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
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| 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
|
| Pubblicazione: | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1952 |
| Descrizione fisica: | 1 online resource (30 pages) : illustrations |
| Soggetto topico: | Nozzles - Fluid dynamics |
| Supersonic nozzles - Design and construction | |
| Axial flow | |
| Wind tunnel testing | |
| Mathematical analysis | |
| Persona (resp. second.): | RidyardHerbert W. |
| CromerNancy | |
| Note generali: | "June 1952." |
| No Federal Depository Library Program (FDLP) item number. | |
| Nota di bibliografia: | Includes bibliographical references (page 18). |
| Titolo autorizzato: | The aerodynamic design of high Mach number nozzles utilizing axisymmetric flow with application to a nozzle of square test section |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910713895903321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |