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Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles / / Mary L. Mason and Bobby L. Berrier
Static investigation of several yaw vectoring concepts on nonaxisymmetric nozzles / / Mary L. Mason and Bobby L. Berrier
Autore Mason Mary L.
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , June 1985
Descrizione fisica 1 online resource (216 pages) : illustrations
Collana NASA/TP
Soggetto topico Static tests
Thrust vector control
Convergent-divergent nozzles
Yaw
Wind tunnel tests
Jet nozzles - Testing
Yawing (Aerodynamics)
Airplanes - Motors - Thrust
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910709791903321
Mason Mary L.  
Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , June 1985
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations / / Robert W. Hess, F.W. Cazier, and Eleanor C. Wynne
Steady and unsteady transonic pressure measurements on a clipped delta wing for pitching and control-surface oscillations / / Robert W. Hess, F.W. Cazier, and Eleanor C. Wynne
Autore Hess R. W (Robert W.)
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , October 1986
Descrizione fisica 1 online resource (115 pages) : illustrations
Collana NASA/TP
Soggetto topico Steady state
Pressure measurement
Transonic speed
Delta wings
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910709875703321
Hess R. W (Robert W.)  
Washington, D.C. : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , October 1986
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Subsonic aerodynamic characteristics of a circular body Earth-to-orbit vehicle / / Roger A. Lepsch, Jr. and George M. Ware, Ian 0. MacConochie
Subsonic aerodynamic characteristics of a circular body Earth-to-orbit vehicle / / Roger A. Lepsch, Jr. and George M. Ware, Ian 0. MacConochie
Autore Lepsch Roger A.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 1996
Descrizione fisica 1 online resource (29 pages.) : illustrations
Collana NASA technical memorandum
Soggetto topico Wind tunnel tests
Space transportation system
Single stage to orbit vehicles
Reusable spacecraft
Lift drag ratio
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910704399003321
Lepsch Roger A.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , July 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Subsonic dynamics of stardust sample return capsule / / R.A. Mitcheltree and C.M. Fremaux
Subsonic dynamics of stardust sample return capsule / / R.A. Mitcheltree and C.M. Fremaux
Autore Mitcheltree Robert A (Robert Alan), <1961->
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 1997
Descrizione fisica 1 online resource (18 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Dynamic stability
Wind tunnel tests
Stability tests
Atmospheric entry
Space capsules
Landing modules
Aerodynamics
Subsonic speed
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707903503321
Mitcheltree Robert A (Robert Alan), <1961->  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 1997
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Subsonic investigation of a leading-edge boundary layer contol suction system on a high-speed civil transport configuration / / Bryan A. Campbell [and seven others]
Subsonic investigation of a leading-edge boundary layer contol suction system on a high-speed civil transport configuration / / Bryan A. Campbell [and seven 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 (128 pages) : illustrations
Collana NASA/TM
Soggetto topico Boundary layer control
Leading edges
Wind tunnel tests
Flaps (control surfaces)
Pressure effects
Subsonic speed
Supersonic transports
Aerodynamic configurations
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Subsonic investigation of a leading-edge boundary layer control suction system on a high-speed civil transport configuration
Record Nr. UNINA-9910706520903321
Campbell Bryan A.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , December 1999
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Summary of the 2017 blockage test in the 10- by 10-foot supersonic wind tunnel / / Christine Pastor-Barsi, Christopher Peters, and Manan Vyas
Summary of the 2017 blockage test in the 10- by 10-foot supersonic wind tunnel / / Christine Pastor-Barsi, Christopher Peters, and Manan Vyas
Autore Pastor-Barsi Christine <1982->
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2018
Descrizione fisica 1 online resource (19 pages) : illustrations (mostly color)
Collana NASA/TM
Soggetto topico Wind tunnel tests
Blocking
Supersonic wind tunnels
Pressure measurement
Boundary layer thickness
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910711552503321
Pastor-Barsi Christine <1982->  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , October 2018
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Supersonic retropropulsion test 1853 in NASA LaRC Unitary Plan Wind Tunnel test section 2 / / Scott A. Berry and Matthew N. Rhode
Supersonic retropropulsion test 1853 in NASA LaRC Unitary Plan Wind Tunnel test section 2 / / Scott A. Berry and Matthew N. Rhode
Autore Berry Scott A.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2014
Descrizione fisica 1 online resource (xxxvi, 977 pages) : color illustrations
Collana NASA/TP
Soggetto topico Boundary layer separation
Flow distribution
Internal flow
Separated flow
Wind tunnel tests
Forebodies
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Supersonic retropropulsion test 1853 in NASA Langley Research Center Unitary Plan Wind Tunnel test section 2
Record Nr. UNINA-9910702700403321
Berry Scott A.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , April 2014
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system / / J.R. DeBonis and C.J. Trefny
Supersonic wind tunnel tests of a half-axisymmetric 12°-spike inlet to a rocket-based combined-cycle propulsion system / / J.R. DeBonis and C.J. Trefny
Autore DeBonis James R.
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2001
Descrizione fisica 1 online resource (18 pages) : illustrations
Collana NASA/TM
Soggetto topico Air breathing boosters
Hypersonic speed
Computational fluid dynamics
Wind tunnel tests
Propulsion
Pressure distribution
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Supersonic wind tunnel tests of a half-axisymmetric 12 degree spike inlet to a rocket-based combined-cycle propulsion system
Record Nr. UNINA-9910706590803321
DeBonis James R.  
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , February 2001
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Takeoff/approach noise for a model counterrotation propeller with a forward-swept upstream rotor [[electronic resource] /] / Richard P. Woodward, ... [and others]
Takeoff/approach noise for a model counterrotation propeller with a forward-swept upstream rotor [[electronic resource] /] / Richard P. Woodward, ... [and others]
Pubbl/distr/stampa [Cleveland, Ohio] : , : [National Aeronautics and Space Administration, Lewis Research Center], , [1993]
Descrizione fisica 1 online resource (21 pages) : digital, PDF file
Altri autori (Persone) WoodwardRichard P
Collana NASA technical memorandum
Soggetto topico Acoustic properties
Aeroacoustics
Aircraft noise
Approach
Contrarotating propellers
Counter rotation
Sound pressure
Takeoff
Turboprop aircraft
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910699539703321
[Cleveland, Ohio] : , : [National Aeronautics and Space Administration, Lewis Research Center], , [1993]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Three-dimensional flow field measurements in a transonic turbine cascade / / P.W. Giel [and seven others]
Three-dimensional flow field measurements in a transonic turbine cascade / / P.W. Giel [and seven others]
Autore Giel P. W (Paul W.)
Pubbl/distr/stampa Cleveland, Ohio : , : NASA Lewis Research Center : U.S. Army Research Laboratory, , December 1996
Descrizione fisica 1 online resource (14 pages) : illustrations
Collana NASA technical memorandum
Army Research Laboratory technical report
Soggetto topico Three dimensional flow
Turbine blades
Cascade flow
Flow distribution
Transonic flow
Rotor aerodynamics
Pressure distribution
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707497903321
Giel P. W (Paul W.)  
Cleveland, Ohio : , : NASA Lewis Research Center : U.S. Army Research Laboratory, , December 1996
Materiale a stampa
Lo trovi qui: Univ. Federico II
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