Vai al contenuto principale della pagina
| Autore: |
Smith Hamilton A.
|
| Titolo: |
Aerodynamic characteristics at Reynolds numbers of 3.0 x 10⁶ and 6.0 x 10⁶ of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section / / by Hamilton A. Smith and Raymond F. Schaefer
|
| Pubblicazione: | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1950 |
| Descrizione fisica: | 1 online resource (18 pages) : illustrations |
| Soggetto topico: | Aerofoils |
| Aerodynamics | |
| Lift (Aerodynamics) | |
| Drag (Aerodynamics) | |
| Pitching (Aerodynamics) | |
| Reynolds number | |
| Persona (resp. second.): | SchaeferRaymond F. |
| Note generali: | "April 1950." |
| No Federal Depository Library Program (FDLP) item number. | |
| Nota di bibliografia: | Includes bibliographical references (page 9). |
| Altri titoli varianti: | Aerodynamic characteristics at Reynolds numbers of 3.0 x 10(exp 6) and 6.0 x 10(exp 6) of three airfoil sections formed by cutting off various amounts from the rear portion of the National Advisory Committee for Aeronautics 0012 airfoil section |
| Titolo autorizzato: | Aerodynamic characteristics at Reynolds numbers of 3.0 x 10⁶ and 6.0 x 10⁶ of three airfoil sections formed by cutting off various amounts from the rear portion of the NACA 0012 airfoil section ![]() |
| Formato: | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910713757103321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |