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Skin friction drag reduction in turbulent flow using spanwise traveling surface waves

机译:使用翼展方向传播的表面波减少湍流中的皮肤摩擦阻力

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A major technological driver in current aircraft and other vehicles is the improvement of fuel efficiency. One way to increase the efficiency is to reduce the skin friction drag on these vehicles. This experimental study presents an active drag reduction technique which decreases the skin friction using spanwise traveling waves. A novel method is introduced for generating traveling waves which is low-profile, non-intrusive, and operates under various flow conditions. This wave generation method is discussed and the resulting traveling waves are presented. These waves are then tested in a low-speed wind tunnel to determine their drag reduction potential. To calculate the drag reduction, the momentum integral method is applied to turbulent boundary layer data collected using a pitot tube and traversing system. The skin friction coefficients are then calculated and the drag reduction determined. Preliminary results yielded a drag reduction of ≈5% for 244Hz traveling waves. Thus, this novel wave generation method possesses the potential to yield an easily implementable, non-invasive drag reduction technology.
机译:当前飞机和其他车辆的主要技术驱动因素是燃油效率的提高。一种提高效率的方法是减少这些车辆上的皮肤摩擦阻力。该实验研究提出了一种主动减阻技术,该技术使用翼展方向行波减小了皮肤摩擦。引入了一种新颖的产生行波的方法,该行波是低剖面的,非侵入的并且在各种流动条件下运行。讨论了这种波产生方法,并给出了产生的行波。然后在低速风洞中测试这些波浪,以确定其减阻潜力。为了计算减阻,将动量积分方法应用于使用皮托管和横移系统收集的湍流边界层数据。然后计算皮肤摩擦系数并确定减阻。初步结果对244Hz行波产生了约5%的阻力减小。因此,这种新颖的波浪产生方法具有产生易于实施的非侵入性减阻技术的潜力。

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