Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients / / Bobby W. Sanders

• Autore: Sanders Bobby W.
• Pubblicazione: Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Office, , January 1980
• Descrizione fisica: 1 online resource (iii, 98 pages) : illustrations
• Soggetto topico: Airplanes - Turbojet engines - Air intakes; Airplanes - Motors - Valves; Aerodynamic stability; Bypasses; Propulsion system performance; Supersonic inlets; Turbojet engines; Wind tunnel stability tests
• Note generali: Title from title screen (viewed Sept. 22, 2014).; "January 1980."; "Performing organization, Lewis Research Center"--Technical report documentation page.
• Nota di bibliografia: Includes bibliographical references (pages 27-28).
• Titolo autorizzato: Dynamic response of a Mach 2.5 axisymmetric inlet and turbojet engine with a poppet-valve-controlled inlet-stability bypass system when subjected to internal and external airflow transients
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910702682503321
• Lo trovi qui: Univ. Federico II