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Boundary element simulation of inviscid flow around an oscillatory foil with vortex sheet

机译:带有涡旋片的振荡箔片周围无粘性流的边界元模拟

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The dynamic performance of a rigid foil with harmonic vertical and rotational motions in fluid flow has been studied through velocity potential theory. A boundary element based time stepping scheme is introduced to simulate the flow around the foil and the vortex wake. The body surface condition is satisfied on the exact foil surface and the motion and deformation of the wake sheet shed at the trailing edge is tracked. Kelvin condition is satisfied and a Kutta condition for the unsteady motion is proposed to circumvent the singularity at the trailing edge. Point vortex, which is reduced from wake vortex dipole, is introduced to approximate the vorticity. The performance of foil NACA0012 with harmonic vertical and rotational motions are studied extensively; the propulsion/swimming mode, energy harvesting mode and the flying mode are analysed in detail.
机译:通过速度势理论研究了具有谐波垂直和旋转运动的刚性箔片在流体中的动态性能。引入了基于边界元素的时间步进方案,以模拟围绕箔片和涡流绕过的流动。在精确的箔片表面上满足了车身表面条件,并跟踪了尾缘处脱落的尾流板的运动和变形。满足开尔文条件,并提出了用于非定常运动的Kutta条件,以规避后缘的奇异性。引入了从尾涡旋偶极子减少的点涡,以近似涡度。箔NACA0012在垂直和旋转谐波运动下的性能得到了广泛的研究。详细分析了推进/游泳模式,能量收集模式和飞行模式。

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