Computational analyses of the LIMX TBCC inlet high-speed flowpath [[electronic resource] /] / Vance F. Dippold, III

• Autore: Dippold Vance
• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2012]
• Descrizione fisica: 1 online resource (26 pages) : color illustrations
• Soggetto topico: Turbine engines; Cycles; Inlet flow; Supersonic combustion ramjet engines; Combustion chambers; High speed; Mass flow rate; Reynolds averaging; Free flow
• Note generali: Title from title screen (viewed on July 9, 2012).; "Prepared for the 58th Joint Army-Navy-NASA-Air Force (JANNAF) Propulsion Meeting sponsored by the JANNAF Interagency Propulsion Committee, Arlington, Virginia, April 18-22, 2011."; "January 2012."
• Nota di bibliografia: Includes bibliographical references (page 9).
• Titolo autorizzato: Computational analyses of the LIMX TBCC inlet high-speed flowpath
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910701830003321
• Lo trovi qui: Univ. Federico II