Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion / / Lancert E. Foster [and three others]

• Autore: Foster Lancert E.
• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2012
• Descrizione fisica: 1 online resource (13 pages) : illustrations (some color)
• Soggetto topico: Engine inlets; Hypersonic flight; Supersonic speed; Air breathing engines; Supersonic combustion ramjet engines; Specific impulse; Propulsion system configurations
• Note generali: Title from title screen (viewed on July 12, 2013).; "December 2012."; "Prepared for the Joint Propulsion Conference and Exhibit cosponsored by AIAA, ASME, SAE, ASEE, Atlanta, Geogria, July 30 to August 1, 2012."
• Nota di bibliografia: Includes bibliographical references (page 13).
• Titolo autorizzato: Highlights from a Mach 4 experimental demonstration of inlet mode transition for Turbine-Based Combined Cycle hypersonic propulsion
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910704671703321
• Lo trovi qui: Univ. Federico II