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The aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear / / by Fred E. Weick and Thomas A. Harris
| The aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear / / by Fred E. Weick and Thomas A. Harris |
| Autore | Weick Fred E. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1932 |
| Descrizione fisica | 1 online resource (7 pages, 11 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Wind tunnel testing
Split flaps (Airplanes) Airplanes - Models - Wings Trailing edge flaps |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713650303321 |
Weick Fred E.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1932 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model / / by M.J. Bamber
| Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model / / by M.J. Bamber |
| Autore | Bamber M. J. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934 |
| Descrizione fisica | 1 online resource (8 pages, 5 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerodynamics
Spin (Aerodynamics) Split flaps (Airplanes) Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713646103321 |
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Bamber M. J.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The effect of split trailing-edge wing flaps on the aerodynamic characteristics of a parasol monoplane / / by Rudolf N. Wallace
| The effect of split trailing-edge wing flaps on the aerodynamic characteristics of a parasol monoplane / / by Rudolf N. Wallace |
| Autore | Wallace Rudolf N. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1933 |
| Descrizione fisica | 1 online resource (8 pages, 8 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Wings
Split flaps (Airplanes) Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715384703321 |
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Wallace Rudolf N.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1933 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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The effects of full-span and partial-span split flaps on the aerodynamic characteristics of a tapered wing / / by Carl J. Wenzinger
| The effects of full-span and partial-span split flaps on the aerodynamic characteristics of a tapered wing / / by Carl J. Wenzinger |
| Autore | Wenzinger Carl J (Carl Joseph), <1903-1988, > |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934 |
| Descrizione fisica | 1 online resource (6 pages, 5 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Wings - Testing
Aerodynamics Flaps (Airplanes) Split flaps (Airplanes) Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715927103321 |
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Wenzinger Carl J (Carl Joseph), <1903-1988, >
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Full-scale span load distribution on a tapered wing with split flaps of various spans / / by John F. Parsons and Abe Silverstein
| Full-scale span load distribution on a tapered wing with split flaps of various spans / / by John F. Parsons and Abe Silverstein |
| Autore | Parsons John F. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1937 |
| Descrizione fisica | 1 online resource (10 pages, 18 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Wings
Aerodynamic load Split flaps (Airplanes) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716601603321 |
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Parsons John F.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1937 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Interference of wing and fuselage from tests of 18 combinations in the N.A.C.A. variable-density tunnel combinations with split flaps / / by Albert Sherman
| Interference of wing and fuselage from tests of 18 combinations in the N.A.C.A. variable-density tunnel combinations with split flaps / / by Albert Sherman |
| Autore | Sherman Albert |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1938 |
| Descrizione fisica | 1 online resource (9 pages, 7 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Wings - Testing
Airplanes - Fuselage - Testing Split flaps (Airplanes) Interference (Aerodynamics) Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716879403321 |
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Sherman Albert
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1938 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A method of estimating the aerodynamic effects of ordinary and split flaps of airfoils similar to the Clark Y / / by H.A. Pearson
| A method of estimating the aerodynamic effects of ordinary and split flaps of airfoils similar to the Clark Y / / by H.A. Pearson |
| Autore | Pearson Henry A (Henry Adolph), <1906-> |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1936 |
| Descrizione fisica | 1 online resource (19 pages, 12 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerofoils
Split flaps (Airplanes) Aerodynamics - Forecasting |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716021303321 |
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Pearson Henry A (Henry Adolph), <1906->
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1936 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Pressure distribution over a Clark Y-H airfoil section with a split flap / / by Carl J. Wenzinger
| Pressure distribution over a Clark Y-H airfoil section with a split flap / / by Carl J. Wenzinger |
| Autore | Wenzinger Carl J (Carl Joseph), <1903-1988, > |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1937 |
| Descrizione fisica | 1 online resource (5 pages, 6 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerofoils
Split flaps (Airplanes) Aerodynamic load Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716721103321 |
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Wenzinger Carl J (Carl Joseph), <1903-1988, >
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1937 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Pressure-distribution measurements on a rectangular wing with a partial-span split flap in curved flight / / by Frank G. Rokus
| Pressure-distribution measurements on a rectangular wing with a partial-span split flap in curved flight / / by Frank G. Rokus |
| Autore | Rokus Frank G. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 |
| Descrizione fisica | 1 online resource (7 pages, 8 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerodynamic load
Flaps (Airplanes) Split flaps (Airplanes) Rolling (Aerodynamics) Yawing (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717156303321 |
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Rokus Frank G.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Pressure-distribution measurements on a tapered wing with a full-span split flap in curved flight / / by Th. Troller and F. Rokus
| Pressure-distribution measurements on a tapered wing with a full-span split flap in curved flight / / by Th. Troller and F. Rokus |
| Autore | Troller T. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 |
| Descrizione fisica | 1 online resource (8 pages, 8 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Wings
Split flaps (Airplanes) Aerodynamic load - Measurement Rolling (Aerodynamics) Yawing (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716990503321 |
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Troller T.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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