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Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 / / Kevin W. Noonan and Gene J. Bingham
Aerodynamic characteristics of three helicopter rotor airfoil sections at Reynolds numbers from model scale to full scale at Mach numbers from 0.35 to 0.90 / / Kevin W. Noonan and Gene J. Bingham
Autore Noonan Kevin W.
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , September 1980
Descrizione fisica 1 online resource (82 pages) : chiefly illustrations
Collana NASA technical paper
AVRADCOM technical report
Soggetto topico Aerodynamic characteristics
Airfoils
Helicopters
Reynolds number
Wind tunnel tests
Aerofoils - Testing
Helicopters - Aerodynamics
Rotors (Helicopters) - Testing
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707473303321
Noonan Kevin W.  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , September 1980
Materiale a stampa
Lo trovi qui: Univ. Federico II
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Aerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses / / by Charles D. Harris
Aerodynamic characteristics of two NASA supercritical airfoils with different maximum thicknesses / / by Charles D. Harris
Autore Harris Charles D. <1952->
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, , April 1972
Descrizione fisica 1 online resource (55 pages) : illustrations
Collana NASA technical memorandum
Soggetto topico Aerodynamic characteristics
Supercritical airfoils
Airfoil profiles
Transonic wind tunnels
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707148103321
Harris Charles D. <1952->  
Washington, D.C. : , : National Aeronautics and Space Administration, , April 1972
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel / / David M. Schuster
Aerodynamic measurements on a large splitter plate for the NASA Langley Transonic Dynamics Tunnel / / David M. Schuster
Autore Schuster D. M (David M.)
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 2001
Descrizione fisica 1 online resource (37 pages) : illustrations
Collana NASA/TM
Soggetto topico Transonic wind tunnels
Aerodynamic characteristics
Dynamic pressure
Static pressure
Viscous flow
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910706548703321
Schuster D. M (David M.)  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 2001
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Aerodynamic parameters of an advanced fighter aircraft estimated from flight data [[electronic resource] ] : preliminary results / / Vladislav Klein, Kevin P. Breneman, Thomas P. Ratvasky
Aerodynamic parameters of an advanced fighter aircraft estimated from flight data [[electronic resource] ] : preliminary results / / Vladislav Klein, Kevin P. Breneman, Thomas P. Ratvasky
Autore Klein Vladislav
Pubbl/distr/stampa Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1989]
Descrizione fisica iv, 53 pages : digital, PDF file
Altri autori (Persone) BrenemanKevin P
RatvaskyThomas P
Collana NASA technical memorandum
Soggetto topico Fighter planes
Aerodynamic characteristics
Aircraft instruments
Aircraft maneuvers
Fighter aircraft
Flight tests
Mathematical models
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Aerodynamic parameters of an advanced fighter aircraft estimated from flight data
Record Nr. UNINA-9910698069803321
Klein Vladislav  
Hampton, Va. : , : National Aeronautics and Space Administration, Langley Research Center, , [1989]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Aerodynamic simulation of ice accretion on airfoils [[electronic resource] /] / Andy P. Broeren ... [and others]
Aerodynamic simulation of ice accretion on airfoils [[electronic resource] /] / Andy P. Broeren ... [and others]
Pubbl/distr/stampa Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011]
Descrizione fisica 1 online resource (iii, 66 pages) : illustrations (some color)
Altri autori (Persone) BroerenAndy P
Collana NASA/TP
Soggetto topico Airfoils
Ice formation
Wind tunnel tests
Aerodynamic stalling
Scale models
Simulation
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910701049903321
Cleveland, Ohio : , : National Aeronautics and Space Administration, Glenn Research Center, , [2011]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Aeroservoelastic testing of free flying wind tunnel models / / Robert C. Scott [and four others]
Aeroservoelastic testing of free flying wind tunnel models / / Robert C. Scott [and four others]
Autore Scott Robert C.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2013
Descrizione fisica 1 online resource (2 volumes) : color illustrations
Collana NASA/TP
Soggetto topico Aeroservoelasticity
Flaps (control surfaces)
Gust loads
Semispan models
Transonic wind tunnels
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Nota di contenuto pt 1. A sidewall supported semispan model tested for gust load alleviation and flutter suppression. -- pt 2. A centerline supported fullspan model tested for gust load alleviation.
Record Nr. UNINA-9910702418703321
Scott Robert C.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , 2013
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Aerothermal analysis of a wing-elevon cove with variable leakage / / L. Roane Hunt
Aerothermal analysis of a wing-elevon cove with variable leakage / / L. Roane Hunt
Autore Hunt L. Roane (Lewis Roane)
Pubbl/distr/stampa [Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , September 1980
Descrizione fisica 1 online resource (41 pages) : illustrations
Collana NASA technical paper
Soggetto topico Elevons
Mathematical models
Reynolds number
Space Shuttle orbiters
Wind tunnel tests
Aerothermodynamics
Airplanes - Wings
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910707473203321
Hunt L. Roane (Lewis Roane)  
[Washington, D.C.] : , : National Aeronautics and Space Administration, Scientific and Technical Information Branch, , September 1980
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Analysis and test evaluation of the dynamic stability of three advanced turboprop models at zero forward speed [[electronic resource] /] / by Arthur F. Smith
Analysis and test evaluation of the dynamic stability of three advanced turboprop models at zero forward speed [[electronic resource] /] / by Arthur F. Smith
Autore Smith Arthur F
Pubbl/distr/stampa Windsor Locks, Conn. : , : Hamilton Standard Division, United Technologies Corporation
Descrizione fisica 1 online resource (ix/x, 114 pages) : illustrations
Collana NASA CR
Soggetto topico Dynamic stability
Evaluation
Prop-fan technology
Turboprop engines
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910701902003321
Smith Arthur F  
Windsor Locks, Conn. : , : Hamilton Standard Division, United Technologies Corporation
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Analysis of wind tunnel longitudinal static and oscillatory data of the F-16XL aircraft / / Vladislav Klein [and three others]
Analysis of wind tunnel longitudinal static and oscillatory data of the F-16XL aircraft / / Vladislav Klein [and three others]
Autore Klein Vladislav
Pubbl/distr/stampa Hampton, Virginia, : National Aeronautics and Space Administration, Langley Research Center, December 1997
Descrizione fisica 1 online resource (63 pages) : illustrations
Collana NASA/TM
Soggetto topico Aerodynamic coefficients
Angle of attack
Control surfaces
F-16 aircraft
Fourier series
Harmonic analysis
Wind tunnel tests
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705768203321
Klein Vladislav  
Hampton, Virginia, : National Aeronautics and Space Administration, Langley Research Center, December 1997
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
An assessment of 3-C PIV analysis methodology for HART II measured data [[electronic resource] /] / Joon W. Lim, Berend G. van der Wall
An assessment of 3-C PIV analysis methodology for HART II measured data [[electronic resource] /] / Joon W. Lim, Berend G. van der Wall
Autore Lim Joon W
Pubbl/distr/stampa Moffett Field, CA : , : National Aeronautics and Space Administration, Ames Research Center, , [2010]
Descrizione fisica 1 online resource (39 pages) : color illustrations
Altri autori (Persone) LimJoon W
WallBerend G. van der
Collana NASA/TM
Soggetto topico Vortices
Wind tunnel tests
Blade-vortex interaction
Vorticity
Rotor blades
Aeroacoustics
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910701464503321
Lim Joon W  
Moffett Field, CA : , : National Aeronautics and Space Administration, Ames Research Center, , [2010]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

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