NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Energy Efficient Engine acoustic supporting technology reportThe acoustic development of the Energy Efficient Engine combined testing and analysis using scale model rigs and an integrated Core/Low Spool demonstration engine. The scale model tests show that a cut-on blade/vane ratio fan with a large spacing (S/C = 2.3) is as quiet as a cut-off blade/vane ratio with a tighter spacing (S/C = 1.27). Scale model mixer tests show that separate flow nozzles are the noisiest, conic nozzles the quietest, with forced mixers in between. Based on projections of ICLS data the Energy Efficient Engine (E3) has FAR 36 margins of 3.7 EPNdB at approach, 4.5 EPNdB at full power takeoff, and 7.2 EPNdB at sideline conditions.
Document ID
19900019241
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Lavin, S. P.
(General Electric Co. Cincinnati, OH, United States)
Ho, P. Y.
(General Electric Co. Cincinnati, OH, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1985
Subject Category
Aircraft Propulsion And Power
Report/Patent Number
NAS 1.26:174834
R84AEB246
NASA-CR-174834
Report Number: NAS 1.26:174834
Report Number: R84AEB246
Report Number: NASA-CR-174834
Accession Number
90N28557
Funding Number(s)
CONTRACT_GRANT: NAS3-20643
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available