Zhang Shiyu, Zhao Xuejun, Chen Zelin. Application of surface-heat-flux estimation by measuring model interior temperature in hypersonic wind tunnel tests[J]. Journal of Experiments in Fluid Mechanics, 2015, (2): 61-67. DOI: 10.11729/syltlx20140089
Citation: Zhang Shiyu, Zhao Xuejun, Chen Zelin. Application of surface-heat-flux estimation by measuring model interior temperature in hypersonic wind tunnel tests[J]. Journal of Experiments in Fluid Mechanics, 2015, (2): 61-67. DOI: 10.11729/syltlx20140089

Application of surface-heat-flux estimation by measuring model interior temperature in hypersonic wind tunnel tests

More Information
  • A series of hypersonic wind tunnel tests are implemented to estimate the aero-heat-ing flux of a test plate.The heat flux at the heated surface is not directly measured,but is esti-mated by solving an inverse heat conduction problem (IHCP)based on measured temperature at the back surface or inside of the plate.The most outstanding advantage of this method is that the temperature sensors do not contact with the high temperature outflow directly,but are embed ded inside the plate.Therefore,it provides an alternative approach to estimate the high tempera-ture surface heat flux for practical hypersonic vehicle flight tests.The primary aim of this paper is to verify the applicability of this method to predict the flow characteristics of the outflow filed. The hypersonic wind tunnel tests are implemented in FD-03 WT of China Academy of Aerospace Aerodynamics (CAAA).Some tests apply a smooth plate in general hypersonic wind tunnel tests;and others adopt a test plate bounded with a trip line to interrupt the boundary layer of the plate.As shown in the heat flux estimated results,severe changes in the outflow such as shock waves caused by the trip line can be predicted by the estimated heat flux.
  • Related Articles

    [1]LI Linkai, HUANG Zi, GU Yunsong, PENG Zhenjun, ZHANG Zongyuan, LEI Yu. Development of forebody asymmetric vortex control based on alternating synthetic jet and the verification on model free flight[J]. Journal of Experiments in Fluid Mechanics, 2023, 37(4): 96-104. DOI: 10.11729/syltlx20230042
    [2]ZHANG Yi, PAN Chong, DOU Jianyu, ZHANG Miao. Flowfield and friction characteristics downstream of mirco vortex generator in turbulent boundary layer[J]. Journal of Experiments in Fluid Mechanics, 2023, 37(4): 48-58. DOI: 10.11729/syltlx20230027
    [3]QU Xiaoli, LIU Qin, ZHU Bo, NIE Xutao, WANG Chao. Experimental research and analysis of gust generator for low speed wind tunnel[J]. Journal of Experiments in Fluid Mechanics, 2021, 35(5): 99-105. DOI: 10.11729/syltlx20200114
    [4]WANG Jun, LAI Qingren, KANG Hongming, ZHANG Liu, LI Binbin, ZHAO Lei, JIN Yi. Experimental study on jet turning based on spiral flap[J]. Journal of Experiments in Fluid Mechanics, 2021, 35(5): 47-53. DOI: 10.11729/syltlx20210036
    [5]GAO Limin, LIU Zhe, CAI Ming, LI Haoxue. Study on two-dimensional control technology of flow field in high-load compressor cascade test[J]. Journal of Experiments in Fluid Mechanics, 2021, 35(2): 13-21. DOI: 10.11729/syltlx20200099
    [6]Li Renkang, Wang Rugen, He Cheng, Hu Jiaguo, Ma Caidong, Huang Danqing. Experimental investigation on the effects of vortex generator on corner separation in a high-load compressor cascade[J]. Journal of Experiments in Fluid Mechanics, 2017, 31(6): 22-28, 36. DOI: 10.11729/syltlx20160195
    [7]Zhang Jin, Liu Jingyuan, Zhang Binqian. Experimental and CFD study on the mechanism of supercritical airfoil drag reduction with micro vortex generators[J]. Journal of Experiments in Fluid Mechanics, 2016, 30(4): 37-41. DOI: 10.11729/syltlx20150157
    [8]Ouyang Shaoxiu, Liu Yi, Zhao Xiaoxia. The experimental research on a flow control device of horizontal tail[J]. Journal of Experiments in Fluid Mechanics, 2015, (1): 66-70. DOI: 10.11729/syltlx20130119
    [9]ZHANG Jin, ZHANG Bin-qian, YAN Wen-cheng, DUAN Zhuo-yi, CHEN Ying-chun, JIAO Yu-qin, YU Xin. Investigation of boundary layer separation control for supercritical airfoil using micro vortex generator[J]. Journal of Experiments in Fluid Mechanics, 2005, 19(3): 58-60,84. DOI: 10.3969/j.issn.1672-9897.2005.03.012
    [10]LI Bao-ming, Li Hong-zhi, YUAN Wei-qun. AExperimental studies of ablation-controlled arc discharges in plasma generator[J]. Journal of Experiments in Fluid Mechanics, 2000, 14(4): 14-19. DOI: 10.3969/j.issn.1672-9897.2000.04.003

Catalog

    Article Metrics

    Article views (144) PDF downloads (11) Cited by()
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return
    x Close Forever Close

    重要公告

    www.syltlx.com是《实验流体力学》期刊唯一官方网站,其他皆为仿冒。请注意识别。

    《实验流体力学》期刊不收取任何费用。如有组织或个人以我刊名义向作者、读者收取费用,皆为假冒。

    相关真实信息均印刷于《实验流体力学》纸刊。如有任何疑问,请先行致电编辑部咨询并确认,以避免损失。编辑部电话0816-2463376,2463374,2463373。

    请广大读者、作者相互转告,广为宣传!

    感谢大家对《实验流体力学》的支持与厚爱,欢迎继续关注我刊!


    《实验流体力学》编辑部

    2021年8月13日