NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
State-of-the-art of turbofan engine noise controlA description is presented of some of the recent advances in the technology of turbofan engine noise reduction, taking into account turbomachinery noise sources, new fans for low noise, fan and core noise suppression, and a new program for improving static noise testing of fans and engines. The problem of jet noise has been substantially reduced in connection with the lower jet velocities employed in the case of the high bypass turbofan engines. The dominant noise sources are now related to the turbomachinery with the fan stage, the compressor, and the turbine. Since the fan stage is the primary source of turbomachinery noise, it has been considered in a major part of the investigations designed to reduce turbofan engine noise.
Document ID
19780051749
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Jones, W. L.
(NASA Lewis Research Center Cleveland, OH, United States)
Groeneweg, J. F.
(NASA Lewis Research Center Cleveland, Ohio, United States)
Date Acquired
August 9, 2013
Publication Date
January 1, 1977
Subject Category
Aircraft Propulsion And Power
Meeting Information
Meeting: In: NOISE-CON 77; National Conference on Noise Control Engineering
Location: Hampton, VA
Start Date: October 17, 1977
End Date: October 19, 1977
Accession Number
78A35658
Distribution Limits
Public
Copyright
Other

Available Downloads

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