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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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The aerodynamic characteristics of an aspect-ratio-20 wing having thick airfoil sections and employing boundary-layer control by suction / / by Bennie W. Cocke, Jr., Marvin P. Fink, and Stanley M. Gottlieb
| The aerodynamic characteristics of an aspect-ratio-20 wing having thick airfoil sections and employing boundary-layer control by suction / / by Bennie W. Cocke, Jr., Marvin P. Fink, and Stanley M. Gottlieb |
| Autore | Cocke Bennie W. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1953 |
| Descrizione fisica | 1 online resource (63 pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Wings
Aerofoils Boundary layer control Lift (Aerodynamics) Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713889103321 |
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Cocke Bennie W.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1953 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A comparison of several tapered wings designed to avoid tip stalling / / by Raymond F. Anderson
| A comparison of several tapered wings designed to avoid tip stalling / / by Raymond F. Anderson |
| Autore | Anderson Raymond F. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 |
| Descrizione fisica | 1 online resource (19 pages, 8 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Wings
Airplanes - Wings - Design and construction Stalling (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717169103321 |
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Anderson Raymond F.
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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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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 |
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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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The effect of partial-span split flaps on the aerodynamic characteristics of a Clark Y wing / / by Carl J. Wenzinger
| The effect of partial-span split flaps on the aerodynamic characteristics of a Clark Y wing / / by Carl J. Wenzinger |
| Autore | Wenzinger Carl J (Carl Joseph), <1903-1988, > |
| Pubbl/distr/stampa | Washington [D.C.] : , : National Advisory Committee for Aeronautics, , 1933 |
| Descrizione fisica | 1 online resource (5 pages, 4 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Wings
Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715385903321 |
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Wenzinger Carl J (Carl Joseph), <1903-1988, >
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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 partial-span plain flaps on the aerodynamic characteristics of a rectangular and a tapered Clark Y-wing / / by R.O. House
| The effects of partial-span plain flaps on the aerodynamic characteristics of a rectangular and a tapered Clark Y-wing / / by R.O. House |
| Autore | House R. O. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1938 |
| Descrizione fisica | 1 online resource (6 pages, 7 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Wings
Flaps (Airplanes) Ailerons Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716849703321 |
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House R. O.
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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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The effects of partial-span slotted flaps on the aerodynamic characteristics of a rectangular and a tapered N.A.C.A. 23012 wing / / by Rufus O. House
| The effects of partial-span slotted flaps on the aerodynamic characteristics of a rectangular and a tapered N.A.C.A. 23012 wing / / by Rufus O. House |
| Autore | House R. O. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 |
| Descrizione fisica | 1 online resource (5 pages, 5 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Wings
Slotted flaps (Airplanes) Flaps (Airplanes) Aerodynamics Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717166803321 |
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House R. O.
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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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Measurements and analysis of the motion of a canard airplane model in gusts / / by Philip Donely, Harold B. Pierce, and Philip W. Pepoon
| Measurements and analysis of the motion of a canard airplane model in gusts / / by Philip Donely, Harold B. Pierce, and Philip W. Pepoon |
| Autore | Donely Philip |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1940 |
| Descrizione fisica | 1 online resource (20 pages, 9 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Wings
Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717126903321 |
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Donely Philip
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1940 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Pressure-distribution investigation of an N.A.C.A. 0009 airfoil with a 30-percent-chord plain flap and three tabs / / by Milton B. Ames, Jr. and Richard I. Sears
| Pressure-distribution investigation of an N.A.C.A. 0009 airfoil with a 30-percent-chord plain flap and three tabs / / by Milton B. Ames, Jr. and Richard I. Sears |
| Autore | Ames Milton B., Jr. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1940 |
| Descrizione fisica | 1 online resource (14 pages, 29 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Wings
Flaps (Airplanes) Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717125703321 |
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Ames Milton B., Jr.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1940 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Span load distribution on two monoplane wing models as affected by twist and sweepback / / by Montgomery Knight and Richard W. Noyes
| Span load distribution on two monoplane wing models as affected by twist and sweepback / / by Montgomery Knight and Richard W. Noyes |
| Autore | Knight Montgomery |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1930 |
| Descrizione fisica | 1 online resource (7 pages, 12 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Wings
Loads (Mechanics) Stability of airplanes |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910714048703321 |
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Knight Montgomery
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1930 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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