Shock position control for mode transition in a turbine based combined cycle engine inlet model / / Jeffrey T. Csank and Thomas J. Stueber

• Autore: Csank Jeffrey T.
• 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