LI Duo, CAO Junyi, ZHANG Zhengyu, HUANG Xuhui. Applications of modern design of experiment method in transonic wind tunnel[J]. ACTA AERODYNAMICA SINICA, 2018, 36(1): 26-30. DOI: 10.7638/kqdlxxb-2015.0196
Citation: LI Duo, CAO Junyi, ZHANG Zhengyu, HUANG Xuhui. Applications of modern design of experiment method in transonic wind tunnel[J]. ACTA AERODYNAMICA SINICA, 2018, 36(1): 26-30. DOI: 10.7638/kqdlxxb-2015.0196

Applications of modern design of experiment method in transonic wind tunnel

More Information
  • Received Date: November 08, 2015
  • Revised Date: January 25, 2016
  • Available Online: January 07, 2021
  • In order to overcome the shortages of the one factor at a time (OFAT) wind tunnel tests, such as slow test efficiency, neglected variable interaction, and indirect expression of test results, a modern design of experiment (MDOE) method for wind tunnel experiments has been performed in a 2.4m×2.4m transonic wind tunnel. In this paper, the test space dividing, test data number calculating and data point distributing have been illustrated. The aerodynamic coefficients at tested points have been acquired through wind tunnel experiments. The response surface model has been established, and its accuracy has been verified by checking the additional acquisition data points within the 95% confidence interval. The results indicate that the proposed MDOE method only uses 20 percent of data points and 50 percent of experimental time of traditional methods. This method possesses a better performance in describing experiment results, providing response results, and revealing variable interaction relationship.
  • [1]
    张江, 秦永明, 马汉东.亚跨超风洞现代试验设计方法研究[J].空气动力学学报, 2015, 33(3):384-391. http://manu27.magtech.com.cn/Jweb_aas/CN/abstract/abstract11682.shtml
    [2]
    战培国. MDOE风洞试验方法研究[J].航空科学技术, 2011(6):11-14. http://d.wanfangdata.com.cn/Periodical_hkkxjs201106004.aspx
    [3]
    张江, 秦永明, 马汉东.风洞MDOE的形式实验设计方法研究[J].空气动力学学报, 2016, 34(1):59-69. http://manu27.magtech.com.cn/Jweb_aas/CN/abstract/abstract11773.shtml
    [4]
    唐志共, 王文正, 陈功, 等.气动模型在现代气动试验设计中的应用研究[J].空气动力学学报, 2017, 35(2):172-176. http://manu27.magtech.com.cn/Jweb_aas/CN/abstract/abstract11997.shtml
    [5]
    Kaymaz I, McMahon C A. A response surface method based on weighted regression for structural reliability analysis[J]. Probabilistic Engineering Mechanics, 2005, 20(1):11-17. doi: 10.1016/j.probengmech.2004.05.005
    [6]
    Garrent J H. Where and why article neural networks are applicable in civil engineering[J]. Journal of Computing in Civil Engineering, ASCE, 1994, 8(2):129-130. doi: 10.1061/(ASCE)0887-3801(1994)8:2(129)
    [7]
    Erickson G E. Analysis of a split-plot experimental design applied to a low-speed wind tunnel investigation[R]. NASA/TM-20130218013. http://ntrs.nasa.gov/search.jsp?R=20130014844
    [8]
    De Loach R. Applications of modern experiment design to wind tunnel testing at NASA langley research center[C]//36th AIAA Aerospace Sciences Meeting & Exhibit, Reno, Nevada, January 1998, AIAA-1998-0713. doi: 10.2514/6.1998-713
    [9]
    Landman D, Simpson J, Vicroy D, et al. Efficient methods for complex aircraft configuration aerodynamic characterization using response surface methodologies[C]//44th AIAA Aerospace Sciences Meeting & Exhibit, Reno, Nevada, January 2006, AIAA-2006-0922. doi: 10.2514/6.2006-922
    [10]
    马逢时, 周暐.六西格玛管理统计指南:MINITAB使用指导[M].北京:中国人民大学出版社, 2013.
  • Related Articles

    [1]LIU Xiangnan, SHAO Tianshuang, LIU Shaoteng. Analysis of impact and sensitivity of wall interference parameters in wind tunnel test of rotors[J]. ACTA AERODYNAMICA SINICA, 2025, 43(3): 78-86. DOI: 10.7638/kqdlxxb-2024.0157
    [2]ZHANG Zhigang, CHEN Ting, ZHAO Jinshan, ZHU Zhiwei, LIAO Junhao, SHI Yilei, YIN Yanxin, PENG Zhiyu. Infrared thermal tests and analysis of a lifting-body model with gaps[J]. ACTA AERODYNAMICA SINICA, 2024, 42(4): 46-54. DOI: 10.7638/kqdlxxb-2023.0123
    [3]YAN Yu, LU Bo, YANG Xinghua, GUO Hongtao, YU Li. Review on buzz wind tunnel test technology for aircraft control surfaces[J]. ACTA AERODYNAMICA SINICA, 2022, 40(3): 1-9. DOI: 10.7638/kqdlxxb-2021.0303
    [4]WANG Yeteng, SUN Zhenxu, JU Shengjun, WANG Mengying, YANG Guowei. Influence of groove microstructures on the aerodynamic performance of high speed trains under crosswind[J]. ACTA AERODYNAMICA SINICA, 2021, 39(5): 132-141. DOI: 10.7638/kqdlxxb-2021.0149
    [5]WU Jiurong, ZHONG Wenkun, XU An. Wind-induced vibration response analysis of high-rise lattice structure by considering modification effect for three-dimensional spatial and nonlinear vibration mode shape[J]. ACTA AERODYNAMICA SINICA, 2018, 36(6): 966-973. DOI: 10.7638/kqdlxxb-2017.0111
    [6]Wu Chenghui, Huang Mingfeng, Jiang Xiong, Chen Yongjun, Qiu Jian. Wind-induced vibration analysis of lattice-truss tower installed with a boiler based on semi-rigid model test[J]. ACTA AERODYNAMICA SINICA, 2015, 33(3): 353-359. DOI: 10.7638/kqdlxxb-2013.0041
    [7]SHI Wen-hai, LI Zheng-nong, WU jian-jia. A contrastive study of different time interval moving average statistical characteristics of strong wind near ground[J]. ACTA AERODYNAMICA SINICA, 2013, 31(5): 611-615. DOI: 10.7638/kqdlxxb-2011.0309
    [8]吴寿荣. 平面定常跨声速等熵流动的分析[J]. ACTA AERODYNAMICA SINICA, 2012, 30(6): 699-703.
    [9]Modeling and analysis of the aeroelastic response of the horizontal axis wind turbine blade[J]. ACTA AERODYNAMICA SINICA, 2012, 30(2): 192-197.
    [10]WANG Xiu-qiong, LIN Zhi-jie. Hybrid Regressive Model and its Application in the Time-Domain Analysis of Response of High-Rise Structures to Wind Action[J]. ACTA AERODYNAMICA SINICA, 2000, 18(4): 478-483.
  • Cited by

    Periodical cited type(6)

    1. 江嘉伟,程起有,刘正江,陈卫星. 基于多项式响应面MDOE的低速风洞试验方法研究. 航空科学技术. 2024(06): 114-120 .
    2. 刘思余,梁言,马明明. 基于离散优化的飞行试验点优化设计方法. 空气动力学学报. 2023(01): 86-92 . 本站查看
    3. 尤文佳,王慧杰,韩仁坤,陈刚. 高超声速风洞现代试验设计方法研究. 实验流体力学. 2022(03): 20-32 .
    4. 韩逸非,冯娜娜. 引射式跨声速风洞流场控制软件设计. 计算机测量与控制. 2021(01): 66-70 .
    5. 王岩,宋放. 基于PMAC的超声速风洞控制系统软件开发设计. 计算机测量与控制. 2021(02): 122-125+131 .
    6. 周照耀,王林国,卢煌军,王郡文. 小型风洞放气特性的数值计算及试验研究. 机床与液压. 2020(11): 66-69 .

    Other cited types(2)

Catalog

    Article views (215) PDF downloads (314) Cited by(8)

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return