Three Component Laser-Doppler-Velocimeter Development for Large Wind Tunnel

U. Seelhorst, K. Butefisch, K. Sauerland
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引用次数: 11

Abstract

Within the scope of a co-operative programme between DLR and US Air Force and the DLr programme co-rot a three component laser- Doppler-velocimeter together with a position monitoring system has to be developed in order to determine the unsteady flow field around a rotating helicopter rotor blade. Most of these measurements have to be performed in the DNW (Deutsch-Niederlaendischer Windkanal.The Netherlands), a large wind tunnel with an open test section of 6m-8m. Experiences from previous tests in the DNW on the same helicopter rotor blade with different LDV set-ups were gained and finally led to a 3 component LDV with a working distance of 5m and a 350 mmaperture receiving optics. By the new set-up it was possible to obtain high quality data although the total laser power does not exceed 3 Watts.
大型风洞用三分量激光多普勒测速仪的研制
在DLR和美国空军以及DLR项目合作项目的范围内,为了确定旋转直升机旋翼叶片周围的非定常流场,必须开发一种三组件激光-多普勒测速仪以及位置监测系统。大多数这些测量必须在DNW (deutschniederlaendischer Windkanal)中进行。荷兰),一个大型风洞,开放测试段为6m-8m。从DNW先前在同一直升机旋翼叶片上使用不同LDV设置的测试中获得经验,并最终导致工作距离为5米的3组件LDV和350毫米孔径接收光学器件。通过新的设置,虽然总激光功率不超过3瓦,但可以获得高质量的数据。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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