Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed / / Daniel S. Jones [and four others]
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| Autore: |
Jones Daniel S.
|
| Titolo: |
Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed / / Daniel S. Jones [and four others]
|
| Pubblicazione: | Edwards, CA : , : National Aeronautics and Space Administration, Armstrong Flight Research Center, , October 2014 |
| Descrizione fisica: | 1 online resource (25 pages) : color illustrations |
| Soggetto topico: | Convergent-divergent nozzles |
| Flow distribution | |
| Inviscid flow | |
| Nozzle design | |
| Rocket nozzles | |
| Note generali: | Title from title screen (viewed July 2, 2015). |
| "October 2014." | |
| Nota di bibliografia: | Includes bibliographical references (page 14). |
| Titolo autorizzato: | Conceptual design for a dual-bell rocket nozzle system using a NASA F-15 airplane as the flight testbed |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910703728303321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |