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Enforcement of Flow-Induced Oscillations of a Circular Cylinder due to Interference Effects: Numerical Simulations and Experimental Studies

机译:干涉效应引起的圆柱体流致振荡的增强:数值模拟和实验研究

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The enforcement of flow induced oscillations of a spring mounted circular cylinder (d_(cyl)) due to the presence of a fixed square cylinder (d_(s.cyl)) is investigated. An integrated approach takes place by means of 2D CFD simulations and experimental studies in the wind tunnel. The results show that a reduction of the square cylinder distance (g) leads to a higher oscillation of the upstream cylinder (until a critical distance is reached). Furthermore, there is an enlargement of the flow velocity region where lock-in takes place (factor 4 at g/d_(cyl) = 0.8). The main reason for those phenomena that can be found is the raising pressure field downstream of the cylinder due to the square cylinder interference. This increased pressure field leads to a reduction of the separation angle which controls the lift force of the upstream cylinder. The alternating vortices are now farther away from one another what increases the time of their energy absorption before they cut each other off. The reduced vortex interaction leads to a slower rise of the phase angle between lift force and cylinder movement with increasing flow velocity. Hence the vortex separation pattern remains longer in the 2S mode where higher lift forces occur than in the self-limiting 2P mode. Therefore the leaving of the lock-in region at a critical phase angle can be delayed.
机译:研究了由于存在固定的方形圆柱体(d_(s.cyl))而导致弹簧安装的圆柱体(d_(cyl))的流动引起的振荡的执行情况。通过风洞中的2D CFD模拟和实验研究,实现了一种集成方法。结果表明,减小方形气缸距离(g)会导致上游气缸的更高振动(直到达到临界距离)。此外,发生锁定的流速区域扩大(g / d_(cyl)= 0.8时的系数4)。可以发现这些现象的主要原因是由于方形气缸的干扰,气缸下游的压力场升高。该增加的压力场导致分离角的减小,该分离角控制上游气缸的升力。现在,交替的涡流彼此之间距离越来越远,这增加了它们彼此切断之前的能量吸收时间。减小的涡流相互作用导致提升力和气缸运动之间的相角随流速的增加而缓慢增加。因此,在产生更高升力的2S模式下,涡流分离模式比在自限2P模式下保持更长的时间。因此,可以延迟在临界相位角处的锁定区域的离开。

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