留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

大弯角扩压叶栅吸力面全域压力分布的PSP实验

高丽敏 高杰 王欢 周强 刘波

高丽敏, 高杰, 王欢, 周强, 刘波. 大弯角扩压叶栅吸力面全域压力分布的PSP实验[J]. 航空动力学报, 2011, 26(9): 2061-2067.
引用本文: 高丽敏, 高杰, 王欢, 周强, 刘波. 大弯角扩压叶栅吸力面全域压力分布的PSP实验[J]. 航空动力学报, 2011, 26(9): 2061-2067.
GAO Li-min, GAO Jie, WANG Huan, ZHOU Qiang, LIU Bo. PSP experiment of global surface pressure distribution on suction surface of compressor cascade with large curved angle[J]. Journal of Aerospace Power, 2011, 26(9): 2061-2067.
Citation: GAO Li-min, GAO Jie, WANG Huan, ZHOU Qiang, LIU Bo. PSP experiment of global surface pressure distribution on suction surface of compressor cascade with large curved angle[J]. Journal of Aerospace Power, 2011, 26(9): 2061-2067.

大弯角扩压叶栅吸力面全域压力分布的PSP实验

基金项目: 国家自然基金(51076132); 航空基金(2010ZB53014); 西北工业大学基础研究基金; 2010年度新世纪人才计划

PSP experiment of global surface pressure distribution on suction surface of compressor cascade with large curved angle

  • 摘要: 基于自行组建的PSP(pressure sensitive paint)测量系统,采用中国科学院化学研究所PSP,实验测量了来流马赫数分别为0.4和0.5时大弯角扩压叶栅叶片吸力面全域压力分布,并与传统测压技术所得结果进行了比较.研究结果表明:①采用PSP技术测量可以获得叶片表面全域的连续压力分布,具有空间分布率高、定量测量的特点;②叶片中部PSP测量压力值与压力扫描阀结果吻合得非常好,但受到叶片吸力面曲率的影响,叶片前缘与尾缘附近的误差较大,最大误差为4.48%;③随着来流速度的提高,PSP与压力扫描阀之间的误差逐渐减小.

     

  • [1] 刘波,周强,靳军,等.压力敏感涂料技术及其应用[J].航空动力学报, 2006,21(2):225-233. LIU Bo,ZHOU Qiang,JIN Jun,et al.Applications of pressure-sensitive paint technique[J].Journal of Aerospace Power,2006,21(2):225-233.(in Chinese)
    [2] Peterson J I,Fitzgerald R V.New technique of surface flow visualization based on oxygen quenching of fluorescence[J].Rev.Sci.Instrum., 1980,51(5):670-671.
    [3] Sakaue H,Gregory J W,Sullivan J P.Porous pressure sensitive paint for characterizing unsteady flow fields[J].AIAA Journal,2002,40(6):1094-1098.
    [4] Basu B J,Anandan C,Rajam K S.Study of the mechanism of degradation of pyrene-based pressure sensitive paints [J]. Sensors and Actuators B:Chemical,2003,94(3):257-266.
    [5] Bencic T J.Application of pressure-sensitive paint to ice-accreted wind tunnel models .AIAA-2000-0834,2000.
    [6] Fonov S D,Goss L P,Jones J W,et al.Surface pressure and shear force fields measurements using elastic polymeric film //The 11th International Symposium on Flow Visualization.IN,USA:IOS Press,2004:9-12.
    [7] Engler R H,Klein C.DLR PSP system:intensity and lifetime measurements //ICIASF'97 Record,International Congress on Instrumentation in Aerospace Simulation Facilities.CA,USA:IEEE ,1997:46-56.
    [8] Asai K.Status of pressure sensitive paint technology at national aerospace laboratory //18th International Congress on Instrumentation in Aerospace Simulation Facilities (ICIASF).Toulouse,France:IEEE,1999:15.1-15.11.
    [9] Nakakita K,Asai K.Pressure-sensitive paint application to a wing-body model in a hypersonic shock tunnel .AIAA-2002-2911,2002.
    [10] Bencic T J.Rotating pressure and temperature measurements on scale-model fans using luminescent paints .AIAA Paper,98-3452,1998.
    [11] Lepicovsky J,Bencic T J.Use of pressure-sensitive paint for diagnostics in turbomachinery flows with shocks[J].Experiments in Fluids,2002,33(4):531-538.
    [12] Engler R H,Klein C,Trinks O.Pressure sensitive paint systems for pressure distribution measurements in wind tunnels and turbomachines[J].Meas.Sci.Technol.,2000,11 (7):1077-1085.
    [13] 高丽敏,王欢,刘波,等.测量系统特性对压敏涂料校准影响的实验研究[J].航空学报,2010,31(1):76-81. GAO Limin,WANG Huan,LIU Bo,et al.Experimental of study influence of measurement system characteristics on pressure-sensitive paint calibration[J].Acta Aeronautica et Astronautica Sinica,2010,31(1):76-81.(in Chinese)
    [14] 金熹高,林勇,史燚,等.一类芘衍生物及其制备方法与应用:中国,200610112965.5 .2008-03-19. JIN Xigao,LIN Yong,SHI Yi,et al.The preparation method and application of pyrene derivatives:China,200610112965.5 .2008-03-19(in Chinese).
    [15] 张永存,邢汉奇,赵文涛,等.光学压力测量技术的应用研究 //第六届全国实验流体力学学术会议论文集.太原:中国力学学会、中国空气动力学学会,2004:388-391. ZHANG Yongcun,XING Hanqi,ZHAO Wentao,et al.Application of optical pressure measurement //The Sixth Chinese Conference of Experiments in Fluid Mechanics Papers.Taiyuan:The Chinese Society of Theoretical and Applied Mechanics,Chinese Aerodynamics Research Society,2004:388-391.(in Chinese)
    [16] 程厚梅,张永存,陈柳生.光学涂层测压技术 //2003空气动力学前沿研究论文集.北京:中国空气动力学学会,2003:108-115. CHEN Houmei,ZHANG Yongcun,CHEN Liusheng.The optical pressure paint measurement technique //2003 Aerodynamics Former Research Papers.Beijing:Chinese Aerodynamics Research Society,2003:108-115.(in Chinese)
    [17] 郑立新,郝重阳,刘波,等.压力敏感涂料内流场测量系统及涂料校准[J].实验流体力学,2008,22(3):86-93. ZHENG Lixin,HAO Chongyang,LIU Bo,et al.Construction of pressure-sensitive paint measurement system and calibration for homemade paint[J].Journal of Experiments in Fluid Mechanics,2008,22(3):86-93.(in Chinese)
    [18] ZHOU Qiang,LIU Bo,GAO Limin,et al.Pressure measurement on suction surface of a single vane using pressure-sensitive paint[J].Chinese Journal of Aeronautics,2009,22(2):138-144.
  • 加载中
计量
  • 文章访问数:  1945
  • HTML浏览量:  259
  • PDF量:  16
  • 被引次数: 0
出版历程
  • 收稿日期:  2010-09-21
  • 修回日期:  2011-06-01
  • 刊出日期:  2011-09-28

目录

    /

    返回文章
    返回