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Characteristics of Condensation Shock Waves

Characteristics of Condensation Shock Waves
凝结冲击波的特性
批准号:
62550133
负责人:
KAWAGOE Shigetoshi
金额:
$1.22万
依托单位:
依托单位国家:
日本
项目类别:
Grant-in-Aid for General Scientific Research (C)
财政年份:
1987
资助国家:
日本
项目状态:
已结题
起止时间:
1987 至 1988

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项目成果

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中文摘要
翻译
对超音速喷管内湿空气膨胀引发凝结激波的凝结流动进行了数值模拟和实验研究,并在超音速凝结流动中插入楔形激波发生器,对凝结激波与斜激波的相互作用进行了实验研究。结果表明,凝结激波的特性得到了明确的体现。结果表明:(1)当喷嘴内发生冷凝时,空气的熵增大,水蒸气的熵减小。冷凝产生的液滴的表面熵略有增加。因此,由于这些效应,混合物的熵增加。总压损失的计算值略小于实验值,约为2%~5%。初始过饱和度越大,湿空气初始温度越大,喷嘴膨胀率越大,总压力损失越大。(3)明确了斜激波相对于冷凝区的位置和凝结时斜激波的形状变化。工作在喷管壁面上的载荷随着初始过饱和度和初始温度的增大而增大。(4)定性地解释了凝结激波与斜激波的相互作用规律。当正凝聚激波与斜激波相互作用时,斜激波在一定条件下消失。当凝结作用大于此状态时,正常凝结激波位于上游位置,斜激波从楔形前缘再次出现。
英文摘要
Condensing flow with a condensation shock wave initiated by an expansion of moist air in a supersonic nozzle was investigated numerically and experimentally, and then by inserting a wedge-type shock generator in the supersonic condensing flow, the interaction of the condensation shock wave with an oblique shock wave was investigated experimentally. As the results, the characteristics of condensation shock wave are clarified. The results obtaind are summarized as follows.(1) When condensation takes place in a nozzle, the entropy of the air increases and that of the vapor decreases. The surface entropy of a droplet generated by condensation increases a little. Therefore, the entropy of the mixture increases due to these effects. As the results, the total pressure of the flow decreases.(2) The calculated value of the total pressure loss are a little smaller than those of the experimental results and they are about 2 to 5 percent. The larger the initial degree of supersaturation, the initial temperature of moist air and the higher the expansion rate of nozzle are, the larger the total pressure loss becomes.(3) The position of the oblique shock wave relative to the condensation zone and the change of shape of the obligue shock wave due to condensation are clarified. The load working on the nozzle wall increases with an increasing in the initial degree of supersaturation and the initial temperature.(4) The interaction patterns of the condensation shock wave with the oblique shock wave are explained qualitatively. When a normal condensation shock wave interacts with an oblique shock wave, the oblique shock wave disappears under a certain condition. When the effect of condensation becomes stronger than this state, the normal condensation shock wave stands more upstream position and then the oblique shock wave appears again from the leading of wedge.
期刊论文(10)
专著(0)
科研奖励(0)
会议论文
権純範: 日本機械学会論文集. 54. 798-802 (1988)
Junnori Gon:日本机械工程师学会会议记录 54. 798-802 (1988)。
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通讯作者:
Soon Bum KWON: "Total Pressure Loss in Supersonic Nozzle Flows with Condensation (Numerical Analyses)" JSME International Journal. 31. 16-21 (1988)
Soon Bum KWON:“超音速喷嘴冷凝流动中的总压力损失(数值分析)”JSME 国际期刊。
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川越茂敏: 日本機械学会第66期全国大会講演会(昭和63年10月18日)において口頭発表 日本機械学会論文集.
Shigetoshi Kawagoe:在第 66 届日本机械工程师学会全国会议上的口头报告(1986 年 10 月 18 日),日本机械工程师学会会议记录。
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通讯作者:
Soon Bum KWON: "Effects of Condensing Flow on an Oblique Shock Wave in a Supersonic Nozzle" Transactions of the Japan Society of Mechanical Engineers. 54. 798-802 (1988)
Soon Bum KWON:“超音速喷嘴中冷凝流对倾斜冲击波的影响”日本机械工程师学会会刊。
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