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Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine / / Daniel E. Paxson [and three others]
| Comparison of numerically simulated and experimentally measured performance of a rotating detonation engine / / Daniel E. Paxson [and three others] |
| Autore | Paxson Daniel E. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2015 |
| Descrizione fisica | 1 online resource (10 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Detonation
Computational fluid dynamics Inlet flow Convergent-divergent nozzles Potential flow |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704025303321 |
Paxson Daniel E.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed / / Daniel S. Jones [and four others]
| Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed / / Daniel S. Jones [and four others] |
| Autore | Jones Daniel S. |
| Pubbl/distr/stampa | Edwards, CA : , : National Aeronautics and Space Administration, Armstrong Flight Research Center, , October 2014 |
| Descrizione fisica | 1 online resource (25 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Convergent-divergent nozzles
Flow distribution Inviscid flow Nozzle design Rocket nozzles |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910703728303321 |
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Jones Daniel S.
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| Edwards, CA : , : National Aeronautics and Space Administration, Armstrong Flight Research Center, , October 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles / / Jeffery A. Yetter, Laurance D. Leavitt
| Effects of sidewall geometry on the installed performance of nonaxisymmetric convergent-divergent exhaust nozzles / / Jeffery A. Yetter, Laurance D. Leavitt |
| Autore | Yetter Jeffery A. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 |
| Descrizione fisica | 1 online resource (116 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Convergent-divergent nozzles
Exhaust flow simulation Nozzle design Static pressure Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707455003321 |
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Yetter Jeffery A.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Exhaust nozzle plume and shock wave interaction / / Raymond S. Castner, Alaa Elmiligui, Susan Cliff
| Exhaust nozzle plume and shock wave interaction / / Raymond S. Castner, Alaa Elmiligui, Susan Cliff |
| Autore | Castner Raymond S. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013 |
| Descrizione fisica | 1 online resource (21 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Shock wave interaction Convergent-divergent nozzles Sonic booms |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704910603321 |
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Castner Raymond S.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft / / Bobby L. Berrier and Richard J. Re
| Investigation of convergent-divergent nozzles applicable to reduced-power supersonic cruise aircraft / / Bobby L. Berrier and Richard J. Re |
| Autore | Berrier Bobby L. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 |
| Descrizione fisica | 1 online resource (215 pages) : chiefly illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Convergent-divergent nozzles
Mach number Nozzle design Performance tests Pressure ratio |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707455903321 |
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Berrier Bobby L.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , December 1980 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf / / Milton Lamb and John G. Taylor, Mark C. Frassinelli
| Static internal performance of a two-dimensional convergent-divergent nozzle with external shelf / / Milton Lamb and John G. Taylor, Mark C. Frassinelli |
| Autore | Lamb Milton |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 1996 |
| Descrizione fisica | 1 online resource (iii, 103 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Convergent-divergent nozzles
Two dimensional flow Two dimensional models Transonic wind tunnels Trailing edges |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704399403321 |
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Lamb Milton
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles / / Mary L. Mason and Bobby L. Berrier
| Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles / / Mary L. Mason and Bobby L. Berrier |
| Autore | Mason Mary L. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , June 1985 |
| Descrizione fisica | 1 online resource (216 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Static tests
Thrust vector control Convergent-divergent nozzles Yaw Wind tunnel tests Jet nozzles - Testing Yawing (Aerodynamics) Airplanes - Motors - Thrust |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709791903321 |
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Mason Mary L.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , June 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Transonic investigation of two-dimensional nozzles designed for supersonic cruise / / Francis J. Capone and Karen A. Deere
| Transonic investigation of two-dimensional nozzles designed for supersonic cruise / / Francis J. Capone and Karen A. Deere |
| Autore | Capone Francis J. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2015 |
| Descrizione fisica | 1 online resource (iii, 311 pages) : color illustration |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Pressure drag Convergent-divergent nozzles Transonic nozzles Reynolds stress |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704024703321 |
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Capone Francis J.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2015 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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