Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model / / Jeffrey T. Csank and Thomas J. Stueber
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| Autore: |
Csank Jeffrey T.
|
| Titolo: |
Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model / / Jeffrey T. Csank and Thomas J. Stueber
|
| Pubblicazione: | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2013] |
| Descrizione fisica: | 1 online resource (12 pages) : illustrations |
| Soggetto topico: | Inlet flow |
| Controllers | |
| Feedback control | |
| Computerized simulation | |
| Turbine engines | |
| Engine inlets | |
| Persona (resp. second.): | StueberThomas J. |
| Note generali: | Title from title screen (viewed Nov. 13, 2013). |
| "May 2013." | |
| Nota di bibliografia: | Includes bibliographical references (pages 11-12). |
| Titolo autorizzato: | Advanced shock position control for mode transition in a turbine based combined cycle engine inlet model |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910704816803321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |