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Avco Lycoming quiet clean general aviation turbofan engineA fan module was developed using an existing turboshaft engine. The fan was designed using the latest in large engine noise control technology. A mixer was added to reduce the already low exhaust gas velocity. A nacelle incorporating sound treatment was provided for the test engine. A noise prediction model was used through the design process to evaluate the various design alternatives. Acoustic tests were then made to verify the prediction and identify the noise characteristics of the fan, core, jet, and sound treatment. Analysis of the recorded data yielded close agreement with the expected results. Core noise, as was expected, was the predominant source of noise for the quiet clean general aviation turbofan (QCGAT) engine. Flyover noise predictions were made which indicated that the Avco Lycoming QCGAT engine would meet the goals set for the QCGAT program.
Document ID
19800013846
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Wilson, C. A.
(Avco Lycoming Div. Stratford, CT, United States)
Date Acquired
August 10, 2013
Publication Date
March 1, 1980
Publication Information
Publication: NASA. Lewis Res. Center Gen. Aviation Propulsion
Subject Category
Aircraft Propulsion And Power
Accession Number
80N22333
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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