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Record Nr. |
UNINA9910699539803321 |
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Autore |
Arrington Lynn A |
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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 |
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Pubbl/distr/stampa |
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[Cleveland, Ohio] : , : National Aeronautics and Space Administration, Lewis Research Center, , [1992?] |
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Descrizione fisica |
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1 online resource (20 pages) : digital, PDF file |
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Collana |
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NASA technical memorandum ; ; 105967 |
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Altri autori (Persone) |
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Soggetti |
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Axisymmetric flow |
Coolants |
Film cooling |
Fluid injection |
Hydrogen |
Hydrogen oxygen engines |
Propulsion system performance |
Reacting flow |
Three dimensional flow |
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Lingua di pubblicazione |
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Formato |
Materiale a stampa |
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Livello bibliografico |
Monografia |
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Note generali |
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Title from title screen (viewed Aug. 25, 2010). |
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Nota di bibliografia |
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Includes bibliographical references (pages 8-9). |
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