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首页> 外文期刊>Applied Ocean Research >Critical angle of attack and the corresponding impact cavity for non-circuitous trajectory of water entry of circular cylinder
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Critical angle of attack and the corresponding impact cavity for non-circuitous trajectory of water entry of circular cylinder

机译:圆柱形圆柱进入非迂回轨迹的临界攻角和相应的冲击腔

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摘要

The critical initial angle of attack that the cylinder can move along the non-circuitous trajectory in water entry is investigated experimentally and numerically. A primary focus is on characterizing the relationship between the initial inclined angle alpha(0) and horizontal velocity u(0) in the parameters space of alpha(0)similar to u(0)/v(0), where u(0)/v(0) is the horizontal velocity u(0) to vertical velocity v(0) ratio. To build a dense initial parameter space to capture the accurate critical curvature boundary (CCB), which is the critical parameters of the cylinder moving along a noncircuitous trajectory, a substantial water entry experiment is performed for the cylinder with different initial inclined angles and horizontal velocities. In this experiment, a high-speed camera is employed to record the position and the inclined angle of the cylinder. In addition, a large eddy simulation method is used to simulate some particular water entry cases that the cylinder initial parameters are near the CCB space. After the analysis, the initial parameter space for the oblique water entry almost locates in the left circuitous space. Based on the equation of the oblique water entry in the parameter space of alpha(0)similar to u(0)/v(0) , an empirical equation of CCB is established by giving a correction item of deviation angle of attack. When the initial parameters of the cylinder satisfy the equation of CCB, the cylinder first moves along the initial line L-u and then along the offset line L-d. The offset distance d(offset), between these two lines first increases with alpha(0) and u(0)/v(0) and then gradually tends to a constant about d(offset)/D = 1, where D is the diameter of the cylinder. Moreover, the simulation results indicate that the pressure distribution on the cylinder surface is affected by the impact velocity, the wettability of the cylinder surface, the initial angle of attack and the distance between the cylinder surface and the pinch-off location.
机译:在实验和数值上研究气缸可以沿着水处理中的非迂回轨迹移动的临界初始攻角。在表征初始倾斜角度α(0)和水平速度u(0)之间的关系的主要焦点在于与u(0)/ v(0)的参数空间中的初始倾斜角度α(0)和水平速度U(0)之间的关系,其中U(0) / V(0)是垂直速度V(0)比的水平速度U(0)。为了构建密集的初始参数空间来捕获精确的临界曲率边界(CCB),该临界曲率边界(CCB)是沿着非迂回轨迹移动的汽缸的临界参数,对于具有不同初始倾斜角度和水平速度的圆柱体进行大量的水入口实验。在该实验中,采用高速摄像机记录圆筒的位置和倾斜角度。此外,大型涡旋仿真方法用于模拟一些特定的水入口壳体,即气缸初始参数靠近CCB空间。分析后,倾斜水入口的初始参数空间几乎位于左侧迂回空间。基于α(0)的参数空间中的倾斜水条目的等式,与U(0)/ V(0)类似,通过给出偏离攻击角度的校正项来建立CCB的经验方程。当汽缸的初始参数满足CCB的等式时,圆筒首先沿着初始线L-U移动,然后沿偏移线L-D移动。偏移距离d(偏移),在这两条线之间首先用α(0)和u(0)/ v(0)增加,然后逐渐倾向于常数(偏移)/ d = 1,其中d是d气缸的直径。此外,模拟结果表明汽缸表面上的压力分布受冲击速度,气缸表面的润湿性,初始迎角和汽缸表面之间的距离和夹紧位置的影响。

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