Info
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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Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap / / Richard J. Re and Laurence D. Leavitt
| Static internal performance of a thrust vectoring and reversing two-dimensional convergent-divergent nozzle with an aft flap / / Richard J. Re and Laurence D. Leavitt |
| Autore | Re Richard J. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 |
| Descrizione fisica | 1 online resource (110 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Static tests
Thrust vector control Thrust reversal Wind tunnel tests Nozzle geometry Jet nozzles Jet planes - Thrust reversers |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709716003321 |
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Re Richard J.
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| Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60° / / Bobby L. Berrier and Laurence D. Leavitt
| Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60° / / Bobby L. Berrier and Laurence D. Leavitt |
| Autore | Berrier Bobby L. |
| Pubbl/distr/stampa | [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , October 1984 |
| Descrizione fisica | 1 online resource (141 pages) : illustrations |
| Collana | NASA technical paper |
| Soggetto topico |
Axisymmetric bodies
Nozzle thrust coefficients Static tests Thrust vector control Transonic wind tunnels Two dimensional flow |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Static internal performance of single -expansion-ramp nozzles with thrust-vectoring capability up to 60 degrees |
| Record Nr. | UNINA-9910707970903321 |
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Berrier Bobby L.
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| [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , October 1984 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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