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Force prediction during transverse and vortex gust encounters

机译:横向和涡旋阵风相遇时的力预测

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This paper proposes a flowfield-based force prediction method for both transverse and vortex gust encounters, and examines the behavior of the maximum lift coefficient experienced during the transverse gust encounters. A sine-squared transverse gust was created in a water towing tank by using a water jet, whilst a vortex gust was created in a water channel by rotation of an upstream gust generator plate. Forces and flowfields were acquired for both gust types and examined. Average velocity variations in time were obtained along an upstream line, and variations in the effective angle of attack and lift coefficient were then computed based on these average velocities. A sensitivity study was performed, and coupling between the wing and the transverse gust was found to be important. For both gust types, lift coefficients from the measurements and the predictions were found to agree well with each other if the prediction results were to multiplied with the span of the wing. The transients in the lift force were observed to match the variations in the effective angle of attack. Furthermore, the peak lift coefficient experienced by a wing encountering sine-squared transverse gust was found to depend on the maximum effective angle of attack rather than individual values of the geometric angle of attack or the gust ratio.
机译:本文提出了一种基于流场的横向和涡流阵风力预测方法,并研究了横向阵风遇到的最大升力系数的行为。通过使用喷水器在拖水罐中产生正弦平方横向阵风,同时通过旋转上游阵风发生器板在水通道中产生涡旋阵风。获得了两种阵风类型的力和流场并进行了检查。沿上游线获得了时间的平均速度变化,然后根据这些平均速度计算了有效迎角和升力系数的变化。进行了敏感性研究,并且发现机翼和横向阵风之间的耦合很重要。对于两种阵风类型,如果将预测结果与机翼跨度相乘,则发现来自测量值和预测值的升力系数彼此吻合良好。观察到提升力的瞬变与有效迎角的变化相匹配。此外,发现机翼遇到正弦平方横向阵风时所经历的峰值升力系数取决于最大有效攻角,而不是取决于几何攻角或阵风比的各个值。

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