The effects of full-span and partial-span split flaps on the aerodynamic characteristics of a tapered wing / / by Carl J. Wenzinger
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| Autore: |
Wenzinger Carl J (Carl Joseph), <1903-1988, >
|
| Titolo: |
The effects of full-span and partial-span split flaps on the aerodynamic characteristics of a tapered wing / / by Carl J. Wenzinger
|
| Pubblicazione: | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1934 |
| Descrizione fisica: | 1 online resource (6 pages, 5 unnumbered pages) : illustrations |
| Soggetto topico: | Airplanes - Wings - Testing |
| Aerodynamics | |
| Flaps (Airplanes) | |
| Split flaps (Airplanes) | |
| Wind tunnel testing | |
| Note generali: | "September 1934." |
| No Federal Depository Library Program (FDLP) item number. | |
| Nota di bibliografia: | Includes bibliographical references (page 6). |
| Titolo autorizzato: | The effects of full-span and partial-span split flaps on the aerodynamic characteristics of a tapered wing |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910715927103321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |