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Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade / / Ashlie B. McVetta, Paul W. Giel, Gerard E. Welch
| Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade / / Ashlie B. McVetta, Paul W. Giel, Gerard E. Welch |
| Autore | McVetta Ashlie B. |
| Edizione | [Revised copy.] |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2014 |
| Descrizione fisica | 1 online resource (23 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Supersonic turbines
Turbine blades Aerodynamic heat transfer Computational fluid dynamics Reynolds number Pressure distribution Inlet flow Angles (geometry) |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702656103321 |
McVetta Ashlie B.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , June 2014 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade / / Ashlie B. McVetta, Paul W. Giel, Gerard E. Welch
| Aerodynamic investigation of incidence angle effects in a large scale transonic turbine cascade / / Ashlie B. McVetta, Paul W. Giel, Gerard E. Welch |
| Autore | McVetta Ashlie B. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2013 |
| Descrizione fisica | 1 online resource (18 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aerodynamic heat transfer
Computational fluid dynamics Flow measurement Inlet flow Supersonic turbines Turbine blades |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702431803321 |
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McVetta Ashlie B.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2013 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Modeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas / / Parviz A. Bahrami
| Modeling of aerobrake ballute stagnation point temperature and heat transfer to inflation gas / / Parviz A. Bahrami |
| Autore | Bahrami Parviz A (Parviz Ahmadi) |
| Pubbl/distr/stampa | Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , 2012 |
| Descrizione fisica | 1 online resource (iv, 13 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Aerobraking
Aerocapture Aerodynamic heat transfer Ballutes Drag devices Spacecraft reentry Aerothermodynamics Atmospheric entry Descent trajectories Mathematical models Trajectories |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704472803321 |
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Bahrami Parviz A (Parviz Ahmadi)
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| Moffett Field, California : , : National Aeronautics and Space Administration, Ames Research Center, , 2012 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Results of A M = : 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42) / / by John Marroquin
| Results of A M = : 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel (IH-42) / / by John Marroquin |
| Autore | Marroquin J. |
| Pubbl/distr/stampa | Houston, Texas : , : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, , March 1985 |
| Descrizione fisica | 1 online resource (iii, 27 pages) : illustrations |
| Collana | NASA/CR |
| Soggetto topico |
Aerothermodynamics
Hypersonic heat transfer Aerodynamic heat transfer Hypersonic speed Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Results of A M = 5.3 heat transfer test of the integrated vehicle using phase-change paint techniques on the 0.0175-scale model 56-OTS in the NASA/AMES Research Center 3.5-foot hypersonic wind tunnel |
| Record Nr. | UNINA-9910709972703321 |
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Marroquin J.
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| Houston, Texas : , : Systems Engineering Division, Johnson Space Center, National Aeronautics and Space Administration, , March 1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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