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
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596 |a 1 
650 7 |a Acoustics  |2 nasat 
650 7 |a Aerodynamic noise  |2 nasat 
650 7 |a Engine design  |2 nasat 
650 7 |a Exhaust systems  |2 nasat 
650 7 |a Jet aircraft noise  |2 nasat 
650 7 |a Laser anemometers  |2 nasat 
650 7 |a Laser doppler velocimeters  |2 nasat 
650 7 |a Noise reduction  |2 nasat 
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