Acoustic and laser doppler anemometer results for confluent, 22-lobed, and unique-lobed mixer exhaust systems for subsonic jet noise reduction
By: M. Salikuddin ... [et al.].
Contributors: Salikuddin, M.; NASA Glenn Research Center.
Series: [NASA contractor report] -- NASA/CR-2002-211598.; NASA contractor report -- NASA CR-211598.
Publisher: National Aeronautics and Space Administration, Glenn Research Center; Available from NASA Center for Aerospace Information
Published: 2002
Place of publication: [Cleveland, Ohio]; Hanover, MD
Language: eng
Format: Microform
Subjects: Acoustics.; Laser doppler velocimeters.; Exhaust systems.; Jet aircraft noise.; Engine design.; Noise reduction.; Laser anemometers.; Aerodynamic noise.
Notes: Shipping list no.: 2003-0340-M.

"September 2002."

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.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 2002] 4 microfiches.