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STOL noise sources and fan noise treatmentSTOL noise goals, noise sources, and their affects on engine and propulsion systems design are considered. It is shown that major noise sources constitute the blown-flap system with its turbofan engine and the augmentor wing propulsion system. Most of the problem areas associated with STOL propulsion systems are defined and the development of a multistage fan engine with proper rotor-stator spacings and low noise core exhaust jet is illustrated. A variable-area acoustic inlet provides near sonic flow conditions during takeoff and landing.
Document ID
19730003296
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Rulis, R. J.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1972
Publication Information
Publication: Aircraft Engine Noise Reduction
Subject Category
Aircraft
Accession Number
73N12023
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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