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Experimental Study on Cavity Characteristics of Low Speed Water Entry of Cylinder Based on High-Speed Imaging Technology

机译:基于高速成像技术的气缸低速水分腔特性试验研究

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摘要

During the launching of the underwater vehicle especially in air-launching, the water entry problem is complicated. Factors such as nose shape, water entry velocity, water entry angle, surface property and specific gravity will have a profound effect on the cavity shape, which will affect the initial trajectory and attitude of underwater vehicle. A launch platform with variable launch velocity and multiple launch angle is designed and constructed independently. Launch platform, water tank, high-speed camera, floodlights and synchronizing device together constitute the experiment platform. Five kinds of nose shapes with different hemispherical angles are used. A series of experiments are carried out to investigate how nose shape, water entry velocity and water entry angle will affect the cavity characteristics. The conclusions are performed and the three different cavities (flow separation cavity, weak flow separation cavity, cavity behind the moving cylinder) formed during water entry process are observed and analyzed originally.
机译:在推出水下车间特别是在空气发射时,水处理问题很复杂。鼻形,水入口速度,水入口角度,表面特性和比重等因素对腔形来说是深切影响,这将影响水下车辆的初始轨迹和姿态。具有可变启动速度和多个发射角度的发射平台独立设计和构造。发射平台,水箱,高速摄像机,泛光灯和同步装置一起构成实验平台。使用具有不同半球形角度的五种鼻形。进行了一系列实验,以研究鼻子,水入口速度和水入口角如何影响腔特性。已经进行了结论,并且最初观察到在水进入过程中形成的三个不同的腔(流动分离腔,流动分离腔,移动圆筒后面的腔)。

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