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Aerodynamic loads on a leading-edge flap and a leading-edge slat on the NACA 64A010 airfoil section / / by John A. Kelly and George B. McCullough
Aerodynamic loads on a leading-edge flap and a leading-edge slat on the NACA 64A010 airfoil section / / by John A. Kelly and George B. McCullough
Autore Kelly John A.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954
Descrizione fisica 1 online resource (33 pages) : illustrations
Collana Technical notes / National Advisory Committee for Aeronautics
Soggetto topico Aerodynamic load
Aerofoils
Flaps (Airplanes)
Leading edge flaps
Leading edges (Aerodynamics)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Aerodynamic loads on a leading-edge flap and a leading-edge slat on the National Advisory Committee for Aeronautics 64A010 airfoil section
Record Nr. UNINA-9910713887803321
Kelly John A.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1954
Materiale a stampa
Lo trovi qui: Univ. Federico II
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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
Wind tunnel investigation of passive porosity applied to the leading-edge extension and leading-edge flaps on a slender wing at subsonic speed / / Gary E. Erickson
Wind tunnel investigation of passive porosity applied to the leading-edge extension and leading-edge flaps on a slender wing at subsonic speed / / Gary E. Erickson
Autore Erickson Gary E.
Pubbl/distr/stampa Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 2017
Descrizione fisica 1 online resource (iv, 43 pages) : color illustrations
Collana NASA/TM
Soggetto topico Angle of attack
Delta wings
Leading edge flaps
Static pressure
Subsonic speed
Vortices
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910705787203321
Erickson Gary E.  
Hampton, Virginia : , : National Aeronautics and Space Administration, Langley Research Center, , March 2017
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Wind-tunnel tests on model wing with Fowler flap and specially developed leading-edge slot / / by Fred E. Weick and Robert C. Platt
Wind-tunnel tests on model wing with Fowler flap and specially developed leading-edge slot / / by Fred E. Weick and Robert C. Platt
Autore Weick Fred E.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1933
Descrizione fisica 1 online resource (10 pages, 7 unnumbered pages) : illustrations
Collana Technical note / National Advisory Committee for Aeronautics
Soggetto topico Airplanes - Wings - Testing
Airplanes - Control surfaces
Flaps (Airplanes)
Leading edge flaps
Trailing edge flaps
Slotted flaps (Airplanes)
Fowler flaps
Wind tunnel testing
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910715227303321
Weick Fred E.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1933
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui