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Aeroelastic computations of a compressor stage using the harmonic balance method [[electronic resource] /] / T.S.R. Reddy, Milind A. Bakhle ; prepared for the 45th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Denver, Colorado, August 2-5, 2009
| Aeroelastic computations of a compressor stage using the harmonic balance method [[electronic resource] /] / T.S.R. Reddy, Milind A. Bakhle ; prepared for the 45th Joint Propulsion Conference and Exhibit cosponsored by the AIAA, ASME, SAE, and ASEE, Denver, Colorado, August 2-5, 2009 |
| Autore | Reddy T. S. R |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010] |
| Descrizione fisica | 1 online resource (22 pages) : illustrations |
| Altri autori (Persone) | BakhleMilind A |
| Collana | NASA/TM |
| Soggetto topico |
Aeroelasticity
Balance Compressors Computational fluid dynamics Harmonic analysis Three dimensional models Transonic compressors |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910699644203321 |
Reddy T. S. R
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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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Large eddy simulation of transonic flow field in NASA rotor 37 [[electronic resource] /] / Chunill Hah ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009
| Large eddy simulation of transonic flow field in NASA rotor 37 [[electronic resource] /] / Chunill Hah ; prepared for the 47th Aerospace Sciences Meeting sponsored by the American Institute of Aeronautics and Astronautics, Orlando, Florida, January 5-8, 2009 |
| Autore | Hah C |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009] |
| Descrizione fisica | 1 online resource (18 pages) : illustrations |
| Collana | NASA TM- |
| Soggetto topico |
Transonic compressors
Pressure distribution Large eddy simulation Navier-Stokes equation Computational fluid dynamics Flow characteristics Reynolds averaging Separated flow Turbulent flow Boundary layer separation |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910696907703321 |
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Hah C
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2009] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Results of an advanced fan stage operating over a wide range of speed and bypass ratio / / Kenneth L. Suder [and five others]
| Results of an advanced fan stage operating over a wide range of speed and bypass ratio / / Kenneth L. Suder [and five others] |
| Autore | Suder Kenneth L (Kenneth Lee) |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]-[2011] |
| Descrizione fisica | 1 online resource (2 volumes) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aerodynamic stalling
Bypass ratio Computational fluid dynamics Propulsion system configurations Transonic compressors Turbofans Supersonic speed Computerized simulation |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | pt. 1. Fan stage design and experimental results -- pt 2. Comparison of CFD and experimental results. |
| Record Nr. | UNINA-9910700138803321 |
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Suder Kenneth L (Kenneth Lee)
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2010]-[2011] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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