Impact of an exhaust throat on semi-idealized rotating detonation engine performance / / Daniel E. Paxson

• Autore: Paxson Daniel E.
• Pubblicazione: Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2016
• Descrizione fisica: 1 online resource (12 pages) : color illustrations
• Soggetto topico: Computational fluid dynamics; Exhaust flow simulation; Fuel flow; Inviscid flow; Propulsion system performance
• Note generali: Title from title screen (viewed on June 8, 2016).; "April 2016."; "Prepared for the Scitech 2016 sponsored by the American Institute of Aeronautics and Astronautics, San Diego, California, January 4-8, 2016."; "AIAA-2016-11647."
• Nota di bibliografia: Includes bibliographical references (pages 11-12).
• Titolo autorizzato: Impact of an exhaust throat on semi-idealized rotating detonation engine performance
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910707267903321
• Lo trovi qui: Univ. Federico II