推进技术 ›› 1993, Vol. 14 ›› Issue (4): 1-7.
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刘兴洲,刘敬华,王裕人,葛运圻,杨丽新,胡欲立
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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
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
刘兴洲,刘敬华,王裕人,葛运圻,杨丽新,胡欲立. 超声速燃烧实验研究(Ⅱ)[J]. 推进技术, 1993, 14(4): 1-7.
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