A turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool / / Jeffrey T. Csank and Thomas J. Stueber
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| Autore: |
Csank Jeffrey T.
|
| Titolo: |
A turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool / / Jeffrey T. Csank and Thomas J. Stueber
|
| Pubblicazione: | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012 |
| Descrizione fisica: | 1 online resource (13 pages) : color illustrations |
| Soggetto topico: | Computerized simulation |
| Propulsion system configurations | |
| Wind tunnel tests | |
| Fuel systems | |
| Propulsion system performance | |
| Turbine engines | |
| Engine inlets | |
| Persona (resp. second.): | StueberThomas J. |
| Note generali: | Title from title screen (viewed on Jan. 14, 2013). |
| "September 2012." | |
| "Prepared for the 48th Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, and ASEE Atlanta, Georgia, July 30 to August 1, 2012." | |
| "AIAA-2012-4149." | |
| Nota di bibliografia: | Includes bibliographical references (pages 12-13). |
| Titolo autorizzato: | A turbine based combined cycle engine inlet model and mode transition simulation based on HiTECC tool |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910702486003321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |