NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Status of the JT8D refan noise reduction programThe present work describes measures being taken to suppress jet noise in the JT8D engine and reports on some preliminary acoustic tests to evaluate noise characteristics of the engine. To reduce noise generation without sacrificing other essential engine performance or durability characteristics, the two stage fan will be replaced by a larger-diameter single stage fan. Refanned engines have an increased bypass ratio that contributes to the reduction of jet exhaust noise. Advanced acoustical design features will be incorporated in the larger, single-stage fan, and acoustic treatment will be incorporated in both the engine and the nacelle. First tests have shown that engine component noise levels are about as predicted and the acoustic treatment sections tested to date are providing predicted levels of attenuation. Further work is required to demonstrate engine performance goals and compatibility with 727 and DC-9 installations.
Document ID
19750034462
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Kester, J. D.
(United Aircraft Corp. Pratt and Whitney Aircraft Div., East Hartford, Conn., United States)
Date Acquired
August 8, 2013
Publication Date
January 1, 1974
Subject Category
Aircraft Propulsion And Power
Accession Number
75A18534
Distribution Limits
Public
Copyright
Other

Available Downloads

There are no available downloads for this record.
No Preview Available