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14- by 22-foot subsonic tunnel laser velocimeter upgrade / / James F. Meyers [and three others]
14- by 22-foot subsonic tunnel laser velocimeter upgrade / / James F. Meyers [and three others]
Autore Meyers James F.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2012
Descrizione fisica 1 online resource (793 unnumbered pages) : illustrations (some color)
Collana NASA/TM
Soggetto topico Analog to digital converters
Laser doppler velocimeters
Subsonic wind tunnels
Wind tunnel tests
Data acquisition
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Fourteen by twenty two-foot subsonic tunnel laser velocimeter upgrade
Record Nr. UNINA-9910704474203321
Meyers James F.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2012
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Data reduction functions for the Langley 14- by 22-foot subsonic tunnel / / Andy D. Boney
Data reduction functions for the Langley 14- by 22-foot subsonic tunnel / / Andy D. Boney
Autore Boney Andy D.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2014
Descrizione fisica 1 online resource (iii, 77 pages)
Collana NASA/TM
Soggetto topico Data reduction
Subsonic wind tunnels
Flowmeters
Jet exhaust
Wall pressure
Loads (forces)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910702734603321
Boney Andy D.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , August 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Experimental investigation of an ejector-powered free-jet facility [[electronic resource] /] / Mary Jo Long
Experimental investigation of an ejector-powered free-jet facility [[electronic resource] /] / Mary Jo Long
Autore Long Mary Jo
Pubbl/distr/stampa [Washington, D.C.] : , : [National Aeronautics and Space Administration], , [1992]
Descrizione fisica 1 online resource (13 pages) : digital, PDF file
Collana NASA technical memorandum
Soggetto topico Aircraft noise
Ejectors
Engine noise
Exhaust nozzles
Free jets
Subsonic wind tunnels
Test facilities
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910699534103321
Long Mary Jo  
[Washington, D.C.] : , : [National Aeronautics and Space Administration], , [1992]
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Ice accretions and full-scale iced aerodynamic performance data for a two-dimensional NACA 23012 airfoil / / Harold E. Addy, Jr. [and six others]
Ice accretions and full-scale iced aerodynamic performance data for a two-dimensional NACA 23012 airfoil / / Harold E. Addy, Jr. [and six others]
Autore Addy Harold E., Jr., <1960->
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2016
Descrizione fisica 1 online resource (iv, 437 pages) : color illustrations
Collana NASA/TP
Soggetto topico Aerodynamics
Airfoils
Ice formation
Low Reynolds number
Subsonic wind tunnels
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707967503321
Addy Harold E., Jr., <1960->  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , April 2016
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Low-speed stability-and-control and ground-effects measurements on the industry reference high speed civil transport / / Guy T. Kemmerly [and three others]
Low-speed stability-and-control and ground-effects measurements on the industry reference high speed civil transport / / Guy T. Kemmerly [and three others]
Autore Kennerly Guy T.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999
Descrizione fisica 1 online resource (28 pages, 154 unnumbered pages) : illustrations
Collana NASA/TM
Soggetto topico Civil aviation
High speed
Subsonic wind tunnels
Ground effect (aerodynamics)
Low speed stability
Control surfaces
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706120003321
Kennerly Guy T.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration / / Bryan A. Campbell [and three others]
Subsonic investigation of leading-edge flaps designed for vortex- and attached-flow on a high-speed civil transport configuration / / Bryan A. Campbell [and three others]
Autore Campbell Bryan A.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999
Descrizione fisica 1 online resource (103 pages) : illustrations
Collana NASA/TM
Soggetto topico Subsonic wind tunnels
Leading edge flaps
Vortices
Supersonic transports
Aerodynamic configurations
Separated flow
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706120203321
Campbell Bryan A.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Using pressure sensitive paint to measure aerodynamic forces on a rotor blade in hover / / Anthony Neal Watkins [and five others]
Using pressure sensitive paint to measure aerodynamic forces on a rotor blade in hover / / Anthony Neal Watkins [and five others]
Autore Watkins Anthony Neal
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 2018
Descrizione fisica 1 online resource (52 pages) : color illustrations
Collana NASA/TM
Soggetto topico Aerodynamic forces
Rotary wing aircraft
Hovering
Subsonic wind tunnels
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910711533403321
Watkins Anthony Neal  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , October 2018
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Wind tunnel test of a risk-reduction wing/fuselage model to examine juncture-flow phenomena / / Michael A. Kegerise and Dan H. Neuhart
Wind tunnel test of a risk-reduction wing/fuselage model to examine juncture-flow phenomena / / Michael A. Kegerise and Dan H. Neuhart
Autore Kegerise Michael A.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , November 2016
Descrizione fisica 1 online resource (118 pages) : color illustrations
Collana NASA/TM
Soggetto topico Body-wing configurations
Flow distribution
Laser doppler velocimeters
Reynolds number
Subsonic wind tunnels
Wind tunnel models
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707928203321
Kegerise Michael A.  
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