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.
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 |
Wenzinger Carl J (Carl Joseph), <1903-1988, >
|
||
| Washington [D.C.] : , : National Advisory Committee for Aeronautics, , 1933 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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 |
|
Wenzinger Carl J (Carl Joseph), <1903-1988, >
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
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 |
|
Wenzinger Carl J (Carl Joseph), <1903-1988, >
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1937 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Résumé of air-load data on slats and flaps / / by Carl J. Wenzinger and Francis M. Rogallo
| Résumé of air-load data on slats and flaps / / by Carl J. Wenzinger and Francis M. Rogallo |
| Autore | Wenzinger Carl J (Carl Joseph), <1903-1988, > |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 |
| Descrizione fisica | 1 online resource (10 pages, 26 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Flaps (Airplanes)
Aerofoils Leading edges (Aerodynamics) Trailing edges (Aerodynamics) Aerodynamic load |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716931703321 |
|
Wenzinger Carl J (Carl Joseph), <1903-1988, >
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Tests of round and flat spoilers on a tapered wing in the NACA 19-foot pressure wind tunnel / / by Carl J. Wenzinger and John D. Bowen
| Tests of round and flat spoilers on a tapered wing in the NACA 19-foot pressure wind tunnel / / by Carl J. Wenzinger and John D. Bowen |
| Autore | Wenzinger Carl J (Carl Joseph), <1903-1988, > |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1941 |
| Descrizione fisica | 1 online resource (5 pages, 7 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Wings - Testing
Spoilers (Airplanes) Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717293403321 |
|
Wenzinger Carl J (Carl Joseph), <1903-1988, >
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1941 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Wind tunnel force tests in wing systems through large angles of attack / / by Carl J. Wenzinger and Thomas A. Harris
| Wind tunnel force tests in wing systems through large angles of attack / / by Carl J. Wenzinger and Thomas A. Harris |
| Autore | Wenzinger Carl J (Carl Joseph), <1903-1988, > |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1928 |
| Descrizione fisica | 1 online resource (7 pages, 19 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Wings - Testing
Wind tunnel testing Angle of attack (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713659703321 |
|
Wenzinger Carl J (Carl Joseph), <1903-1988, >
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1928 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Wind tunnel pressure distribution tests on an airfoil with trailing edge flap / / by Carl J. Wenzinger and Oscar Loeser, Jr
| Wind tunnel pressure distribution tests on an airfoil with trailing edge flap / / by Carl J. Wenzinger and Oscar Loeser, Jr |
| Autore | Wenzinger Carl J (Carl Joseph), <1903-1988, > |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1929 |
| Descrizione fisica | 1 online resource (10 pages, 12 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerofoils
Flaps (Airplanes) Wind tunnel testing Aerodynamic load - Testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713818903321 |
|
Wenzinger Carl J (Carl Joseph), <1903-1988, >
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1929 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Wind-tunnel investigation of rectangular and tapered N.A.C.A. 23012 wings with plain ailerons and full-span split flaps / / by Carl J. Wenzinger and Milton B. Ames, Jr
| Wind-tunnel investigation of rectangular and tapered N.A.C.A. 23012 wings with plain ailerons and full-span split flaps / / by Carl J. Wenzinger and Milton B. Ames, Jr |
| Autore | Wenzinger Carl J (Carl Joseph), <1903-1988, > |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1938 |
| Descrizione fisica | 1 online resource (11 pages, 9 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Wings - Testing
Split flaps (Airplanes) Ailerons Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716863003321 |
|
Wenzinger Carl J (Carl Joseph), <1903-1988, >
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1938 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Wind-tunnel measurements of air loads on split flaps / / by Carl J. Wenzinger
| Wind-tunnel measurements of air loads on split flaps / / 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 (8 pages, 7 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Wings
Split flaps (Airplanes) Aerodynamic load Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910715344303321 |
|
Wenzinger Carl J (Carl Joseph), <1903-1988, >
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Wind-tunnel tests of a Clark Y wing having split flaps with gaps / / by Carl J. Wenzinger
| Wind-tunnel tests of a Clark Y wing having split flaps with gaps / / by Carl J. Wenzinger |
| Autore | Wenzinger Carl J (Carl Joseph), <1903-1988, > |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1938 |
| Descrizione fisica | 1 online resource (4 pages, 3 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Models - Wings
Split flaps (Airplanes) Lift (Aerodynamics) Drag (Aerodynamics) Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716874003321 |
|
Wenzinger Carl J (Carl Joseph), <1903-1988, >
|
||
| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1938 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
