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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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Pubblicazione: | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2001 |
Descrizione fisica: | 1 online resource (18 pages) : illustrations |
Soggetto topico: | Air breathing boosters |
Hypersonic speed | |
Computational fluid dynamics | |
Wind tunnel tests | |
Propulsion | |
Pressure distribution | |
Persona (resp. second.): | TrefnyCharles J. |
Note generali: | "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. | |
Nota di bibliografia: | Includes bibliographical references (page 5). |
Altri titoli varianti: | Supersonic wind tunnel tests of a half-axisymmetric 12 degree spike inlet to a rocket-based combined-cycle propulsion system |
Titolo autorizzato: | Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system ![]() |
Formato: | Materiale a stampa ![]() |
Livello bibliografico | Monografia |
Lingua di pubblicazione: | Inglese |
Record Nr.: | 9910706590803321 |
Lo trovi qui: | Univ. Federico II |
Opac: | Controlla la disponibilità qui |