|
|
|
|
|
|
|
|
1. |
Record Nr. |
UNINA9910713895903321 |
|
|
Autore |
Beckwith Ivan E. |
|
|
Titolo |
The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section / / by Ivan E. Beckwith, Herbert W. Ridyard, and Nancy Cromer |
|
|
|
|
|
|
|
Pubbl/distr/stampa |
|
|
Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952 |
|
|
|
|
|
|
|
|
|
Descrizione fisica |
|
1 online resource (30 pages) : illustrations |
|
|
|
|
|
|
Collana |
|
Technical notes / National Advisory Committee for Aeronautics ; ; No. 2711 |
|
|
|
|
|
|
|
|
Soggetti |
|
Nozzles - Fluid dynamics |
Supersonic nozzles - Design and construction |
Axial flow |
Wind tunnel testing |
Mathematical analysis |
|
|
|
|
|
|
|
|
Lingua di pubblicazione |
|
|
|
|
|
|
Formato |
Materiale a stampa |
|
|
|
|
|
Livello bibliografico |
Monografia |
|
|
|
|
|
Note generali |
|
"June 1952." |
No Federal Depository Library Program (FDLP) item number. |
|
|
|
|
|
|
|
|
Nota di bibliografia |
|
Includes bibliographical references (page 18). |
|
|
|
|
|