Applying pressure sensitive paint technology to rotor blades / / A. Neal Watkins [and five others]
| Applying pressure sensitive paint technology to rotor blades / / A. Neal Watkins [and five others] |
| Autore | Watkins A. Neal |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2014 |
| Descrizione fisica | 1 online resource (36 pages) : illustrations (some color) |
| Collana | NASA/TM |
| Soggetto topico |
Pressure sensitive paints
Horizontal flight Rotor blades (turbomachinery) Rotary wing aircraft Pressure measurement |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702505803321 |
Watkins A. Neal
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2014 | ||
| Lo trovi qui: Univ. Federico II | ||
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Assessment of JVX proprotor performance data in hover and airplane-mode flight conditions / / C.W. Acree, Jr
| Assessment of JVX proprotor performance data in hover and airplane-mode flight conditions / / C.W. Acree, Jr |
| Autore | Acree C. W. |
| Pubbl/distr/stampa | Moffett Field, CA : , : National Aeronautics and Space Administration, Ames Research Center, , February 2016 |
| Descrizione fisica | 1 online resource (89 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Buffeting
Dynamic pressure Pressure sensitive paints Unsteady aerodynamics Vortex shedding |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Assessment of joint vertical experimental proprotor performance data in hover and airplane-mode flight conditions |
| Record Nr. | UNINA-9910707253903321 |
Acree C. W.
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| Moffett Field, CA : , : National Aeronautics and Space Administration, Ames Research Center, , February 2016 | ||
| Lo trovi qui: Univ. Federico II | ||
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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]
| 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] |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] |
| Descrizione fisica | 1 online resource (18 pages) : color illustrations |
| Altri autori (Persone) | WatkinsAnthony Neal |
| Collana | NASA/TM |
| Soggetto topico |
Pressure measurement
Pressure sensitive paints Flow distribution Flight simulation Pressure sensors Horizontal flight Blade tips |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Deployment of a pressure sensitive paint system for measuring global surface pressures on rotorcraft blades in simulated forward flight |
| Record Nr. | UNINA-9910701779103321 |
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] | ||
| Lo trovi qui: Univ. Federico II | ||
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Experimental verification of buffet calculation procedure using unsteady PSP / / Jayanta Panda
| Experimental verification of buffet calculation procedure using unsteady PSP / / Jayanta Panda |
| Autore | Panda J (Jayanta) |
| Pubbl/distr/stampa | Moffett Field, CA : , : National Aeronautics and Space Administration, Ames Research Center, , February 2016 |
| Descrizione fisica | 1 online resource (19 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Buffeting
Dynamic pressure Pressure sensitive paints Unsteady aerodynamics Vortex shedding |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Experimental verification of buffet calculation procedure using unsteady pressure sensitive paint |
| Record Nr. | UNINA-9910707195003321 |
Panda J (Jayanta)
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| Moffett Field, CA : , : National Aeronautics and Space Administration, Ames Research Center, , February 2016 | ||
| Lo trovi qui: Univ. Federico II | ||
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Investigation of unsteady pressure-sensitive paint (uPSP) and a dynamic loads balance to predict launch vehicle buffet environments / / David M. Schuster [and ten others]
| Investigation of unsteady pressure-sensitive paint (uPSP) and a dynamic loads balance to predict launch vehicle buffet environments / / David M. Schuster [and ten others] |
| Autore | Schuster D. M (David M.) |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 2016 |
| Descrizione fisica | 1 online resource (97 pages) : color illustrations. |
| Collana | NASA/TM |
| Soggetto topico |
Buffeting
Dynamic loads Launch vehicles Pressure sensitive paints Spacecraft launching Unsteady flow Wind tunnel tests |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Investigation of unsteady pressure-sensitive paint |
| Record Nr. | UNINA-9910707921103321 |
Schuster D. M (David M.)
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 2016 | ||
| Lo trovi qui: Univ. Federico II | ||
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Measuring global surface pressures on a circulation control concept using pressure sensitive paint [[electronic resource] /] / Anthony Neal Watkins ... [and others]
| Measuring global surface pressures on a circulation control concept using pressure sensitive paint [[electronic resource] /] / Anthony Neal Watkins ... [and others] |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] |
| Descrizione fisica | 1 online resource (28 pages) : illustrations (some color) |
| Altri autori (Persone) | WatkinsAnthony Neal |
| Collana | NASA/TM |
| Soggetto topico |
Pressure
Pressure sensitive paints Computational fluid dynamics Transonic wind tunnels Wings Atmospheric circulation Fabrication Aircraft models |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910702247203321 |
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2012] | ||
| Lo trovi qui: Univ. Federico II | ||
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Pressure- and temperature-sensitive paint at 0.3-m transonic cryogenic tunnel / / A. Neal Watkins [and three others]
| Pressure- and temperature-sensitive paint at 0.3-m transonic cryogenic tunnel / / A. Neal Watkins [and three others] |
| Autore | Watkins A. Neal |
| Pubbl/distr/stampa | Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2015 |
| Descrizione fisica | 1 online resource (20 pages) : color illustrations |
| Collana | NASA/TM |
| Soggetto topico |
Cryogenics
Pressure sensitive paints Temperature sensitive paints Transonic wind tunnels Laminar flow airfoils |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910704157203321 |
Watkins A. Neal
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| Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2015 | ||
| Lo trovi qui: Univ. Federico II | ||
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Results from a pressure sensitive paint test conducted at the National Transonic Facility on test 197 [[electronic resource] ] : the common research model / / A Neal Watkins ... [and others]
| Results from a pressure sensitive paint test conducted at the National Transonic Facility on test 197 [[electronic resource] ] : the common research model / / A Neal Watkins ... [and others] |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] |
| Descrizione fisica | 1 online resource (17 pages) : color illustrations |
| Altri autori (Persone) | WatkinsA. Neal |
| Collana | NASA/TM |
| Soggetto topico |
Cryogenics
Pressure sensitive paints Lessons learned |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Altri titoli varianti | Results from a pressure sensitive paint test conducted at the National Transonic Facility on test 197 |
| Record Nr. | UNINA-9910700812203321 |
| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2011] | ||
| Lo trovi qui: Univ. Federico II | ||
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Unified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields [[electronic resource] /] / Gary E. Erickson
| Unified application of vapor screen flow visualization and pressure sensitive paint measurement techniques to vortex- and shock wave-dominated flow fields [[electronic resource] /] / Gary E. Erickson |
| Autore | Erickson Gary E |
| Pubbl/distr/stampa | Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2010] |
| Descrizione fisica | 1 online resource (v, 32 pages) : illustrations |
| Collana | NASA/TM- |
| Soggetto topico |
Aerodynamic configurations
Pressure sensitive paints Flow visualization Shock waves Static pressure Leading edges Angle of attack |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910697041803321 |
Erickson Gary E
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| Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2010] | ||
| Lo trovi qui: Univ. Federico II | ||
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