Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system / / J.R. DeBonis and C.J. Trefny

• Autore: DeBonis James R.
• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2001
• Descrizione fisica: 1 online resource (18 pages) : illustrations
• Soggetto topico: Air breathing boosters; Hypersonic speed; Computational fluid dynamics; Wind tunnel tests; Propulsion; Pressure distribution
• Persona (resp. second.): TrefnyCharles J.
• Note generali: "February 2001."; "Prepared for the 37th Combustion Subcommittee, 25th Airbreathing Propulsion Subcommittee, and 19th Propulsion Systems Hazards Subcommittee Joint Meeting sponsored by the Joint Army-Navy-Air Force Interagency Propulsion Committee, Monterey, California, November 13-17, 2000."; "Performing organization: National Aeronautics and Space Administration, John H. Glenn Research Center at Lewis Field"--Report documentation page.
• Nota di bibliografia: Includes bibliographical references (page 5).
• Altri titoli varianti: Supersonic wind tunnel tests of a half-axisymmetric 12 degree spike inlet to a rocket-based combined-cycle propulsion system
• Titolo autorizzato: Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910706590803321
• Lo trovi qui: Univ. Federico II