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Measurement and prediction of Energy Efficient Engine noiseThe NASA/GE Energy Efficient Engine (E3) static noise levels were measured in an acoustic arena on the Integrated Core and Low Spool Test System. These measured levels were scaled to the appropriate size to power four study aircraft and were projected to flight for evaluation of noise levels relative to FAR36, Stage III limits. As a result of these evaluations, it is predicted that the NASA/GE E3 engine with a wide spacing cut-on blade/vane ratio fan and a forced mixer nozzle can meet FAR36 Stage III limits with sufficient design margin.
Document ID
19850031803
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Lavin, S. P.
(General Electric Co. Cincinnati, OH, United States)
Ho, P. Y.
(General Electric Co., Aircraft Engine Business Group, Cincinnati OH, United States)
Chamberlin, R.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
August 12, 2013
Publication Date
October 1, 1984
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
AIAA PAPER 84-2284
Accession Number
85A13954
Distribution Limits
Public
Copyright
Other

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