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Shock Wave in Supersonic Moist Air Jet for a Low Pressure Ratio

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摘要在现在的学习，一个计算液体动力学工作被执行在超声的潮湿的空气喷气由冷凝作用调查冲击波的出现。不稳定的、可压缩的axisymmetric海军司烧方程被TVD(减少的全部的变化)解决在这研究的计划。数字模拟为低压力比率和各种各样的湿度被执行了。结果为低压力比率在超声的潮湿的空气喷气看冲击波的出现马赫磁盘什么时候不发生，取决于空气的湿度。

DOI n490zn2x4y/986411

作者 Yumiko OTOBE;Hideo KASHIMURA;Toshiaki SETOGUCHI

机构地区不详

出处《热科学学报：英文版》 2011年4期

关键词空气喷射超音速冲击波潮湿 STOKES方程计算流体动力学

分类 [理学][物理]

出版日期 2011年04月14日（中国期刊网平台首次上网日期，不代表论文的发表时间）

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来源期刊

热科学学报：英文版

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相关关键词

空气喷射超音速冲击波潮湿 STOKES方程计算流体动力学

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