|
|
|
|
|
|
|
|
1. |
Record Nr. |
UNINA9910713805003321 |
|
|
Autore |
Knight Montgomery |
|
|
Titolo |
Wind tunnel pressure distribution tests on a series of biplane wing models . Part III Effects of changes in various combinations of stagger, gap, sweepback, and decalage / / by Montgomery Knight and Richard W. Noyes |
|
|
|
|
|
|
|
Pubbl/distr/stampa |
|
|
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1929 |
|
|
|
|
|
|
|
|
|
Descrizione fisica |
|
1 online resource (6 pages, 22 unnumbered pages) : illustrations |
|
|
|
|
|
|
Collana |
|
Technical notes / National Advisory Committee for Aeronautics ; ; No. 330 |
|
|
|
|
|
|
|
|
Soggetti |
|
Aerodynamic load - Testing |
Airplanes - Models - Testing |
Airplanes - Wings, Swept-back |
Wind tunnel testing |
Biplanes |
|
|
|
|
|
|
|
|
Lingua di pubblicazione |
|
|
|
|
|
|
Formato |
Materiale a stampa |
|
|
|
|
|
Livello bibliografico |
Monografia |
|
|
|
|
|
Note generali |
|
"December, 1929." |
Includes errata. |
No Federal Depository Library Program (FDLP) item number. |
|
|
|
|
|
|
|
|
Nota di bibliografia |
|
Includes bibliographical references (page 6). |
|
|
|
|
|