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Record Nr. |
UNINA9910699547103321 |
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Autore |
Castner Raymond S |
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Titolo |
Wind tunnel model design for the study of plume effects on sonic boom for isolated exhaust nozzles [[electronic resource] /] / Raymond S. Castner ; prepared for the 45th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE, Denver, Colorado, August 2-5, 2009 |
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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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Wind tunnel tests |
Supersonic aircraft |
Aerodynamic configurations |
Low cost |
Supersonic wind tunnels |
Wind tunnel models |
Sonic booms |
Static pressure |
Pressure sensors |
Exhaust nozzles |
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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). |
"April 2010." |
"AIAA-2009-5369." |
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Nota di bibliografia |
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Includes bibliographical references (page 10) |
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