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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 |
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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Impact of an exhaust throat on semi-idealized rotating detonation engine performance / / Daniel E. Paxson
| Impact of an exhaust throat on semi-idealized rotating detonation engine performance / / Daniel E. Paxson |
| Autore | Paxson Daniel E. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2016 |
| Descrizione fisica | 1 online resource (12 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Computational fluid dynamics
Exhaust flow simulation Fuel flow Inviscid flow Propulsion system performance |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707267903321 |
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Paxson Daniel E.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2016 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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