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Record Nr. |
UNINA9910707267903321 |
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Autore |
Paxson Daniel E. |
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Titolo |
Impact of an exhaust throat on semi-idealized rotating detonation engine performance / / Daniel E. Paxson |
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Pubbl/distr/stampa |
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2016 |
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Descrizione fisica |
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1 online resource (12 pages) : color illustrations |
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Collana |
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Soggetti |
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Computational fluid dynamics |
Exhaust flow simulation |
Fuel flow |
Inviscid flow |
Propulsion system performance |
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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 June 8, 2016). |
"April 2016." |
"Prepared for the Scitech 2016 sponsored by the American Institute of Aeronautics and Astronautics, San Diego, California, January 4-8, 2016." |
"AIAA-2016-11647." |
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Nota di bibliografia |
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Includes bibliographical references (pages 11-12). |
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