Report/Patent Number
A-4469
NASA-TM-X-2749
Report Number: A-4469
Report Number: NASA-TM-X-2749
Accession Number
73N18041
Funding Number(s)
PROJECT: RTOP 760-72-01-05-00-21
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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