Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight [[electronic resource] ] : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel / / Anthony Neal Watkins ... [and others]
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| Titolo: |
Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight [[electronic resource] ] : preliminary PSP results from test 581 in the 14- x 22-foot subsonic tunnel / / Anthony Neal Watkins ... [and others]
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| Pubblicazione: | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] |
| Descrizione fisica: | 1 online resource (18 pages) : color illustrations |
| Soggetto topico: | Pressure measurement |
| Pressure sensitive paints | |
| Flow distribution | |
| Flight simulation | |
| Pressure sensors | |
| Horizontal flight | |
| Blade tips | |
| Altri autori: |
WatkinsAnthony Neal
|
| Note generali: | Title from title screen (viewed on May 15, 2012). |
| "December 2011." | |
| Nota di bibliografia: | Includes bibliographical references (pages 17-18). |
| Altri titoli varianti: | Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight |
| Titolo autorizzato: | Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910701779103321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |