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Windspeed and Flow Angle Measurement by Tracking of a Laser-Induced Breakdown Spark

机译:通过跟踪激光诱发的击穿火花来测量风速和流角

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An experimental measurement of three components of velocity and associated flow angles by optical tracking of the light emitted by a laser-induced breakdown (LIB) spark is described. The measurements were performed in a blowdown wind tunnel at a nominal flow Mach number of 4.38. The tests showed that flow velocity could be accurately measured using the technique, with a demonstrated flow-angle uncertainty of less than ± 0.2° at the Mach 4.38 test condition. Wavefront measurements through the shock of a 20° wedge were also performed, and indicated that the measurements could also be performed through a shock with negligible effect on spark formation due to the much smaller aperture of the LIB laser beam in relation to the wavelength of the shock aero-optical effect.
机译:通过对激光诱导击穿(LIB)火花发出的光进行光学跟踪,描述了速度和相关流角三个分量的实验测量。该测量在排污风洞中以标称流量马赫数为4.38进行。测试表明,使用该技术可以精确地测量流速,在4.38马赫的测试条件下,流角不确定度小于±0.2°。还进行了通过20°楔形波冲击的波前测量,结果表明,由于LIB激光束的孔径相对于激光束的波长要小得多,因此也可以通过冲击对火花形成的影响可忽略不计地进行测量。休克航空光学效果。

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