首页> 外文会议>ASME summer heat transfer conference;HT2009 >HOTWIRE MEASUREMENTS DOWNSTREAM OF A DELTA WINGLET PAIR AT TWO ANGLES OF ATTACK
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HOTWIRE MEASUREMENTS DOWNSTREAM OF A DELTA WINGLET PAIR AT TWO ANGLES OF ATTACK

机译:在两个攻击角度对三角翼小翼对的下行测量

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Hotwire measurements were obtained downstream of a delta winglet pair placed on an unheated flat surface. Time-averaged mean velocity, RMS, fast Fourier transform and instantaneous velocity statistics are examined to gain insight into the effect that a delta winglet pair has on manipulating an otherwise steady baseline flow. Typically, results presented in the literature are in time-averaged form and this implies that the majority of information that relates to enhanced heat transfer, i.e. unsteady flow phenomena, is lost. It is for this reason that the current investigation examines the flow downstream of the vortex generator (VG) with hotwire anemometry so as to achieve good temporal and spatial measurement resolution.The mean velocity and RMS profiles presented at two different Angles of Attack (AoA) provide valuable information on the extent to which the VG manipulates the flow. In the centreline the boundary layer is significantly thinned in comparison to other spanwise locations indicating the presence of the downwash region. The shape of the mean velocity and RMS profiles also indicate the extent to which the vortex structures grow in the spanwise direction with downstream distance from the VG The peak RMS values are shown to increase with downstream distance in some spanwise planes and decrease with downstream distance for other spanwise planes thereby illustrating complex fluid flow interactions.Examining the instantaneous flow features reveals the true nature of the unsteadiness and also elucidates some of the more complex flow phenomena, such as positive spikes found in the near-wall region, that may lead to enhanced heat transfer. It is also observed from the instantaneous velocity traces that large negative spikes are observed in the freestream region close to theboundary layer edge. These structures help to explain the interaction between the near wall and freestream flow field thereby resulting in significantly enhanced mixing.
机译:热线测量是在未加热的平坦表面上的三角翼小翼对的下游进行的。检验了平均时间平均速度,RMS,快速傅立叶变换和瞬时速度统计信息,以洞悉三角翼小翼对对操纵本来稳定的基准流的影响。通常,文献中给出的结果是时间平均形式的,这意味着与增强的热传递有关的大多数信息,即非稳态流动现象,都将丢失。出于这个原因,当前的研究使用热线风速仪检查了涡流发生器(VG)下游的流动,从而获得了良好的时间和空间测量分辨率。 在两个不同的迎角(AoA)处显示的平均速度和RMS曲线提供了有关VG操纵流的程度的有价值的信息。与其他翼展方向位置相比,边界线在中心线明显变薄,表明存在下洗区域。平均速度和RMS曲线的形状还指示了涡旋结构在距VG的下游距离处沿翼展方向增长的程度。在某些翼展方向平面中,RMS峰值显示为随着下游距离的增加而减小,对于其他翼展方向平面由此说明了复杂的流体流动相互作用。 检查瞬时流动特征揭示了不稳定的真实性质,还阐明了一些更复杂的流动现象,例如在近壁区域中发现的正峰值,这可能会导致传热增强。从瞬时速度轨迹还可以观察到,在靠近流场的自由流区域中观察到了较大的负尖峰。 边界层边缘。这些结构有助于解释近壁和自由流流场之间的相互作用,从而显着增强混合效果。

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