Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan / / Christopher E. Hughes, John A. Gazzaniga
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| Autore: |
Hughes Christopher E.
|
| Titolo: |
Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan / / Christopher E. Hughes, John A. Gazzaniga
|
| Pubblicazione: | Cleveland, Ohio : , : National Aeronautics and Space Administration, Langley Research Center, , November 2013 |
| Descrizione fisica: | 1 online resource (22 pages) : color illustrations |
| Soggetto topico: | Aircraft performance |
| Bypass ratio | |
| Fan blades | |
| Fixed wings | |
| Low speed wind tunnels | |
| Noise reduction | |
| Note generali: | Title from title screen (viewed July 9, 2014). |
| "November 2013." | |
| Nota di bibliografia: | Includes bibliographical references (pages 5-6). |
| Titolo autorizzato: | Effect of two advanced noise reduction technologies on the aerodynamic performance of an ultra high bypass ratio fan |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910702436203321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |