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Record Nr. |
UNINA9910701779103321 |
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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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Pubbl/distr/stampa |
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Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] |
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Descrizione fisica |
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1 online resource (18 pages) : color illustrations |
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Collana |
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Altri autori (Persone) |
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Soggetti |
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Pressure measurement |
Pressure sensitive paints |
Flow distribution |
Flight simulation |
Pressure sensors |
Horizontal flight |
Blade tips |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Title from title screen (viewed on May 15, 2012). |
"December 2011." |
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Nota di bibliografia |
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Includes bibliographical references (pages 17-18). |
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