Exhaust plume effects on sonic boom for a delta wing and a swept wing-body model /

Bibliographic Details
Main Author: Castner, Raymond
Corporate Authors: NASA Glenn Research Center, AIAA Aerospace Sciences Meeting
Other Authors: Lake, Troy
Format: Government Document Conference Proceeding eBook
Language:English
Published: Cleveland, Ohio : National Aeronautics and Space Administration, Glenn Research Center, [2012]
Series:NASA technical memorandum ; 2012-217446.
Subjects:
Online Access:https://purl.fdlp.gov/GPO/gpo30596

MARC

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245 1 0 |a Exhaust plume effects on sonic boom for a delta wing and a swept wing-body model /  |c Raymond Castner, Troy Lake. 
264 1 |a Cleveland, Ohio :  |b National Aeronautics and Space Administration, Glenn Research Center,  |c [2012] 
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500 |a Title from title screen (viewed on Oct. 29, 2012). 
500 |a "April 2012." 
500 |a "Prepared for the 50th Aerospace Science Conference sponsored by the American Institute of Aeronautics and Astronautics Nashville, Tennessee, January 9-12, 2012." 
504 |a Includes bibliographical references (page 13). 
500 |a "AIAA-2012-1033." 
536 |a Sponsored by National Aeronautics and Space Administration  |h WBS 984754.02.07.03.13.02 
536 |d E-18176 
500 |a Electronic resource. 
650 7 |a Exhaust gases.  |2 nasat 
650 7 |a Exhaust nozzles.  |2 nasat 
650 7 |a Pressure distribution.  |2 nasat 
650 7 |a Sonic booms.  |2 nasat 
650 7 |a Body-wing configurations.  |2 nasat 
650 7 |a Plumes.  |2 nasat 
700 1 |a Lake, Troy. 
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