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- W3140863112 abstract "推动和极超音速的入口在 6.5 的马赫数字设计了的混合压缩的自我开始特征被使用不稳定的计算液体动力学(CFD ) 方法学习。完整的 NavierStokes 方程与假设被解决粘滞二方程的雷纳兹平均的完美的煤气的模型，和砍压力运输(SST ) k NavierStokes (RANS ) 模型被用于骚乱建模。结果显示在推动开始期间，流动领域被主要吃惊和在上游面对的吃惊与不同空气动力学的参数划分成三个地区。斜面的肩膀上的分离水泡经历产生，成长，吞咽并且消失在顺序的过程。但是在入口的入口的一个分离水泡存在直到 freestream 速度在自我期间被加速到开始的马赫数字开始。因为在吃惊和边界层之间的相互作用，流动地的集体流动分发是不一致的，以便在喉咙的集体流动率在推动开始期间是不稳定的。启动过程的推动的持续时间与 freestream 马赫数字的减少几乎线性地增加，但是当 freestream 马赫数字接近开始的马赫数字时，突然地升起。增强软件的加速的表演几乎没在开始极超音速的入口的能力的自我上有影响。" @default.
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- W3140863112 date "2013-01-01" @default.
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- W3140863112 title "Numerical study of unsteady starting characteristics of a hypersonic inlet" @default.
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