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Power extraction performance of two semi-active flapping airfoils at biplane configuration

机译:两种半主动扑翼的功率提取性能在双半主动扑翼翼型

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The power extraction performance of two semi-active flapping airfoils at biplane configuration is analyzed in this work through numerical approach. Two NACA0015 airfoils, which are regarded as an energy extraction turbine, are arranged in a biplane configuration to perform forced counter pitching motion and are subsequently induced in a plunging motion. A numerical code based on finite volume method to solve the Navier-Stokes equations coupled with finite center difference method to solve the passive plunging motion governing equation is developed to simulate the interaction between the two semi-active flapping airfoils and fluid. Results show that the semi-active flapping airfoil cannot absorb more power from the fluid with biplane arrangement, but this arrangement is beneficial for the power extraction efficiency of the airfoil. Analysis of the fluid field of the airfoil reveals that the wing-wing interaction can promote the vortex evolution and reduce the vortex magnitude of the suction side of the biplane airfoils with appropriate initial distance (h(s) = 2.5d). As a result, the maximum plunging of the biplane airfoils is smaller than that of the single airfoil. The smaller maximum plunging displacement contributes to the increase in power extraction efficiency.
机译:通过数值方法在这项工作中分析了两种半主动扇形翼型的功率提取性能。被视为能量提取涡轮机的两个NACA0015翼型被布置成双翼膜配置,以进行强制计数器俯仰运动,随后在狭窄的运动中被引起。基于有限体积方法解决与有限中心差分方法求解的Navier-Stokes方程的数值代码开发了用于解决被动泄漏运动控制方程的,以模拟两个半主动扇形翼型和流体之间的相互作用。结果表明,半主动扇形翼型不能用双翼飞机排列吸收更多的功率,但这种布置是有利于翼型的功率提取效率。翼型的流体场的分析表明,翼翼相互作用可以通过适当的初始距离(H(s)= 2.5d)促进涡旋施加的涡流蒸馏并降低所述双翼翼翼型的吸入侧的涡流幅度(H(s)= 2.5d)。结果,双翼翼翼型的最大灌注小于单个翼型的最大灌注。较小的最大急剧位移有助于提高功率提取效率。

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