| 摘要: |
| 用电弧加热空气,对带有突扩台阶后扩张形,入口M_a=2.1和3.0的超声速燃烧室进行了实验研究,并对两种不同燃烧室长度、煤油和氢气在垂直和平行喷射下的燃烧状况作了比较。 |
| 关键词: 超声速燃烧 试验 研究 |
| DOI： |
| 分类号: |
| 基金项目:国家自然科学基金资助项目 |
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| EXPERIMENTAL INVESTIGATION ON SUPERSONIC COMBUSTION (Ⅱ) |
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Liu XingZhou, Liu JingHua, Wang YuRen, Ge YunQi, Yang LiXing, Hu YuLi
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The 31st Research Institute
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| Abstract: |
| The experimental investigation with a model supersonic combustor which consists of rearward-facing step and diverging duct was carried out by using electric arc-heated air to simulate combustor inlet Mach number 2. 1 and 3. 0. Comparisons were made with combus-tors in two kinds of length by burning kerosene or hydrogen fuel injected parallelly or perpendicularly to the airstream. |
| Key words: Supersonic combustion Test Research |
