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Record Nr. |
UNINA9910699548503321 |
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Autore |
Castner Raymond S |
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Titolo |
Slot nozzle effects for reduced sonic boom on a generic supersonic wing section [[electronic resource] /] / Raymond S. Castner ; prepared for the 48th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics Orlando, Florida, January 4-7, 2010 |
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Pubbl/distr/stampa |
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
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Descrizione fisica |
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1 online resource (10 pages) : illustrations |
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Collana |
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Soggetti |
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Exhaust nozzles |
Sonic booms |
Wing slots |
Aircraft control |
Computational fluid dynamics |
Exhaust gases |
Supersonic speed |
Mach number |
High aspect ratio |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Title from title screen (viewed on Oct. 7, 2010). |
"March 2010." |
"AIAA-2010-1386." |
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Nota di bibliografia |
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Includes bibliographical references (page 10) |
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