Cooling process of liquid propellant rocket by means of kerosene-alumina nanofluid
Heat transfer augmentation of kerosene-alumina nanofluid is studied for the possible use in the regenerative cooling channel of semi cryogenic engine. The basic partial differential equations are reduced to ordinary differential equations which are solved using differential transformation method. Ve...
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| Autors principals: | , |
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| Format: | Artigo |
| Idioma: | Inglês |
| Publicat: |
KeAi Communications Co., Ltd.
2016-12-01
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| Col·lecció: | Propulsion and Power Research |
| Matèries: | |
| Accés en línia: | http://www.sciencedirect.com/science/article/pii/S2212540X16300396 |
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