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Noise measurements for various configurations of a model of a mixer nozzle externally blown flap systemNoise data were taken for variations to a large scale model of an externally blown flap lift augmentation system. The variations included two different mixer nozzles (7 and 8 lobes), two different wing models (2 and 3 flaps), and different lateral distances between the wing chord line and the nozzle centerline. When the seven lobe was used with the trailing flap in the 60 deg position, increasing the wing to nozzle distance had no effect on the sound level. When the eight lobe nozzle was used there was a decrease in sound level. With the 20 deg flap setting the noise level decreased when the distance was increased using either nozzle.
Document ID
19730012332
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Goodykoontz, J. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Wagner, J. M.
(NASA Lewis Research Center Cleveland, OH, United States)
Sargent, N. B.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
April 1, 1973
Subject Category
Aircraft
Report/Patent Number
NASA-TM-X-2776
E-7300
Report Number: NASA-TM-X-2776
Report Number: E-7300
Accession Number
73N21059
Funding Number(s)
PROJECT: RTOP 741-89
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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