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Noise computation of a shock-containing supersonic axisymmetric jet by the CE/SE method / Ching Y. Loh [and three others].

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U.S. Government Documents Available online

U.S. Government Documents
Format:
Book
Government document
Author/Creator:
Loh, Ching Y. (Ching Yuen), 1944- author.
Contributor:
NASA Glenn Research Center, issuing body.
Series:
NASA technical memorandum ; 1999-209658.
NASA/TM ; 1999-209658
Language:
English
Genre:
Online resources.
Physical Description:
1 online resource (16 pages) : illustrations.
Other Title:
Noise computation of a shock-containing supersonic axisymmetric jet by the conservation element solution element method
Place of Publication:
Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, December 1999.
Notes:
"December 1999."
"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
Includes bibliographical references (pages 8-9).
Online resource; title from PDF title page (NASA, viewed Sep. 14, 2017).
"AIAA-2000-0475."
Other Format:
Microfiche version: Noise computation of a shock-containing supersonic axisymmetric jet by the CE/SE method
OCLC:
1003640882

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