NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Due to the lapse in federal government funding, NASA is not updating this website. We sincerely regret this inconvenience.

Back to Results
Methods for reducing blade passing frequency noise generated by rotor-wake - stator interactionA theoretical model for the generation of blade-passage noise caused by the interaction of rotor wakes with the downstream stator blades in a fan stage has been compiled. This model has combined a description of the rotor wake based on existing experimental correlations with an existing theory for the response of the stator blades to those wakes. This model of the interaction-caused blade-passage noise has been used to examine some effects of blade geometry and flow conditions on the noise generated. A set of significant parameters has been identified to reduce this interaction-caused blade-passage frequency noise. A redesign of an existing fan with the use of these concepts has produced a theoretical noise reduction of more than 7 decibels.
Document ID
19730003070
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Dittmar, J. H.
(NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 2, 2013
Publication Date
November 1, 1972
Subject Category
Propulsion Systems
Report/Patent Number
NASA-TM-X-2669
E-7066
Report Number: NASA-TM-X-2669
Report Number: E-7066
Accession Number
73N11797
Funding Number(s)
PROJECT: RTOP 501-04
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available