Scramjet燃烧室流场的三维并行数值模拟及试验比较
Three-dimensional parallel simulation of the flow-field of a scramjet combustor and comparisons with experiments
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摘要: 作者采用时间相关法,通过有限体积离散,运用带化学反应的全N-S方程,在神州巨型机上,针对试验模型,对油气比Φ=0.0和0.35的喷氢Scramjet燃烧室流场进行了三维并行数值模拟,得到了流场的精细结构.并行模拟所得壁面压力分布与试验所测得的壁面压力分布吻合较好.
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