Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight / / Scott R. Thomas, H. Douglas Perkins, and Charles J. Trefny

• Autore: Thomas Scott R.
• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Lewis Research Center, , March 1997
• Descrizione fisica: 1 online resource (10 pages) : illustrations
• Soggetto topico: Ejectors; Hydrocarbon fuels; Wind tunnel tests; Supersonic speed; Mach number; Engine tests; Propulsion system performance; Flow distribution
• Persona (resp. second.): PerkinsH. Douglas; TrefnyCharles J.
• Note generali: "March 1997"--Report documentation page.; "Prepared for the 89th Symposium sponsored by the Propulsion and Energetics Panel of the NATO Advisory Group for Aerospace Research and Development, Palaiseau, France, April 14-17, 1997."; "Performing organization: National Aeronautics and Space Administration, Lewis Research Center"--Report documentation page.
• Nota di bibliografia: Includes bibliographical references (page 4).
• Titolo autorizzato: Evaluation of an ejector ramjet based propulsion system for air-breathing hypersonic flight
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910707625903321
• Lo trovi qui: Univ. Federico II