Penetration and Mixing of Lateral Injected Doublet Liquid Jets in Supersonic Airflow
碩士 === 國立成功大學 === 航空太空工程學系 === 103 === In scramjet engine combustor design, the outcome of liquid fuel injection is a vital issue for engine performance. In a very short residence time, a proper mixing between liquid fuel and supersonic air flow has to be achieved, following by stable combustion whi...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2015
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| Online Access: | http://ndltd.ncl.edu.tw/handle/95821777532804056775 |