Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds / / by Bernard N. Daley and Douglas R. Lord
(Visualizza in formato marc)
(Visualizza in BIBFRAME)
| Autore: |
Daley Bernard N.
|
| Titolo: |
Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds / / by Bernard N. Daley and Douglas R. Lord
|
| Pubblicazione: | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1955 |
| Descrizione fisica: | 1 online resource (57 pages) : illustrations |
| Soggetto topico: | Aerofoils - Testing |
| Angle of attack (Aerodynamics) | |
| Persona (resp. second.): | LordDouglas T. |
| Note generali: | "May 1955." |
| "Supersedes recently declassified NACA RM L9E19. 1949"--Page 1. | |
| No Federal Depository Library Program (FDLP) item number. | |
| Nota di bibliografia: | Includes bibliographical references (page 10). |
| Altri titoli varianti: | Aerodynamic characteristics of several six-percent-thick airfoils at angles of attack from zero degrees to twenty degrees at high subsonic speeds |
| Titolo autorizzato: | Aerodynamic characteristics of several 6-percent-thick airfoils at angles of attack from 0° to 20° at high subsonic speeds |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910713882603321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |