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A preliminary evaluation of noise reduction potential for the upper surface blown flapAn assessment of the basic acoustic characteristics and noise reduction potential of an upper surface blown flap consisting of a rectangular nozzle and a single turning flap which was designed to approximate a typical takeoff setting is presented. The noise reduction concepts studied were: (1) replacing a section of the flap trailing edge with a porous material and (2) active modification of the flow field using blowing near the trailing edge. Diagrams of the airfoil section and test equipment are provided. Photographs of airflow conditions across the aerodynamic surface are included.
Document ID
19730011290
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Hayden, R. E.
(Bolt, Beranek, and Newman, Inc. Cambridge, MA, United States)
Scharton, T. D.
(Bolt, Beranek, and Newman, Inc. Cambridge, MA, United States)
Kadman, Y.
(Bolt, Beranek, and Newman, Inc. Cambridge, MA, United States)
Wilby, J. F.
(Bolt, Beranek, and Newman, Inc. Cambridge, MA, United States)
Rudd, M. J.
(Bolt, Beranek, and Newman, Inc. Cambridge, MA, United States)
Date Acquired
September 2, 2013
Publication Date
January 1, 1972
Subject Category
Aircraft
Report/Patent Number
BBN-2478
NASA-CR-112246
Report Number: BBN-2478
Report Number: NASA-CR-112246
Accession Number
73N20017
Funding Number(s)
CONTRACT_GRANT: NAS1-11839
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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