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马赫数1.95超声速欠膨胀喷流声辐射数值分析 被引量:2
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作者 冯峰 郭力 王强 《航空学报》 EI CAS CSCD 北大核心 2016年第11期3273-3283,共11页
针对马赫数为1.95的欠膨胀超声速喷流声辐射特性,采用高精度计算格式的大涡模拟(LES)方法进行数值研究。通过对喷流平均流及湍流脉动统计结果的对比,确定数值方法的精确性。细致分析了超声速喷流流动特征,特别关注了其中激波胞格和湍流... 针对马赫数为1.95的欠膨胀超声速喷流声辐射特性,采用高精度计算格式的大涡模拟(LES)方法进行数值研究。通过对喷流平均流及湍流脉动统计结果的对比,确定数值方法的精确性。细致分析了超声速喷流流动特征,特别关注了其中激波胞格和湍流相互作用现象。基于流动与声场辐射间的关联性,分析了超声速喷流马赫波、宽频激波噪声辐射特性及形成机理。数值结果表明超声速喷流的剪切层演化及激波胞格与湍流间的相互作用构成欠膨胀超声速喷流的主要噪声源。 展开更多
关键词 超声速欠膨胀喷流 马赫波辐射 宽频激波噪声 激波-湍流相互作用 大涡模拟
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A Study on Broad Band Noise Emitted from Underexpanded Radial Jet
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作者 Yuichi Hiramoto Hiromasa Suzuki +1 位作者 Masaki Endo Yoko Sakakibara 《Open Journal of Fluid Dynamics》 2019年第1期72-81,共10页
This study focuses on a noise emitted from a radial underexpanded jet. The underexpanded jet is well known as one of supersonic jets and it is formed when the pressure ratio across a convergent nozzle is more than the... This study focuses on a noise emitted from a radial underexpanded jet. The underexpanded jet is well known as one of supersonic jets and it is formed when the pressure ratio across a convergent nozzle is more than the critical value. The underexpanded jet has been used in many fields, such a propulsion of rocket, laser cutting and a glass tempering process. Such jet is exhausted from a circular nozzle. The expansion wave, the compression wave and the shock wave are periodically formed in the jet, which leads to quasi-periodical shock-cell structure. On the other hand, an underexpanded jet radially issues from intake and exhaust valves of an internal combustion engine and a pressure control valve. The radial underexpanded jet does not have the quasi- periodical shock-cell structure such as the jet from the circular nozzle, its cell length decreasing along jet axis. In this study, an underexpanded jet radially discharged from a circular slit nozzle, which consists of two circular tubes, is experimentally examined for different nozzle pressure ratios. The jet structure is visualized using Schlieren method and a noise emitted from the jet is measured. Typically, the shock associated broadband noise is analyzed and a relation between the jet structure and the radiation noise frequency is discussed. As a result, it is found that the broadband noise lies on lower frequency than a screech tone and that the 1st cell length plays an important role in broadband noise radiation. 展开更多
关键词 broadband noise shock WAVE Underexpanded JET VISUALIZATION
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