Cover Image

Noise computation of a shock-containing supersonic axisymmetric jet by the CE/SE method /

Bibliographic Details
Main Author: Loh, Ching Y. (Ching Yuen), 1944- (Author)
Format: Government Document eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 1999.
Series:NASA technical memorandum ; 1999-209658.
Subjects:
Supersonic jet flow.
Aeroacoustics.
Jet aircraft noise.
Mechanical shock.
Noise measurement.
Online Access:https://purl.fdlp.gov/GPO/gpo84793
Description
Item Description:"December 1999."
"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
"AIAA-2000-0475."
Physical Description:1 online resource (16 pages) : illustrations.
Bibliography:Includes bibliographical references (pages 8-9).