Acoustic and laser doppler anemometer results for confluent, 22-lobed, and unique-lobed mixer exhaust systems for subsonic jet noise reduction

Acoustic and laser doppler anemometer results for confluent, 22-lobed, and unique-lobed mixer exhaust systems for subsonic jet noise reduction

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Bibliographic Details
Corporate Author: NASA Glenn Research Center
Other Authors: Salikuddin, M
Format: Government Document Book
Language:English
Published: [Cleveland, Ohio] : Hanover, MD : National Aeronautics and Space Administration, Glenn Research Center ; Available from NASA Center for Aerospace Information, [2002]
Series:NASA contractor report NASA CR-211598
Subjects:
Acoustics
Aerodynamic noise
Engine design
Exhaust systems
Jet aircraft noise
Laser anemometers
Laser doppler velocimeters
Noise reduction
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Description
Item Description:Shipping list no.: 2003-0340-M
"September 2002."
Physical Description:1 v
Also available via Internet from the NASA web site. Address as of 9/16/03: http://gltrs.grc.nasa.gov/reports/2002/CR-2002-211598.pdf; current access available via PURL

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