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Record Nr. |
UNINA9910704671703321 |
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Autore |
Foster Lancert E. |
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Titolo |
Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion / / Lancert E. Foster [and three others] |
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Pubbl/distr/stampa |
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012 |
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Descrizione fisica |
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1 online resource (13 pages) : illustrations (some color) |
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Collana |
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Soggetti |
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Engine inlets |
Hypersonic flight |
Supersonic speed |
Air breathing engines |
Supersonic combustion ramjet engines |
Specific impulse |
Propulsion system configurations |
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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 July 12, 2013). |
"December 2012." |
"Prepared for the Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, ASEE, Atlanta, Geogria, July 30 to August 1, 2012." |
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Nota di bibliografia |
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Includes bibliographical references (page 13). |
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