Volume 40 Issue 3
Mar.  2025
Turn off MathJax
Article Contents
WANG Chao, DONG Xiucheng, GU Shifu, et al. Velocity decoupling of fluorescent oil film based on resection[J]. Journal of Aerospace Power, 2025, 40(3):20230332 doi: 10.13224/j.cnki.jasp.20230332
Citation: WANG Chao, DONG Xiucheng, GU Shifu, et al. Velocity decoupling of fluorescent oil film based on resection[J]. Journal of Aerospace Power, 2025, 40(3):20230332 doi: 10.13224/j.cnki.jasp.20230332

Velocity decoupling of fluorescent oil film based on resection

doi: 10.13224/j.cnki.jasp.20230332
  • Received Date: 2023-05-19
    Available Online: 2024-05-11
  • The model vibration in wind tunnel test may easily lead to the coupling of oil flow velocity, while the traditional optical flow method cannot identify or eliminate the vibration. Therefore, an optical flow decoupling algorithm based on resection was proposed. The low resolution optical flow value solved by the interpolated image correlation method was taken as the iterative initial value of the optical flow. Then, based on the resection, a calculation model for vibration angle and displacement under vibration conditions was derived, and then the vibration displacement was eliminated to achieve speed decoupling. The simulation test showed that the AEEs (average endpoint errors) of the traditional optical flow method and the optical flow decoupling algorithm were 0.20, 0.98, 1.44, 1.63 pixel/s and 0.19, 0.20, 0.22, 0.27 pixel/s, respectively, at the simulated vibration angles of 0°, 5°, 10° and 15°, and the measurement error of vibration angle was less than 0.1°; the fluorescence oil flow test further indicated that the velocity field streamline obtained by the optical flow decoupling algorithm based on rear intersection was more accurate, smooth and clearer, which can effectively solve the velocity coupling problem. This method has certain practical engineering application value.

     

  • loading
  • [1]
    赵忠良,吴军强,李浩,等. 高机动导弹气动/运动/控制耦合的风洞虚拟飞行试验技术[J]. 空气动力学学报,2016,34(1): 14-19. ZHAO Zhongliang,WU Junqiang,LI Hao,et al. Wind tunnel based virtual flight testing of aerodyanmics,flight dynamics and flight control for high maneuver missle[J]. Acta Aerodynamica Sinica,2016,34(1): 14-19. (in Chinese doi: 10.7638/kqdlxxb-2015.0128

    ZHAO Zhongliang, WU Junqiang, LI Hao, et al. Wind tunnel based virtual flight testing of aerodyanmics, flight dynamics and flight control for high maneuver missle[J]. Acta Aerodynamica Sinica, 2016, 34(1): 14-19. (in Chinese) doi: 10.7638/kqdlxxb-2015.0128
    [2]
    张晓辉. 高超声速飞行器机翼颤振减损控制研究[D]. 南京: 南京航空航天大学,2019. ZHANG Xiaohui. Damage-mitigating control for the flutter of hypersonic flight vehicle airfoil[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2019. (in Chinese

    ZHANG Xiaohui. Damage-mitigating control for the flutter of hypersonic flight vehicle airfoil[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2019. (in Chinese)
    [3]
    IGNATYEV D I,ZARIPOV K G,SIDORYUK M E,et al. Wind tunnel tests for validation of control algorithms at high angles of attack using autonomous aircraft model mounted in 3DOF gimbals[R]. AIAA 2016-3106,2016 .
    [4]
    NIEL F,SEURET A,ZACCARIAN L,et al. Robust LQR control for stall flutter suppression: a polytopic approach[J]. IFAC,2017,50(1): 11367-11372.
    [5]
    CHAMBERS J R,HALL R M. Historical review of uncommanded lateral-directional motions at transonic conditions[J]. Journal of Aircraft,2004,41(3): 436-447. doi: 10.2514/1.4470
    [6]
    王帅,何国强,秦飞,等. 超声速内流道摩擦阻力分析及减阻技术研究[J]. 航空动力学报,2019,34(4): 908-919. WANG Shuai,HE Guoqiang,QIN Fei,et al. Research on skin-friction drag and drag reduction technics in a supersonic inner flow path[J]. Journal of Aerospace Power,2019,34(4): 908-919. (in Chinese

    WANG Shuai, HE Guoqiang, QIN Fei, et al. Research on skin-friction drag and drag reduction technics in a supersonic inner flow path[J]. Journal of Aerospace Power, 2019, 34(4): 908-919. (in Chinese)
    [7]
    林其勋,郭捷,李亚平,等 . 用热线风速仪研究轴流压气机 的非定常流场及端壁附面层[J]. 航空动力学报,1989,4(2): 141-144. LIN Qixun,GUO Jie,LI Yaping,et al. Investigation on un-steady flow field and endwall boundary layer in axial flow compressor with hot wire anemometer[J]. Journal of Aerospace Power,1989,4(2): 141-144. (in Chinese

    LIN Qixun, GUO Jie, LI Yaping, et al. Investigation on un-steady flow field and endwall boundary layer in axial flow compressor with hot wire anemometer[J]. Journal of Aerospace Power, 1989, 4(2): 141-144. (in Chinese)
    [8]
    唐亮,杨振华,谢艳,等. Optotrak光学跟踪测量仪在风洞迎角测量的应用[J]. 兵工自动化,2015,34(3): 68-70. TANG Liang,YANG Zhenhua,XIE Yan,et al. Application of optotrak optical tracking measurement instrument in wind tunnel angle measurement[J]. Ordnance Industry Automation,2015,34(3): 68-70. (in Chinese

    TANG Liang, YANG Zhenhua, XIE Yan, et al. Application of optotrak optical tracking measurement instrument in wind tunnel angle measurement[J]. Ordnance Industry Automation, 2015, 34(3): 68-70. (in Chinese)
    [9]
    JIA Zhenyuan,MA Xin,LIU Wei,et al. Pose measurement method and experiments for high-speed rolling targets in a wind tunnel[J]. Sensors,2014,14(12): 23933-23953. doi: 10.3390/s141223933
    [10]
    LIU Tianshu,BURNER A W,JONES T W,et al. Photogrammetric techniques for aerospace applications[J]. Progress in Aerospace Sciences,2012,54: 1-58. doi: 10.1016/j.paerosci.2012.03.002
    [11]
    刘春明,赵志军,卜忱,等. 低速风洞双自由度大幅振荡试验技术[J]. 航空学报,2016,37(8): 2417-2425. LIU Chunming,ZHAO Zhijun,BU Chen,et al. Double degree-of-freedom large amplitude oscillation test technology in low speed wind tunnel[J]. Acta Aeronautica et Astronautica Sinica,2016,37(8): 2417-2425. (in Chinese

    LIU Chunming, ZHAO Zhijun, BU Chen, et al. Double degree-of-freedom large amplitude oscillation test technology in low speed wind tunnel[J]. Acta Aeronautica et Astronautica Sinica, 2016, 37(8): 2417-2425. (in Chinese)
    [12]
    QIAN Hongjiang,DONG Xiucheng,ZHANG Zhengyu. Research on stability of gray value of excited-state fluorescent oil film based on variable light vector angle[J]. Mathematical Problems in Engineering,2021,2021: 8632992.
    [13]
    孙岩,姚海艳,张征宇. 单相机迎角测量中振动影响研究[J]. 航空学报,2013,34(3): 525-532. SUN Yan,YAO Haiyan,ZHANG Zhengyu. Vibration influence research on single camera measurement of angle of attack[J]. Acta Aeronautica et Astronautica Sinica,2013,34(3): 525-532. (in Chinese

    SUN Yan, YAO Haiyan, ZHANG Zhengyu. Vibration influence research on single camera measurement of angle of attack[J]. Acta Aeronautica et Astronautica Sinica, 2013, 34(3): 525-532. (in Chinese)
    [14]
    陈磊,钟凯,朱涛,等. 高超声速风洞试验段环境飞行器颤振的视觉三维测量[J]. 光学精密工程,2021,29(8): 1811-1821. CHEN Lei,ZHONG Kai,ZHU Tao,et al. Visual three-dimensional measurement of aircraft flutter in hypersonic wind tunnel tests[J]. Optics and Precision Engineering,2021,29(8): 1811-1821. (in Chinese doi: 10.37188/OPE.2021.0169

    CHEN Lei, ZHONG Kai, ZHU Tao, et al. Visual three-dimensional measurement of aircraft flutter in hypersonic wind tunnel tests[J]. Optics and Precision Engineering, 2021, 29(8): 1811-1821. (in Chinese) doi: 10.37188/OPE.2021.0169
    [15]
    陈丁,吕计男,季辰,等. 双目视觉技术在高超声速颤振风洞试验中的应用[J]. 实验力学,2015,30(3): 381-387. CHEN Ding,LYU Jinan,JI Chen,et al. Application of binocular vision measurement in hypersonic flutter wind tunnel experiment[J]. Journal of Experimental Mechanics,2015,30(3): 381-387. (in Chinese doi: 10.7520/1001-4888-14-192

    CHEN Ding, LYU Jinan, JI Chen, et al. Application of binocular vision measurement in hypersonic flutter wind tunnel experiment[J]. Journal of Experimental Mechanics, 2015, 30(3): 381-387. (in Chinese) doi: 10.7520/1001-4888-14-192
    [16]
    朱林梅,董秀成,张征宇,等. 面向奇异构型目标点分布的相机位姿估计算法[J]. 光子学报,2021,50(7): 0715001. ZHU Linmei,DONG Xiucheng,ZHANG Zhengyu,et al. Camera pose estimation algorithm for singular configuration of target points[J]. Acta Photonica Sinica,2021,50(7): 0715001. (in Chinese

    ZHU Linmei, DONG Xiucheng, ZHANG Zhengyu, et al. Camera pose estimation algorithm for singular configuration of target points[J]. Acta Photonica Sinica, 2021, 50(7): 0715001. (in Chinese)
    [17]
    SCARANO F. Theory of non-isotropic spatial resolution in PIV[J]. Experiments in Fluids,2003,35(3): 268-277. doi: 10.1007/s00348-003-0655-4
    [18]
    THEUNISSEN R,SCARANO F,RIETHMULLER M L. An adaptive sampling and windowing interrogation method in PIV[J]. Measurement Science and Technology,2007,18(1): 275-287. doi: 10.1088/0957-0233/18/1/034
    [19]
    BECKER F,WIENEKE B,PETRA S,et al. Variational adaptive correlation method for flow estimation[J]. IEEE Transactions on Image Processing,2012,21(6): 3053-3065. doi: 10.1109/TIP.2011.2181524
    [20]
    邵绪强,杨艳,刘艺林. 流体运动估计光流算法研究综述[J]. 中国图象图形学报,2021,26(2): 355-367. SHAO Xuqiang,YANG Yan,LIU Yilin. Review of optical flow algorithms in fluid motion estimation[J]. Journal of Image and Graphics,2021,26(2): 355-367. (in Chinese doi: 10.11834/jig.200050

    SHAO Xuqiang, YANG Yan, LIU Yilin. Review of optical flow algorithms in fluid motion estimation[J]. Journal of Image and Graphics, 2021, 26(2): 355-367. (in Chinese) doi: 10.11834/jig.200050
    [21]
    王超,董秀成,古世甫,等. 基于深度学习光流法的荧光油膜全局速度测量[J]. 航空动力学报,2022,37(7): 1539-1549. WANG Chao,DONG Xiucheng,GU Shifu,et al. Global velocity measurement of fluorescent oil film based on deep learning optical flow method[J]. Journal of Aerospace Power,2022,37(7): 1539-1549. (in Chinese

    WANG Chao, DONG Xiucheng, GU Shifu, et al. Global velocity measurement of fluorescent oil film based on deep learning optical flow method[J]. Journal of Aerospace Power, 2022, 37(7): 1539-1549. (in Chinese)
    [22]
    LIU Tianshu,MERAT A,MAKHMALBAF M H M,et al. Comparison between optical flow and cross-correlation methods for extraction of velocity fields from particle images[J]. Experiments in Fluids,2015,56(8): 166. doi: 10.1007/s00348-015-2036-1
    [23]
    HORN B K P,SCHUNCK B G. Determining optical flow[J]. Artificial Intelligence,1981,17(1/2/3): 185-203.
    [24]
    HEITZ D,MÉMIN E,SCHNÖRR C. Variational fluid flow measurements from image sequences: synopsis and perspectives[J]. Experiments in Fluids,2010,48(3): 369-393. doi: 10.1007/s00348-009-0778-3
    [25]
    王佩军,徐亚明. 摄影测量学: 测绘工程专业[M]. 3版. 武汉: 武汉大学出版社,2016. WANG Peijun,XU Yaming. Geo-spatial information science[M]. 3rd ed. Wuhan: Wuhan University Press,2016. (in Chinese

    WANG Peijun, XU Yaming. Geo-spatial information science[M]. 3rd ed. Wuhan: Wuhan University Press, 2016. (in Chinese)
    [26]
    唐正宗,梁晋,郭成. 基于摄影测量校正的斜光轴数字图像相关方法[J]. 光学学报,2011,31(11): 1112007. TANG Zhengzong,LIANG Jin,GUO Cheng. Slant-axis digital image correlation method based on photogrammetric correction[J]. Acta Optica Sinica,2011,31(11): 1112007. (in Chinese doi: 10.3788/AOS201131.1112007

    TANG Zhengzong, LIANG Jin, GUO Cheng. Slant-axis digital image correlation method based on photogrammetric correction[J]. Acta Optica Sinica, 2011, 31(11): 1112007. (in Chinese) doi: 10.3788/AOS201131.1112007
    [27]
    蔡章博,张征宇,余皓,等. 荧光油膜速度场自适应快速光流解法[J]. 航空学报,2023,44(17): 128047. CAI Zhangbo,ZHANG Zhengyu,YU Hao,et al. Adaptive fast optical flow solution for velocity field of fluorescent oil film[J]. Acta Aeronautica et Astronautica Sinica,2023,44(17): 128047. (in Chinese

    CAI Zhangbo, ZHANG Zhengyu, YU Hao, et al. Adaptive fast optical flow solution for velocity field of fluorescent oil film[J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(17): 128047. (in Chinese)
    [28]
    李鹏. 全局表面摩擦应力直接测量技术研究[D]. 南京: 南京航空航天大学,2012. LI Peng. Studies of direct measurement techniques about global skin friction[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2012. (in Chinese

    LI Peng. Studies of direct measurement techniques about global skin friction[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2012. (in Chinese)
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views (849) PDF downloads(32) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return