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Experimental investigation on the steady and unsteady disturbances in a flat plate boundary layer

机译:平板边界层中稳态和非稳态扰动的实验研究

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Recent experiments have shown that miniature vortex generators (MVGs) are coveted devices to stabilize unsteady disturbances in flat plate boundary layers and to delay the onset of turbulence by modulating the base flow in the spanwise direction. The spanwise modulation is a result from the non-modal transient growth of steady and spanwise periodic streamwise vortices being generated by the MVGs. The present experimental investigation aims at studying the transient growth of non-modal disturbances induced by a spanwise periodic array of MVGs and its stabilizing effect on non-linear unsteady disturbances in the boundary layer originating from planar Tollmien-Schlichting (TS) waves. Measurements consist of cross-stream planes at different downstream locations in the boundary layer and a spatio-temporal analysis of different modes of the disturbances is carried out. In the streaky boundary layer generated by the MVGs the fundamental spanwise mode, with the same wavelength as the MVG pairs in the array, and its first harmonic, both undergo transient growth whereas the higher harmonics decay immediately downstream of the array. In the unstable region formed in the wake of the MVG blades, i.e., just downstream of the array, a wide range of spanwise modes contributes to an initial growth in the energy of unsteady disturbances. Similar behavior is observed upstream of branch II position of the neutral stability curve where the unsteady disturbances undergo a second energy growth in the unstable region. It is shown that the spatial gradients of the base flow in the wall-normal and spanwise directions are contributing to the amplification and attenuation of the TS wave disturbances, respectively, in the streaky boundary layer. (C) 2014 AIP Publishing LLC.
机译:最近的实验表明,微型涡旋发生器(MVG)是令人垂涎的设备,可稳定平板边界层中的不稳定扰动并通过在翼展方向上调节基流来延迟湍流的发作。跨度调制是由MVG生成的稳态和跨度周期性流向涡流的非模态瞬态增长的结果。本实验研究旨在研究由MVG的展向周期周期阵列引起的非模态扰动的瞬态增长及其对源自平面Tollmien-Schlichting(TS)波的边界层中非线性非稳态扰动的稳定作用。测量由边界层中不同下游位置处的横流平面组成,并对扰动的不同模式进行了时空分析。在由MVG产生的条纹边界层中,基本的展向模式与阵列中的MVG对具有相同的波长及其一次谐波,都经历瞬态增长,而高次谐波则在阵列下游立即衰减。在MVG叶片的尾部形成的不稳定区域中,即在阵列的下游,大范围的展向模式有助于不稳定波动能量的初始增长。在中性稳定性曲线的分支II位置的上游观察到类似的行为,其中不稳定区域在不稳定区域经历了第二次能量增长。结果表明,在条状边界层中,基流在壁法线方向和翼展方向上的空间梯度分别有助于TS波扰动的放大和衰减。 (C)2014 AIP Publishing LLC。

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