Performance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydrogen/oxyen rocket [[electronic resource] /] / Lynn A. Arrington and Brian D. Reed
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| Autore: |
Arrington Lynn A
|
| Titolo: |
Performance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydrogen/oxyen rocket [[electronic resource] /] / Lynn A. Arrington and Brian D. Reed
|
| Pubblicazione: | [Cleveland, Ohio] : , : National Aeronautics and Space Administration, Lewis Research Center, , [1992?] |
| Descrizione fisica: | 1 online resource (20 pages) : digital, PDF file |
| Soggetto topico: | Axisymmetric flow |
| Coolants | |
| Film cooling | |
| Fluid injection | |
| Hydrogen | |
| Hydrogen oxygen engines | |
| Propulsion system performance | |
| Reacting flow | |
| Three dimensional flow | |
| Altri autori: |
ReedBrian D
|
| Note generali: | Title from title screen (viewed Aug. 25, 2010). |
| Nota di bibliografia: | Includes bibliographical references (pages 8-9). |
| Titolo autorizzato: | Performance comparison of axisymmetric and three-dimensional hydrogen film coolant injection in a 110N hydrogen |
| Formato: | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione: | Inglese |
| Record Nr.: | 9910699539803321 |
| Lo trovi qui: | Univ. Federico II |
| Opac: | Controlla la disponibilità qui |
Serie:
NASA technical memorandum ; ; 105967.