Effect of fuel impingement cooling on the combustion flow field 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 === 91 === In this thesis, the combustion flow in a small bipropellant liquid rocket combustor is numerically simulated. Effects of injecting partial fuel on the chamber wall for cooling are investigated. The parameters investigated include the ratio of the cooling fue...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2003
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| Online Access: | http://ndltd.ncl.edu.tw/handle/13930665941411461830 |