利用超声波驻波声场的声能量密度在空间呈周期分布的性质,结合纹影法,对空气介质中28 k Hz超声波形成的驻波声场进行成像,使得超声波驻波声场的某些特性可视化,进而更加精准测量其波长和声速值。用光线折射几何理论证明了光的不均匀性...利用超声波驻波声场的声能量密度在空间呈周期分布的性质,结合纹影法,对空气介质中28 k Hz超声波形成的驻波声场进行成像,使得超声波驻波声场的某些特性可视化,进而更加精准测量其波长和声速值。用光线折射几何理论证明了光的不均匀性所导致的光的折射和弯曲程度与x、y平面内各自折射率梯度成正比,并推导了光线的偏折角计算公式。为使图像更加形象可视,在MATLAB中先对纹影图像做灰度直方图均衡化,再进行灰度-颜色映射处理,得到了较好伪彩色纹影图,使实验数据测量更加便利。最后利用本文方法推导了声速测量公式,准确测量了速度值,并用数理方法分析了仪器系统的灵敏度。展开更多
The three-dimensional visualization of flow and screech-tone emission from an underexpanded circular jet is first investigated experimentally using high-speed cross-schlieren imaging and microphone measurements in the...The three-dimensional visualization of flow and screech-tone emission from an underexpanded circular jet is first investigated experimentally using high-speed cross-schlieren imaging and microphone measurements in the cross-sectional planes along the jet axis. This experimental technique allows the visualization of the shock-cell structure, directivity of sound intensity, and frequency spectrum in the cross-sectional planes of the screeching jet. The high-speed cross-schlieren observation of the screeching jet shows the occurrence of an asymmetrical shock-cell structure that is generated by the flapping mode in the screeching jet. This contributes to the generation of a screech tone propagating upstream along the jet axis and non-uniform sound intensities around the jet in circumferential direction. These observations by high-speed cross</span><span style="white-space:normal;font-size:10pt;font-family:"">-</span><span style="white-space:normal;font-size:10pt;font-family:"">schlieren imaging were validated by the microphone measurements.展开更多
Based on schlieren imaging method the shock wave generated by diesel injector has been investigated,and the influences of ambient gas property, the progress of the spray, ambient gas density and ambient gas temperatur...Based on schlieren imaging method the shock wave generated by diesel injector has been investigated,and the influences of ambient gas property, the progress of the spray, ambient gas density and ambient gas temperature on shock wave have been analyzed. The results show that:the images of spray shock wave are cleaner using sulfur hexafluoride(SF6) as ambient gas than using the nitrogen(N2); at the beginning of injection, shock wave phenomenon does not generate immediately as the fuel leave the nozzle because of the needle movement, and the hesitation is decided by the injection condition and characteristics of injector. The generation of shock wave in the spray tip and the detachment of shock wave from the spray tip show little effect on the spray macroscopic characteristics. The ambient gas density and temperature have a significant effect on the maximum of spray tip velocity, types of shock wave and the detachment timing of shock wave from the spray tip.展开更多
文摘利用超声波驻波声场的声能量密度在空间呈周期分布的性质,结合纹影法,对空气介质中28 k Hz超声波形成的驻波声场进行成像,使得超声波驻波声场的某些特性可视化,进而更加精准测量其波长和声速值。用光线折射几何理论证明了光的不均匀性所导致的光的折射和弯曲程度与x、y平面内各自折射率梯度成正比,并推导了光线的偏折角计算公式。为使图像更加形象可视,在MATLAB中先对纹影图像做灰度直方图均衡化,再进行灰度-颜色映射处理,得到了较好伪彩色纹影图,使实验数据测量更加便利。最后利用本文方法推导了声速测量公式,准确测量了速度值,并用数理方法分析了仪器系统的灵敏度。
文摘The three-dimensional visualization of flow and screech-tone emission from an underexpanded circular jet is first investigated experimentally using high-speed cross-schlieren imaging and microphone measurements in the cross-sectional planes along the jet axis. This experimental technique allows the visualization of the shock-cell structure, directivity of sound intensity, and frequency spectrum in the cross-sectional planes of the screeching jet. The high-speed cross-schlieren observation of the screeching jet shows the occurrence of an asymmetrical shock-cell structure that is generated by the flapping mode in the screeching jet. This contributes to the generation of a screech tone propagating upstream along the jet axis and non-uniform sound intensities around the jet in circumferential direction. These observations by high-speed cross</span><span style="white-space:normal;font-size:10pt;font-family:"">-</span><span style="white-space:normal;font-size:10pt;font-family:"">schlieren imaging were validated by the microphone measurements.
基金supported by the National Natural Science Foundation of China (51076118, 51006075)the Fundamental Research Funds for the Central Universities (1700219089)+1 种基金China Postdoctoral Science Foundation (2013M531209)Shanghai Rising-Star Program (11QH1402500)
文摘Based on schlieren imaging method the shock wave generated by diesel injector has been investigated,and the influences of ambient gas property, the progress of the spray, ambient gas density and ambient gas temperature on shock wave have been analyzed. The results show that:the images of spray shock wave are cleaner using sulfur hexafluoride(SF6) as ambient gas than using the nitrogen(N2); at the beginning of injection, shock wave phenomenon does not generate immediately as the fuel leave the nozzle because of the needle movement, and the hesitation is decided by the injection condition and characteristics of injector. The generation of shock wave in the spray tip and the detachment of shock wave from the spray tip show little effect on the spray macroscopic characteristics. The ambient gas density and temperature have a significant effect on the maximum of spray tip velocity, types of shock wave and the detachment timing of shock wave from the spray tip.
