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Noise Considerations in the Design and Operation of V/STOL AircraftAvailable propulsion-system noise data have been applied to the problems of design and operation of V/STOL aircraft. In particular, considerations have been given to minimizing adverse community reaction for operations between airports and to minimizing detection due to noise for special missions. For minimizing adverse community reaction, configurations incorporating low-blade-loading rotors, low-tip-speed propellers, or turbofan-type engines are judged to be most satisfactory. For minimizing detection, consideration must be given to minimizing the noise of the generating airplane, having maximum background noise in the vicinity of the observer, and operating the aircraft at minimum altitude.



Document ID
20040047144
Acquisition Source
Langley Research Center
Document Type
Other - NASA Technical Note (TN)
Authors
Maglieri, Domenic J.
(NASA Langley Research Center Hampton, VA, United States)
Hilton, David A.
(NASA Langley Research Center Hampton, VA, United States)
Hubbard, Harvey H.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 21, 2013
Publication Date
April 1, 1961
Subject Category
Aircraft Propulsion And Power
Aircraft Design, Testing And Performance
Report/Patent Number
NASA-TN-D-736
L-1430
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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