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Investigation of flow separation in a transonic-fan linear cascade using visualization methods / / Jan Lepicovsky [and four others]
| Investigation of flow separation in a transonic-fan linear cascade using visualization methods / / Jan Lepicovsky [and four others] |
| Autore | Lepicovsky Jan |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2000 |
| Descrizione fisica | 1 online resource (13 pages) : illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Transonic flutter
Flow visualization Supersonic flow Boundary layer separation |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910706207503321 |
Lepicovsky Jan
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , December 2000 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Methodology of blade unsteady pressure measurement in the NASA transonic flutter cascade / / J. Lepicovsky [and four others]
| Methodology of blade unsteady pressure measurement in the NASA transonic flutter cascade / / J. Lepicovsky [and four others] |
| Autore | Lepicovsky Jan |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2002 |
| Descrizione fisica | 1 online resource (49 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Transonic flutter
Unsteady aerodynamics Rotary wings Computerized simulation Wind tunnels Pressure measurement Data integration |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705661603321 |
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Lepicovsky Jan
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2002 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method / / John W. Edwards
| Transonic shock oscillations and wing flutter calculated with an interactive boundary layer coupling method / / John W. Edwards |
| Autore | Edwards John W. |
| Pubbl/distr/stampa | [Washington, DC] : , : [National Aeronautics and Space Administration], , [1996] |
| Descrizione fisica | 1 online resource (16 pages) : illustrations |
| Collana | NASA-TM |
| Soggetto topico |
Separated flow
Transonic flow Transonic flutter Transonic speed Unsteady flow Viscous flow Computational fluid dynamics Coupling Airfoils Mach number Boundary layer separation Airfoil oscillations |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705776803321 |
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Edwards John W.
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| [Washington, DC] : , : [National Aeronautics and Space Administration], , [1996] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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