Effects of the Asymmetric Impingement of Unlike-Doublet Injection on the Flow of 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 === 92 === In this thesis, the combustion flow in a small bipropellant liquid rocket combustor is numerically simulated. In the present study, how the curvature of the liquid sheet generated by the asymmetric impingement of unlike-doublet injection affects the combusti...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2004
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| Online Access: | http://ndltd.ncl.edu.tw/handle/26640286412071080208 |