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应用压力敏感涂料测量孤立叶片吸力面压力(英文)
引用本文:周强,刘波,高丽敏,陈柳生,史淼.应用压力敏感涂料测量孤立叶片吸力面压力(英文)[J].中国航空学报,2009,22(2):138-144.
作者姓名:周强  刘波  高丽敏  陈柳生  史淼
作者单位:Zhou Qiang,Liu Bo,Gao Limin(National Science and Technology Keystone Lab of Aerodynamics for Aerofoil and Cascade,Northwestern Polytechnical University,Xi'an 710072,China);Chen Liusheng,Shi Miao(Institute of Chemistry,Chinese Academy of Science,Beijing 100190,China) 
基金项目:National Natural Science Foundation of China (50476071, 10577020)
摘    要:以国产温度不敏感的荧光压力敏感涂料和自主建立的测量系统为基础,应用基于光强的压力敏感涂料测量技术获得了叶栅风洞中孤立叶片吸力面的压力分布。实验测量分别在叶栅风洞出口处气流速度0.3和0.4马赫条件下进行,叶片攻角–12°,大气温度与压力分别为15 ℃和95.4kPa。实验叶片吸力面有4排10列测压孔,弯度约40°左右,叶片连同基座被固定在叶栅风洞出口处的下导流档板上,以方便采集荧光图像。实验测量中还同时采用了静压扫描装置进行常规压力测量,以便进行数据对比。在理论与方法确立方面,对基于光强的测量方法进行了回顾并针对自主建立的测量系统提出采用事后校准的方式进行先验校准,以消除校准与测量中参考压力不一致所引起的误差;提出了荧光图像后处理过程的实施步骤及图像对准的操作方法以进一步提高测量的准确性。压力敏感涂料测量所获得的压力值与静压扫描所得数值之间的误差在7%之内,说明实验测量是有效可信的。

收稿时间:28 March 2008

Pressure Measurement on Suction Surface of a Single Vane Using Pressure-sensitive Paint
Zhou Qiang,Liu Bo,Gao Limin,Chen Liusheng,Shi Miao.Pressure Measurement on Suction Surface of a Single Vane Using Pressure-sensitive Paint[J].Chinese Journal of Aeronautics,2009,22(2):138-144.
Authors:Zhou Qiang  Liu Bo  Gao Limin  Chen Liusheng  Shi Miao
Institution:1. National Science and Technology Keystone Lab of Aerodynamics for Aerofoil and Cascade, Northwestern Polytechnical University, Xi''an 710072, China;2. Institute of Chemistry, Chinese Academy of Science, Beijing 100190, China
Abstract:Global pressure distribution on the suction surface of a single vane in a transonic cascade wind tunnel is measured with the help of intensity-based pressure-sensitive paint (PSP) technique using a type of temperature-insensitive fluorescent paint and a self-made measurement system. This measurement is conducted at the outlet of the cascade wind tunnel at the Mach numbers 0.3 and 0.4, attack angle about ?20°, ambient pressure 95.4 kPa and temperature 15 °C. The vane under study owns a large camber angle of about 40° and 4×10 pressure ports on its suction surface with a steel cubic stand attached. It is fixed vertically on the lower guide steel plate at the outlet through the stand for convenient acquisition of images. Conventional electronic static pressure (ESP) measurement is also fulfilled simultaneously with an ESP scanner for comparison. The method of intensity-based PSP technique is introduced, especially, with the self-made PSP system. The operating sequence of PSP measurement for improved accuracy is also proposed. The practical steps of image processing are described. As an image registration, target alignment is introduced after the 4×10 pressure ports have been selected as targets. The comparison of PSP results with ESP data shows that the maximum error remains within 6.5%.
Keywords:turbomachinery  pressure measurement  pressure-sensitive paint  pressure distribution  cascade wind tunnel  suction surface of vane  image registration
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