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Record Nr. |
UNINA9910704025303321 |
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Autore |
Paxson Daniel E. |
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Titolo |
Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine / / Daniel E. Paxson [and three others] |
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Pubbl/distr/stampa |
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2015 |
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Descrizione fisica |
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1 online resource (10 pages) : color illustrations |
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Collana |
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Soggetti |
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Detonation |
Computational fluid dynamics |
Inlet flow |
Convergent-divergent nozzles |
Potential flow |
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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 Nov. 13, 2015). |
"August 2015." |
"Prepared for SciTech 2015 sponsored by the American Institute of Aeronautics and Astronautics, Kissimmee, Florida, January 5-9, 2015." |
"AIAA-2015-1101." |
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Nota di bibliografia |
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Includes bibliographical references (page 10). |
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