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Robustly optimal wind turbine for swirl expansion and decay

机译:极佳的风力涡轮机,可用于涡旋膨胀和衰减

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摘要

The wind turbine optima of propeller actuator disc theories are problematic. The large optimal windmill interference doubles the wake area from the vortex cylinder used to justify the propeller blade element momentum (BEM) theory. The general momentum (GM) theory incorporates expansion, but its optimum windrotor power blows up below a tip speed ratio of about unity where the BEM and experimental optima are low. Even without expansion, the GM and vortex theory optimum can still affect infinitely more gross power flux than in undisturbed wind. The inner massive swirl of their optimal wake is unstable or unrealizable by many indicators. Rather than a cylindrical wake, the BEM is better founded on negligible suction from low swirl in a predominately axial wake expanded after instability and bursting of the hub vorticity outwards to cancel the axial component of the tip vorticity. If moderate swirl at outer high speed ratios can expand first with pressure regain, the optimum local power refines up to 5 per cent higher. Then only as this expanded outer axial vorticity is finally cancelled to relieve the suction from the swirl does the inner BEM flow slow and expand. The inner and outer axial velocities are equal with no radial velocity at local speed ratio 0.57 in the optimal rotor. Direct experimental verification of this dissipated expanded swirl head (DESH) refinement of the BEM is proposed further to support from measurements and computations in the literature. The design blade chord and pitch that make the DESH optimum robust to small changes in windspeed are little changed from the time-proven BEM design, whereas the GM robust chord has a singularity.
机译:螺旋桨致动器盘理论的风力涡轮机优化存在问题。最佳的大风车干扰使用于证明螺旋桨叶片元素动量(BEM)理论合理性的涡流圆柱的尾流面积加倍。通用动量(GM)理论结合了膨胀,但是其最佳风轮机功率在BEM和实验最优值较低的叶尖速度比低于约1时爆炸。即使没有扩展,与不受干扰的风相比,GM和涡旋理论的最优值仍然可以无限地影响更大的总功率通量。它们的最佳尾流内部大量漩涡不稳定或无法通过许多指标实现。 BEM不是圆柱形尾流,而是更好地建立在低涡流可忽略不计的吸力基础上,该不稳定涡流在不稳定性和轮毂涡流向外爆发以抵消尖端涡流的轴向分量后膨胀为主导的轴向尾流中。如果在较高的速比下适度的涡流能够随着压力的恢复而首先扩大,则最佳局部功率可提高多达5%。然后,只有当最终消除此扩展的外部轴向涡旋以减轻旋流的吸力时,内部BEM的流动才会变慢并扩展。在最佳转子中,内部和外部轴向速度相等,在局部速度比为0.57时没有径向速度。 BEM的耗散膨胀旋流头(DESH)改进的直接实验验证被提出,以进一步支持文献中的测量和计算。使DESH在风速变化很小时具有最佳鲁棒性的设计叶片弦和螺距与久经考验的BEM设计相比变化不大,而GM鲁棒弦却具有奇异之处。

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