...
首页> 外文期刊>Experimental Mechanics >High-Precision Digital Image Correlation for Investigation of Fluid-Structure Interactions in a Shock Tube
【24h】

High-Precision Digital Image Correlation for Investigation of Fluid-Structure Interactions in a Shock Tube

机译:高精度数字图像相关性,用于调查冲击管中的流体结构相互作用

获取原文
获取原文并翻译 | 示例
           

摘要

Background: Structural response measurements are challenging in aerodynamic testing environments due to high-speed requirements, facility vibrations, and the desire for non-intrusive measurements. Objective: This study uses stereo digital image correlation (DIC) to investigate the response of a jointed beam under aerodynamic loading in a shock tube. Methods: The incident shock subjects the beam to an impulsive frontal load followed by periodic transverse loading from vortex shedding. Several considerations necessary to realize high-precision are addressed: first, a hybrid stereo camera calibration accounted for tangential distortions when imaging through thick windows. Second, a measurement bias from Xenon flash-lamp light sources was identified and removed using laser illumination. Third, facility motion was mitigated by vibration isolation and appropriate signal filtering. Finally, aero-optical distortions from turbulence were removed using a low-order reconstruction. Results: The resulting displacement data has a noise floor of approximately +/- 1 mu m at 20 kHz sampling rate. The reduction of primary noise sources allows a transient structural response on the order of 10-40 mu m to be quantified. The highest vibrations occurred when the vortex shedding frequency matched the beam's natural frequency. Conclusion: the noise reduction techniques described allow for structural measurements requiring high-precision, non-intrusive displacement data to be performed in aerodynamic environments.
机译:背景:由于高速要求,设施振动以及对非侵入性测量的需求,结构响应测量在空气动力学测试环境中具有挑战性。目的:该研究使用立体声图像相关(DIC)来研究击向管中的空气动力载荷下的关节光束的响应。方法:入射冲击将光束对脉冲的正载荷进行,然后来自涡旋脱落的周期性横向载荷。解决了实现高精度所需的几个考虑因素:首先,混合立体声相机校准在通过厚窗口成像时占切向扭曲。其次,使用激光照射识别和去除氙闪光灯光源的测量偏压。第三,通过振动隔离和适当的信号滤波来减轻设施运动。最后,使用低阶重建去除来自湍流的航空光学扭曲。结果:所得到的位移数据具有20 kHz采样率的噪声底部约+/-1μm。初级噪声源的降低允许量化10-40μm的瞬态结构响应。当涡流缩小频率与光束的固有频率匹配时发生的最高振动。结论:所描述的降噪技术允许在空气动力学环境中进行高精度,非侵入式位移数据的结构测量。

著录项

相似文献

  • 外文文献
  • 中文文献
  • 专利
获取原文

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号