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Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel / / Richard J. Re and Francis J. Capone
| Impingement of boundary-reflected disturbances originating at the nose of a body of revolution in the Langley Research Center 16-foot transonic tunnel / / Richard J. Re and Francis J. Capone |
| Autore | Re Richard J. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 1998 |
| Descrizione fisica | 1 online resource (37 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Supersonic transports
Supersonic speed Static pressure Shock waves Mach number Bow waves Bodies of revolution |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705811003321 |
Re Richard J.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 1998 | ||
| 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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A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 / / Richard J. Re and William K. Abeyounis
| A wind tunnel investigation of three NACA 1-series inlets at Mach numbers up to 0.92 / / Richard J. Re and William K. Abeyounis |
| Autore | Re Richard J. |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 1996 |
| Descrizione fisica | 1 online resource (180 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Aircraft engines
Angle of attack Engine inlets Mach number Pressure distribution Subsonic flow Static pressure Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910707910903321 |
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Re Richard J.
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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