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Unsteady Force Production on a Flat Plate Wing by Large Transverse Gusts and Plunging Maneuvers

机译:大型横向阵风和切入动作在平板机翼上产生的非定常力

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摘要

The transient forces produced by large-amplitude transverse gust encounters and plunge maneuvers were studied experimentally in a water-filled towing tank. Forces were measured as a flat plate wing with an aspect ratio of four was towed through a fluid gust and as the same wing performed plunge maneuvers which matched the shape of the gust velocity profile. The transient velocity in each case conformed to the sine-squared profile, and the peak transient velocities were of the same order of magnitude as the steady towing velocities. In most cases, the wing pitch angle was high enough to cause constant flow separation. Even at low wing pitch angles, the increase in flow incidence angle by the transverse gust or plunge velocity was enough to cause flow separation. Transient force magnitudes were shown to increase with increasing stream-normal velocity for both the gust encounters and plunge maneuvers. Transient forces varied with increasing wing pitch angle during gust encounters but not during plunge maneuvers. Force histories in each case were compared to predictions made by existing small-perturbation force models, and adaptations were made to those models based on physical interpretation of the observed characteristics. Measured forces in both the gust encounters and the plunge maneuvers were found to correspond more closely to predictions made based on attached flow than on separated flow, which supports the suggestion that the presence of a leading edge vortex significantly augments the transient lift. Additionally, a large trailing edge vortex forms at the end of the gust encounter which temporarily reduces the force production below the steady-state values. This was not observed in the plunge maneuver force histories, which were much closer to quasi-steady than were the gust encounter force histories. This analysis contributes to the understanding of unsteady force production in large-amplitude events, and in particular in conditions with separated flow, the behaviors of which are not adequately captured by existing small-perturbation models.
机译:在充满水的拖船中,对大振幅横向阵风遭遇和突降动作产生的瞬态力进行了实验研究。测量力时,将一长宽比为4的平板机翼拖曳通过一阵阵阵风,并在同一条机翼上执行与阵风速度曲线形状相匹配的跳水动作。每种情况下的瞬态速度都符合正弦平方曲线,并且峰值瞬态速度与稳定牵引速度处于相同的数量级。在大多数情况下,机翼的俯仰角足够大,可以引起恒定的气流分离。即使在低机翼俯仰角下,由于横向阵风或突降速度引起的流入射角的增加也足以引起流分离。结果表明,阵风遇到和突降动作时,瞬态力的大小都随着流法向速度的增加而增加。在阵风遇到时,瞬态力随机翼俯仰角的增加而变化,但在俯冲演习中,瞬态力却没有。将每种情况下的力历史与现有的小扰动力模型所做的预测进行比较,并根据对所观察特征的物理解释对这些模型进行了调整。发现阵风遭遇和俯冲演习中的测得力与基于附着流的预测相比,与基于分离流的预测更接近,这表明前缘涡旋的存在会显着增加瞬时升力。另外,阵风遭遇结束时会形成较大的后缘涡流,这会暂时将力产生降低至稳态值以下。在骤降机动力历史中没有观察到这一点,与阵风遭遇力历史相比,它们更接近准稳态。这种分析有助于理解大振幅事件中的非定常力产生,特别是在流动分开的条件下,其行为不能被现有的小扰动模型充分捕获。

著录项

  • 作者

    Perrotta, Gino M.;

  • 作者单位

    University of Maryland, College Park.;

  • 授予单位 University of Maryland, College Park.;
  • 学科 Aerospace engineering.
  • 学位 Ph.D.
  • 年度 2017
  • 页码 134 p.
  • 总页数 134
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

  • 入库时间 2022-08-17 11:36:46

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