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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.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Office, , January 1980 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane / / Donald L. Hughes, Lawrence P. Myers, and Karen G. Mackall
| Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane / / Donald L. Hughes, Lawrence P. Myers, and Karen G. Mackall |
| Autore | Hughes Donald L (Donald Lee), <1926-> |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , 1985 |
| Descrizione fisica | 1 online resource (20 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Static pressure
Aircraft engines Inlet flow Flight tests Pressure measurement Static pressure probes - Testing Airplanes - Turbojet engines - Air intakes Eagle (Jet fighter plane) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709611203321 |
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Hughes Donald L (Donald Lee), <1926->
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A mathematical analysis of supersonic inlet dynamics / / by Ross G. Willoh
| A mathematical analysis of supersonic inlet dynamics / / by Ross G. Willoh |
| Autore | Willoh Ross G. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, , December 1968 |
| Descrizione fisica | 1 online resource (ii, 41 pages) : illustrations |
| Collana | NASA/TN |
| Soggetto topico |
Aerodynamics
Air ducts Applications of mathematics Aerodynamics, Supersonic Air ducts - Aerodynamics Airplanes - Turbojet engines - Air intakes Mathematical analysis |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716078003321 |
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Willoh Ross G.
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| Washington, D.C. : , : National Aeronautics and Space Administration, , December 1968 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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