Exhaust nozzle plume effects on sonic boom test results for vectored nozzles

Exhaust nozzle plume effects on sonic boom test results for vectored nozzles [electronic resource] / Raymond Castner.

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Bibliographic Details
Online Access: Online Access
Online Access
Main Author: Castner, Raymond S.
Corporate Authors: NASA Glenn Research Center, Joint Propulsion Conference and Exhibit
Format: Government Document Electronic Conference Proceeding eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Series:NASA technical memorandum ; 217229.
Subjects:
Exhaust nozzles.
Sonic booms.
Computational fluid dynamics.
Elastic waves.
Plumes.
F-15 aircraft.
Supersonic aircraft.
Pressure ratio.
Description
Item Description:Title from title screen (viewed on Nov. 1, 2012)
"February 2012."
"Prepared for the 47th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE,San Diego, California, July 31-August 3, 2011."
"AIAA-2011-5974."
Physical Description:1 online resource (16 pages) : color illustrations.
Bibliography:Includes bibliographical references (pages 15-16)

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