Numerical Analyses of the Conjugate Heat Transfer in a Bipropellant Liquid Rocket Combustor
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 98 === The high-temperature gas of a bipropellant liquid rocket combustor may burn and erode the chamber wall, damaging the whole structure. Therefore, in a general practice, part of the fuel of a bipropellant liquid rocket is injected toward the chamber wall to f...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2010
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| Online Access: | http://ndltd.ncl.edu.tw/handle/29899202791597923319 |