|
|
|
|
|
|
|
|
1. |
Record Nr. |
UNINA9910716912803321 |
|
|
Autore |
Bamber M. J. |
|
|
Titolo |
Wind-tunnel investigation of effect of yaw on lateral-stability characteristics . II Rectangular N.A.C.A. 23012 wing with a circular fuselage and a fin / / by M.J. Bamber and R.O. House |
|
|
|
|
|
|
|
Pubbl/distr/stampa |
|
|
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1939 |
|
|
|
|
|
|
|
|
|
Descrizione fisica |
|
1 online resource (9 pages, 11 unnumbered pages) : illustrations |
|
|
|
|
|
|
Collana |
|
Technical note / National Advisory Committee for Aeronautics ; ; No. 730 |
|
|
|
|
|
|
|
|
Soggetti |
|
Airplanes - Wings - Testing |
Airplanes - Fuselage |
Stability of airplanes |
Rolling (Aerodynamics) |
Yawing (Aerodynamics) |
Wind tunnel testing |
|
|
|
|
|
|
|
|
Lingua di pubblicazione |
|
|
|
|
|
|
Formato |
Materiale a stampa |
|
|
|
|
|
Livello bibliografico |
Monografia |
|
|
|
|
|
Note generali |
|
"September 1939." |
No Federal Depository Library Program (FDLP) item number. |
|
|
|
|
|
|
|
|
Nota di bibliografia |
|
Includes bibliographical references (page 9). |
|
|
|
|
|