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In-Flight Investigations of Tollmien-Schlichting Waves

机译:TOLLMIEN-SCHLICHTING WAVE的飞行中调查

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Flight tests were performed in order to learn more about the technically important case of naturally occurring Tollmien-Schlicliting waves in boundary layer transition. A multi-element hot-film array, placed on the right hand wing of the flying test bed LFU-205, was used to sense skin friction fluctuations provoked by Tollmien-Schlichting disturbances propagating in the laminar boundary layer. Fourier analysis in time and space of the experimental data revealed that a broadband spectrum of 2d and 3d Tollmien-Schlichting waves is involved in the signals, typical for wave packets. Occurrence of these wave packets happens stochastically and it was found that they vary in intensity as well as in their spanwise extent. Examination of signal time histories from sensors distributed in chordwise direction showed that breakdown to turbulence, indicated by spikes in the signal, starts from within the wave packets with the strongest amplitudes.
机译:进行飞行测试,以便了解有关在边界层转换中自然发生的Tollmien-Schlicliting波的技术上重要的情况。置于飞行试验台LFU-205的右侧翼上的多元素热膜阵列,用于感测通过在层边界层中传播的Tollmien-Schlichting扰动引发的皮肤摩擦波动。实验数据的时间和空间的傅里叶分析显示,2D和3D Tollmien-Schlichting波的宽带光谱涉及信号,典型的波浪分组。这些波包的发生随机发生,发现它们在强度和跨度范围内变化。从分布在弦方向上分布的传感器的信号时间历史表明,通过信号中的尖峰指示的湍流击穿,从波包内的波包中的具有最强的幅度开始。

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