top

  Info

  • Utilizzare la checkbox di selezione a fianco di ciascun documento per attivare le funzionalità di stampa, invio email, download nei formati disponibili del (i) record.

  Info

  • Utilizzare questo link per rimuovere la selezione effettuata.
Aerodynamic effects caused by icing of an unswept NACA 65A004 airfoil / / by Vernon H. Gray and Uwe H. von Glahn
Aerodynamic effects caused by icing of an unswept NACA 65A004 airfoil / / by Vernon H. Gray and Uwe H. von Glahn
Autore Gray Vernon H.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1958
Descrizione fisica 1 online resource (47 pages) : illustrations
Collana Technical notes / National Advisory Committee for Aeronautics
Soggetto topico Aerofoils
Airplanes - Ice prevention
Drag (Aerodynamics)
Leading edges (Aerodynamics)
Lift (Aerodynamics)
Pitching (Aerodynamics)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Aerodynamic effects caused by icing of an unswept National Advisory Committee for Aeronautics 65A004 airfoil
Record Nr. UNINA-9910713871503321
Gray Vernon H.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1958
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
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
Opac: Controlla la disponibilità qui
Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow / / by Charles E. Watkins
Air forces and moments on triangular and related wings with subsonic leading edges oscillating in supersonic potential flow / / by Charles E. Watkins
Autore Watkins Charles E.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1951
Descrizione fisica 1 online resource (44 pages) : illustrations
Collana Technical notes / National Advisory Committee for Aeronautics
Soggetto topico Airplanes - Wings, Swept-back
Airplanes - Wings, Triangular
Leading edges (Aerodynamics)
Oscillating wings (Aerodynamics)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910713754703321
Watkins Charles E.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1951
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Combined experiment . Phase I [[electronic resource] ] : final report / / C.P. Butterfield, W.P. [sic] Musial, D.A. Simms
Combined experiment . Phase I [[electronic resource] ] : final report / / C.P. Butterfield, W.P. [sic] Musial, D.A. Simms
Autore Butterfield C. P (Charles P.)
Pubbl/distr/stampa Golden, Colo. : , : National Renewable Energy Laboratory, , [1992]
Descrizione fisica 1 online resource (221 unnumbered pages) : illustrations
Altri autori (Persone) MusialWalter D
SimmsD. A
Collana NREL/TP
Soggetto topico Wind turbines - Research
Wind power
Aerofoils - Testing
Aerodynamic load
Leading edges (Aerodynamics)
Wind tunnels - Testing
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Altri titoli varianti Combined experiment
Record Nr. UNINA-9910697744103321
Butterfield C. P (Charles P.)  
Golden, Colo. : , : National Renewable Energy Laboratory, , [1992]
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Effect of length of Handley Page tip slots on the lateral-stability factor, damping in roll / / by Fred E. Weick and Carl J. Wenzinger
Effect of length of Handley Page tip slots on the lateral-stability factor, damping in roll / / by Fred E. Weick and Carl J. Wenzinger
Autore Weick Fred E.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1932
Descrizione fisica 1 online resource (6 pages, 11 unnumbered pages) : illustrations
Collana Technical note / National Advisory Committee for Aeronautics
Soggetto topico Airplanes - Models - Wings
Leading edges (Aerodynamics)
Rolling (Aerodynamics)
Stability of airplanes
Wind tunnel testing
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910715268903321
Weick Fred E.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1932
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
The effect of lift, drag, and spinning characteristics of sharp leading edges on airplane wings / / by Fred E. Weick and Nathan F. Scudder
The effect of lift, drag, and spinning characteristics of sharp leading edges on airplane wings / / by Fred E. Weick and Nathan F. Scudder
Autore Weick Fred E.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1933
Descrizione fisica 1 online resource (15 pages, 9 unnumbered pages) : illustrations
Collana Technical note / National Advisory Committee for Aeronautics
Soggetto topico Airplanes - Wings
Leading edges (Aerodynamics)
Lift (Aerodynamics)
Drag (Aerodynamics)
Spin (Aerodynamics)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910715236203321
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
Effect of nose shape on the characteristics of symmetrical airfoils / / by Robert M. Pinkerton
Effect of nose shape on the characteristics of symmetrical airfoils / / by Robert M. Pinkerton
Autore Pinkerton Robert M.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1931
Descrizione fisica 1 online resource (16 pages, 9 unnumbered pages) : illustrations
Collana Technical note / National Advisory Committee for Aeronautics
Soggetto topico Aerofoils
Wind tunnel testing
Leading edges (Aerodynamics)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910715130503321
Pinkerton Robert M.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1931
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
The effect of slots and flaps on the lift and drag of the McDonnell airplane as determined in flight / / by Hartley A. Soulé
The effect of slots and flaps on the lift and drag of the McDonnell airplane as determined in flight / / by Hartley A. Soulé
Autore Soule Hartley A (Hartley Akin), <1904-1988, >
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1931
Descrizione fisica 1 online resource (12 pages, 16 unnumbered pages) : illustrations
Collana Technical note / National Advisory Committee for Aeronautics
Soggetto topico Airplanes - Wings
Leading edges (Aerodynamics)
Flaps (Airplanes)
Slotted flaps (Airplanes)
Lift (Aerodynamics)
Drag (Aerodynamics)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910715121803321
Soule Hartley A (Hartley Akin), <1904-1988, >  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1931
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Effect of wing sweep, angle of attack, Reynolds number, and wing root fillet on the interference heating to the wing windward surface of an entry vehicle configuration / / by Louis E. Clark
Effect of wing sweep, angle of attack, Reynolds number, and wing root fillet on the interference heating to the wing windward surface of an entry vehicle configuration / / by Louis E. Clark
Autore Clark Louis E.
Pubbl/distr/stampa Washington, D.C. : , : National Aeronautics and Space Administration, , December 1972
Descrizione fisica 1 online resource (52 pages) : illustrations
Collana NASA/TN
Soggetto topico Aerospace vehicles
Aerodynamics
Space vehicles - Atmospheric entry
Leading edges (Aerodynamics)
Aerodynamic heating
Aerothermodynamics
Space shuttles
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910716019303321
Clark Louis E.  
Washington, D.C. : , : National Aeronautics and Space Administration, , December 1972
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui
Experiments with an airfoil model on which the boundary layer is controlled without the use of supplementary equipment / / by I.H. Abbott
Experiments with an airfoil model on which the boundary layer is controlled without the use of supplementary equipment / / by I.H. Abbott
Autore Abbott I. H.
Pubbl/distr/stampa Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1931
Descrizione fisica 1 online resource (6 pages, 5 unnumbered pages) : illustrations
Collana Technical notes / National Advisory Committee for Aeronautics
Soggetto topico Boundary layer control
Aerofoils
Leading edges (Aerodynamics)
Lift (Aerodynamics)
Angle of attack (Aerodynamics)
Formato Materiale a stampa
Livello bibliografico Monografia
Lingua di pubblicazione eng
Record Nr. UNINA-9910715137303321
Abbott I. H.  
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1931
Materiale a stampa
Lo trovi qui: Univ. Federico II
Opac: Controlla la disponibilità qui

Data di pubblicazione

Altro...