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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  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , May 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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.  
Moffett Field, CA : , : National Aeronautics and Space Administration, Ames Research Center, , February 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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)  
Moffett Field, CA : , : National Aeronautics and Space Administration, Ames Research Center, , February 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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.)  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , September 2015
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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  
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [2010]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui