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UNSTEADY AERO-HYDRODYNAMIC CHARACTERISTICS OF WING STRUCTURES AT THE INTERACTION WITH HARMONIC GUST

机译:谐波阵风相互作用翼结构的不稳定空气流体动力学特性

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The theoretical and experimental investigating results of unsteady aero-hydrodynamic characteristics (AHCh) of wings conducted in the wind tunnel are presented in the paper. The task of investigations is the measurement of moment and force loads on the wing models at the influence of harmonic air gust. The velocity pulsations of flow were created by specially designed vortical generator, which allowed to disturb the flow in the wide range of Strouhal numbers. The results of experiments have shown that the relative sizes of a wing very essentially influence on the amplitude of the lifting force in the large frequency range of velocity pulsations of flow and well-known classic Sirs function for infinite wings are not applicable for the real wing structures. The developed PC program and received tests dependence of lifting force coefficient versus the numbers of Strouhal are recommended for use in calculating models of ship's wing elements for authentic determination of their AHCh at the designing.
机译:在纸上提出了在风隧道中进行的翅膀的不稳定气流特性(AHCH)的理论和实验研究结果。调查的任务是测量谐波空气阵风的机翼模型上的力矩和力量。通过专门设计的涡流产生的流程速度脉动,可使距离斯特鲁姆数量广泛的流量扰乱流动。实验结果表明,机翼的相对尺寸基本上影响了对无限翼的流动和公知的经典SIRS函数的大型速度脉动的大频率范围内的提升力范围的幅度不适用于真正的机翼结构。建立的PC程序和接收的升降力系数对依赖性的测试依赖性与Strouhal的数量建议用于计算船舶机翼元素的模型,以便在设计时确定其AHCH的答钟。

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