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Externally blown flap impingement noise.An investigation of externally blown flap impingement noise was conducted using a full-scale turbofan engine and aircraft wing. The noise produced with a daisy nozzle installed on the engine exhaust system was greater than that produced by a conical nozzle at the same thrust. The daisy nozzle caused the jet velocity to decay about 35 percent at the flap. The presence of the wing next to the conical nozzle increased the noise, as did increasing the flap deflection. Compared with the conical nozzle, the daisy nozzle produced slightly less noise at a flap deflection of 60 deg but produced more noise at the lower flap deflections tested.
Document ID
19720052295
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Putnam, T. W.
Lasagna, P. L.
(NASA Flight Research Center Edwards, Calif., United States)
Date Acquired
August 6, 2013
Publication Date
June 1, 1972
Subject Category
Aerodynamics
Report/Patent Number
AIAA PAPER 72-664
Meeting Information
Meeting: American Institute of Aeronautics and Astronautics, Fluid and Plasma Dynamics Conference
Location: Boston, MA
Start Date: June 26, 1972
End Date: June 28, 1972
Sponsors: American Institute of Aeronautics and Astronautics
Accession Number
72A35961
Distribution Limits
Public
Copyright
Other

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