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Autore: |
Csank Jeffrey T.
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Titolo: |
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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Pubblicazione: | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013 |
Descrizione fisica: | 1 online resource (17 pages) : color illustrations |
Soggetto topico: | Computerized simulation |
Engine inlets | |
Feedback control | |
Inlet flow | |
Turbine engines | |
Persona (resp. second.): | StueberThomas J. |
Note generali: | Title from title screen (viewed on Feb. 6, 2014). |
"January 2013." | |
"Prepared for the 45th Combustion/33rd Airbreathing Propulsion/33rd Exhaust Plume and Signatures/27th Propulsion Hazards Joint Subcommittee Meeting sponsored by the Joint Army-Navy-NASA-Air Force (JANNAF), Monterey, California, December 3-7, 2012." | |
Nota di bibliografia: | Includes bibliographical references (pages 16-17). |
Titolo autorizzato: | 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.: | 9910704622203321 |
Lo trovi qui: | Univ. Federico II |
Opac: | Controlla la disponibilità qui |