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首页> 外文期刊>Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow >Three-dimensional flow structures and unsteady forces on pitching and surging revolving flat plates
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Three-dimensional flow structures and unsteady forces on pitching and surging revolving flat plates

机译:俯仰和旋动旋转平板上的三维流动结构和非定常力

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Tomographic particle image velocimetry was used to explore the evolution of three-dimensional flow structures of revolving low-aspect-ratio flat plates in combination with force measurements at a Reynolds number of 10,000. Two motion kinematics are compared that result in the same terminal condition (revolution with constant angular velocity and 45. angle of attack) but differ in the motion during the buildup phase: pitching while revolving at a constant angular velocity; or surging with a constant acceleration at a fixed angle of attack. Comparison of force histories shows that the pitching wing generates considerably higher forces during the buildup phase which is also predicted by a quasi-steady model quite accurately. The difference in the buildup phases affects the force histories until six chords of travel after the end of buildup phase. In both cases, a vortex system that is comprised of a leading-edge vortex (LEV), a tip vortex and a trailing edge vortex is formed during the initial period of the motion. The LEV lifts off, forms an arch-shaped structure and bursts into substructures, which occur at slightly different phases of the motions, such that the revolving-surging wing flow evolution precedes that of the revolving-pitching wing. The delay is shown to be in accordance with the behavior of the spanwise flow which is affected by the interaction between the tip vortex and revolving dynamics. Further analysis shows that the enhanced force generation of the revolving-pitching wing during the pitch-up phase originates from: (1) increased magnitude and growth rate of the LEV circulation; (2) relatively favorable position and trajectory of the LEV and the starting vortex; and (3) generation of bound circulation during the pitching motion, whereas that of the revolving-surging wing is negligible in the acceleration phase.
机译:层析成像颗粒图像测速技术与10,000雷诺数的力测量相结合,用于探索旋转低纵横比平板的三维流动结构的演变。比较了两种运动运动学,这些运动学在相同的最终条件下(恒定角速度和45度攻角的旋转)但是在建立阶段的运动不同:以恒定角速度旋转时的俯仰;或以固定的迎角不断加速运动。力历程的比较表明,在建立阶段,俯仰翼产生的力要大得多,准稳态模型也非常准确地预测了这一点。累积阶段之间的差异会影响力的历史,直到累积阶段结束后经过六个和弦为止。在这两种情况下,在运动的初始阶段都会形成由前涡流(LEV),尖端涡流和后缘涡流组成的涡流系统。 LEV升空,形成弓形结构,并破裂成子结构,这些子结构出现在运动的稍有不同的阶段,因此旋升式机翼气流的演化先于旋翼式机翼的演化。所显示的延迟与翼展方向流动的行为一致,翼展方向流动受尖端涡旋和旋转动力学之间的相互作用影响。进一步的分析表明,在俯仰阶段旋转俯仰机翼产生的力增强是由于:(1)LEV循环的大小和增长率增加; (2)LEV和起始涡旋的相对有利位置和轨迹; (3)俯仰运动过程中束缚循环的产生,而在加速阶段,旋涡翼的产生是可以忽略的。

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