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2011年4期
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Shock Wave in Supersonic Moist Air Jet for a Low Pressure Ratio
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
2011年4期
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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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