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Sonic inlet development for turbofan enginesThe static program has shown to date that very large noise reductions can be achieved by the sonic inlet concept with realistic inlet length and good aerodynamic performance. It is also shown that different inlet concepts produce substantially different results.
Document ID
19730003299
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Klujber, F. (Boeing Co. Seattle, WA, United States)
Date Acquired
August 7, 2013
Publication Date
January 1, 1972
Publication Information
Publication: NASA. Lewis Res. Center Aircraft Engine Noise Reduction
Subject Category
Aircraft
Accession Number
73N12026
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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IDRelationTitle19730003285Collected WorksAircraft Engine Noise Reduction
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