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Record Nr. |
UNINA9910706590803321 |
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Autore |
DeBonis James R. |
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Titolo |
Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system / / J.R. DeBonis and C.J. Trefny |
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Pubbl/distr/stampa |
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Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2001 |
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Descrizione fisica |
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1 online resource (18 pages) : illustrations |
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Collana |
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Soggetti |
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Air breathing boosters |
Hypersonic speed |
Computational fluid dynamics |
Wind tunnel tests |
Propulsion |
Pressure distribution |
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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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"February 2001." |
"Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting sponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000." |
"Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page. |
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Nota di bibliografia |
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Includes bibliographical references (page 5). |
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