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Calibration for thrust and airflow measurements in the CE-22 Advanced Nozzle Test Facility [[electronic resource] /] / Roger A. Werner and John D. Wolter
| Calibration for thrust and airflow measurements in the CE-22 Advanced Nozzle Test Facility [[electronic resource] /] / Roger A. Werner and John D. Wolter |
| Autore | Werner Roger A |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
| Descrizione fisica | 1 online resource (49 pages) : illustrations, color |
| Altri autori (Persone) | WolterJohn D |
| Collana | NASA/TM |
| Soggetto topico |
Nozzle thrust coefficients
Discharge coefficient Nozzle flow Calibrating Choked flow Thrust measurement Test facilities Pressure ratio Inlet pressure |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910700371003321 |
Werner Roger A
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner [[electronic resource] /] / Dorothy G. Arbiter
| An investigation at static conditions of nonaxisymmetric nozzle thrust reverser port geometry including effects of rounding and rotating the port corner [[electronic resource] /] / Dorothy G. Arbiter |
| Autore | Arbiter Dorothy G |
| Pubbl/distr/stampa | Hampton, Va. : , : Vigyan Research Associates, Inc. : , : National Aeronautics and Space Administration, Langley Research Center, , [1985] |
| Descrizione fisica | 1 volume : PDF file |
| Collana | NASA contractor report |
| Soggetto topico |
Axisymmetric bodies
Investigation Nozzle thrust coefficients Ports (openings) Rotating cylinders Static tests Thrust reversal Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910699288403321 |
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Arbiter Dorothy G
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| Hampton, Va. : , : Vigyan Research Associates, Inc. : , : National Aeronautics and Space Administration, Langley Research Center, , [1985] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure / / M. Moin Hussaini and John J. Korte
| Investigation of low-Reynolds-number rocket nozzle design using PNS-based optimization procedure / / M. Moin Hussaini and John J. Korte |
| Autore | Hussaini M. Moin |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 1996 |
| Descrizione fisica | 1 online resource (12 pages) : illustrations |
| Collana | NASA technical memorandum |
| Soggetto topico |
Computational fluid dynamics
Navier-Stokes equation Nozzle design Rocket nozzles Low Reynolds number Nozzle thrust coefficients |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Investigation of low Reynolds number rocket nozzle design using parabolized Navier-Stokes based optimization procedure |
| Record Nr. | UNINA-9910707911603321 |
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Hussaini M. Moin
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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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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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Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability / / Mary L. Mason and James R. Burley II
| Static investigation of two STOL nozzle concepts with pitch thrust-vectoring capability / / Mary L. Mason and James R. Burley II |
| Autore | Mason Mary L. |
| Pubbl/distr/stampa | Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , April 1986 |
| Descrizione fisica | 1 online resource (54 pages) : illustrations |
| Collana | NASA/TP |
| Soggetto topico |
Nozzle geometry
Static tests Nozzle thrust coefficients Axisymmetric flow Afterburning Jet nozzles - Testing Airplanes - Motors - Thrust Pitching (Aerodynamics) Short take-off and landing aircraft |
| Soggetto genere / forma | Online resources. |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910709724803321 |
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Mason Mary L.
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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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