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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
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.
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Office, , January 1980
Descrizione fisica 1 online resource (iii, 98 pages) : illustrations
Collana NASA technical paper
Soggetto topico Airplanes - Turbojet engines - Air intakes
Airplanes - Motors - Valves
Aerodynamic stability
Bypasses
Propulsion system performance
Supersonic inlets
Turbojet engines
Wind tunnel stability tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702682503321
Sanders Bobby W.  
Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Office, , January 1980
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Evaluation of the low-speed stability and control characteristics of a Mach 5.5 Waverider concept / David E. Hahne
Evaluation of the low-speed stability and control characteristics of a Mach 5.5 Waverider concept / David E. Hahne
Autore Hahne David E (David Edgar)
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1997
Descrizione fisica 1 online resource (23 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Hypersonic vehicles
Hypersonic speed
Stabilizers (fluid dynamics)
Pitching moments
Wind tunnel stability tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910704204903321
Hahne David E (David Edgar)  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 1997
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui