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The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor / / Richard F. Bozak, Christopher E. Hughes, James Buckley
| The aerodynamic performance of an over-the-rotor liner with circumferential grooves on a high bypass ratio turbofan rotor / / Richard F. Bozak, Christopher E. Hughes, James Buckley |
| Autore | Bozak Richard F. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , August 2013 |
| Descrizione fisica | 1 online resource (8 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Acoustic properties
Aerodynamic noise Blade tips Oscillating flow Pressure ratio Turbofans Rotors |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705296503321 |
Bozak Richard F.
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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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Inlet acoustic data from a high bypass ratio turbofan rotor in an internal flow component test facility / / Richard F. Bozak
| Inlet acoustic data from a high bypass ratio turbofan rotor in an internal flow component test facility / / Richard F. Bozak |
| Autore | Bozak Richard F. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , May 2017 |
| Descrizione fisica | 1 online resource (6 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Acoustic properties
Aerodynamic characteristics Bypass ratio Noise reduction Rotors Turbofan engines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910705713903321 |
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Bozak Richard F.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , May 2017 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Orifice mass flow calculation in NASA's W-8 single stage axial compressor facility / / Richard F. Bozak
| Orifice mass flow calculation in NASA's W-8 single stage axial compressor facility / / Richard F. Bozak |
| Autore | Bozak Richard F. |
| Pubbl/distr/stampa | Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2018 |
| Descrizione fisica | 1 online resource (28 pages) : illustrations (mostly color) |
| Collana | NASA/TM |
| Soggetto topico |
Mass flow
Orifice flow Turbocompressors Discharge coefficient Static pressure |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Orifice mass flow calculation in NASA's W 8 single stage axial compressor facility |
| Record Nr. | UNINA-9910706861803321 |
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Bozak Richard F.
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| Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2018 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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