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摘要:
Two-dimensional critical nozzle flows at low Reynolds numbers are visualized by the rainbow schlieren deflectometry. Experiments have been performed in a region of overexpanded nozzle flow. The variation of the shock structure against the back pressure ratio can be clearly visible with color gradation. Static pressure rises due to the shock-induced flow separation are compared with the previous theories. The unsteady characteristics of overexpanded critical nozzle flows at low Reynolds numbers are quantitatively and qualitatively visualized using laser schlieren and Mach-Zehnder interferometer systems combined with a high-speed digital camera. It was found that an oscillating normal shock wave appears inside the nozzle, and that the shock wave has a specified dominant frequency. Also the time-history of the oscillating shock wave is obtained from both the systems and compared with each other.
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篇名 Optical Measurements of Shock Waves in Critical Nozzles at Low Reynolds Numbers
来源期刊 流量控制、测量及可视化(英文) 学科 物理学
关键词 Compressible FLOW Micro Nozzle Flows Optical FLOW Visualization RAINBOW SCHLIEREN DEFLECTOMETRY MACH-ZEHNDER INTERFEROMETRY Shock Wave Oscillation FLOW Separation
年,卷(期) 2017,(2) 所属期刊栏目
研究方向 页码范围 36-50
页数 15页 分类号 O35
字数 语种
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研究主题发展历程
节点文献
Compressible
FLOW
Micro
Nozzle
Flows
Optical
FLOW
Visualization
RAINBOW
SCHLIEREN
DEFLECTOMETRY
MACH-ZEHNDER
INTERFEROMETRY
Shock
Wave
Oscillation
FLOW
Separation
研究起点
研究来源
研究分支
研究去脉
引文网络交叉学科
相关学者/机构
期刊影响力
流量控制、测量及可视化(英文)
季刊
2329-3322
武汉市江夏区汤逊湖北路38号光谷总部空间
出版文献量(篇)
98
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0
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0
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