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Desirable features of an infrared imaging system for aerodynamic research

机译:用于空气动力学研究的红外成像系统的理想功能

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Abstract: Advantage of non-intrusiveness, capability for field measurement, and increased availability of infrared imaging systems have resulted in their wider use for aerodynamic research. However, certain difficulties persist while using currently available systems for such applications. A critical evaluation of the infrared imaging systems is presented on the basis of the state- of-the-art of infrared imaging technology and experiences in wind tunnel and flight testing at NASA's Langley Research Center. The requirements for using infrared thermography as a measurement tool in aerodynamic research are examined in terms of range, sensitivity, and accuracy of temperature measurement, temporal and spatial resolution, and features of target. Deficiencies of present infrared imaging systems are identified, and user precautions to avoid such problems by proper selection and operation of these units are suggested. Different aspects of imager performance such as imager optics, video capabilities, and environmental tolerance are discussed. Electronic data recording and image processing hardware and software requirements are evaluated. Slit response tests and spatial resolution are discussed with the objective of obtaining reliable, accurate, and meaningful information from infrared thermography measurements for aerodynamic studies.!17
机译:摘要:非侵入性,现场测量的能力以及红外成像系统可用性的提高使得它们在空气动力学研究中得到了更广泛的应用。但是,在将当前可用的系统用于此类应用程序时,仍然存在某些困难。根据红外成像技术的最新技术以及美国宇航局兰利研究中心在风洞和飞行测试中的经验,对红外成像系统进行了重要评估。在范围,灵敏度和温度测量精度,时间和空间分辨率以及目标特征方面,对在空气动力学研究中使用红外热成像作为测量工具的要求进行了检查。确定了当前红外成像系统的不足之处,并建议用户采取适当的预防措施,以通过适当选择和操作这些装置来避免此类问题。讨论了成像器性能的不同方面,例如成像器光学器件,视频功能和环境耐受性。评估电子数据记录和图像处理的硬件和软件要求。讨论了狭缝响应测试和空间分辨率,旨在从红外热像仪测量中获得可靠,准确和有意义的信息,以进行空气动力学研究!17

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