Volume 40 Issue 3
Mar.  2025
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LIU Yongquan, LUO Gang, ZHANG Haiyang, et al. Research progress on bird impact of aero-engine fan blades[J]. Journal of Aerospace Power, 2025, 40（3）：20220653 doi: 10.13224/j.cnki.jasp.20220653
Citation: LIU Yongquan, LUO Gang, ZHANG Haiyang, et al. Research progress on bird impact of aero-engine fan blades[J]. Journal of Aerospace Power, 2025, 40（3）：20220653 doi: 10.13224/j.cnki.jasp.20220653
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Research progress on bird impact of aero-engine fan blades

doi: 10.13224/j.cnki.jasp.20220653
  • 1.

    Shenyang Engine Research Institute，Aero Engine Corporation of China，Shenyang 110015，China

  • 2.

    Key Laboratory of Impact Dynamics on Aero Engine，Liaoning Province，Shenyang Aeroengine Research Institute，Aero Engine Corporation of China，Shenyang 110015，China

  • 3.

    College of Energy and Power Engineering，Nanjing University of Aeronautics and Astronautics，Nanjing 210016，China

  • 4.

    State Key Laboratory of Mechanics and Control for Aerospace Structures，Nanjing University of Aeronautics and Astronautics，Nanjing 210016，China

  • 5.

    School of Civil Aviation，Northwestern Polytechnical University，Xi’an 710072，China

  • Received Date: 2022-09-04
    Available Online: 2024-11-10
    Abstract

  • The progresses made since the late 20th century in addressing bird strike issues on aircraft engine fan blades, covering aspects such as the geometric modeling of birds, transient dynamic numerical analysis methods, fan blade response and damage from bird strikes, as well as key bird strike testing techniques, were reviewed. The results indicated that foreign research on bird strikes on aircraft engine fan blades entered a deep application phase, while domestic research still faced challenges such as unclear research frameworks, undefined systems, and insufficient support. It’s also suggested that future research should focus on high-precision bird modeling, bird strikes on new material blades, bird strike testing techniques for blades in rotating states, and methods for analyzing the dynamic response of the entire engine post-strike.

     

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  • [1]
    陈光. 飞机发动机的防鸟撞设计与试验[J]. 国际航空,2009(11): 63-65. CHEN Guang. Prevention of bird strike hazards to aeroengines[J]. International Aviation,2009(11): 63-65. (in Chinese

    CHEN Guang. Prevention of bird strike hazards to aeroengines[J]. International Aviation, 2009(11): 63-65. (in Chinese)
    [2]
    关玉璞,陈伟,高德平. 航空发动机叶片外物损伤研究现状[J]. 航空学报,2007,28(4): 851-857. GUAN Yupu,CHEN Wei,GAO Deping. Present status of investigation of foreign object damage to blade in aeroengine[J]. Acta Aeronautica et Astronautica Sinica,2007,28(4): 851-857. (in Chinese doi: 10.3321/j.issn:1000-6893.2007.04.014

    GUAN Yupu, CHEN Wei, GAO Deping. Present status of investigation of foreign object damage to blade in aeroengine[J]. Acta Aeronautica et Astronautica Sinica, 2007, 28(4): 851-857. (in Chinese) doi: 10.3321/j.issn:1000-6893.2007.04.014
    [3]
    US National Transportation Safety Board. Boeing 767-300 bird ingestion accident[R]. Chicago: US National Transportation Safety Board,2007.
    [4]
    US National Transportation Safety Board. Loss of thrust in both engines after encountering a fock of birds and subsequent ditching on the hudson river[R]. Weehawken: US National Transportation Safety Board,2010.
    [5]
    BARBER J P,TAYLOR H R,WILBECK J S. Characterization of bird impacts on a rigid plate: Part Ⅰ[R]. Ohio: US University of Dayton Research Institute,1975.
    [6]
    WILBECK J S. Impact behavior of low strength projectiles[R]. Texas : US Air Force Materials Lab,1978.
    [7]
    BARBER J P,TAYLOR H R,WILBECK J S. Bird impact forces and pressures on rigid and compliant target[R]. Ohio: US University of Dayton Research Institute,1978.
    [8]
    EDGE C,DEGRIECK J. Derivation of a dummy bird for analysis and test of airframe structures[R]. Vancouver: CAN Bird Strike Committee,1999.
    [9]
    BUDGEY R. The development of a substitute artificial bird by the international bird strike research group for use in aircraft component testing[R]. Amsterdam: US International Bird Strike Commit tee25,2000.
    [10]
    MEGUID S A,MAO R H,NG T Y. FE analysis of geometry effects of an artificial bird striking an aeroengine fan blade[J]. International Journal of Impact Engineering,2008,35(6): 487-498. doi: 10.1016/j.ijimpeng.2007.04.008
    [11]
    MAO R H,MEGUID S A,NG T Y. Transient three dimensional finite element analysis of a bird striking a fan blade[J]. International Journal of Mechanics and Materials in Design,2008,4(1): 79-96. doi: 10.1007/s10999-008-9067-1
    [12]
    LAVOIE M A,GAKWAYA A,ENSAN M N,et al. Validation of available approaches for numerical bird strike modeling tools[J]. International Review of Mechanical Engineering,2007,1(4): 380-389.
    [13]
    LAVOIE M A,GAKWAYA A,ENSAN M N,et al. Bird’s substitute tests results and evaluation of available numerical methods[J]. International Journal of Impact Engineering,2009,36(10/11): 1276-1287.
    [14]
    SHUPIKOV A N,UGRIMOV S V,SMETANKINA N V,et al. Bird dummy for investigating the bird-strike resistance of aircraft components[J]. Journal of Aircraft,2013,50(3): 817-826. doi: 10.2514/1.C032008
    [15]
    张俊红,刘志远,戴胡伟,等. 撞击位置与风扇转速对鸟撞过程的影响[J]. 天津大学学报,2020,53(5): 492-501. ZHANG Junhong,LIU Zhiyuan,DAI Huwei,et al. Effect of impact position and fan rotational speed on bird-impact process[J]. Journal of Tianjin University (Science and Technology),2020,53(5): 492-501. (in Chinese

    ZHANG Junhong, LIU Zhiyuan, DAI Huwei, et al. Effect of impact position and fan rotational speed on bird-impact process[J]. Journal of Tianjin University (Science and Technology), 2020, 53(5): 492-501. (in Chinese)
    [16]
    郭鹏,刘志远,张桂昌,等. 鸟撞过程中撞击位置与撞击姿态对风扇叶片损伤影响研究[J]. 振动与冲击,2021,40(12): 124-131. GUO Peng,LIU Zhiyuan,ZHANG Guichang,et al. Study on effect of bird impact position and attitude on fan blade damage[J]. Journal of Vibration and Shock,2021,40(12): 124-131. (in Chinese

    GUO Peng, LIU Zhiyuan, ZHANG Guichang, et al. Study on effect of bird impact position and attitude on fan blade damage[J]. Journal of Vibration and Shock, 2021, 40(12): 124-131. (in Chinese)
    [17]
    WU Bin,LIN Jiewei,HEDAYATI R,et al. Dynamic responses of the aero-engine rotor system to bird strike on fan blades at different rotational speeds[J]. Applied Sciences,2021,11(19): 8883. doi: 10.3390/app11198883
    [18]
    WU Bin,HEDAYATI R,LI Zhehua,et al. Effect of impact and bearing parameters on bird strike with aero-engine fan blades[J]. Applied Sciences,2021,12(1): 7. doi: 10.3390/app12010007
    [19]
    ZHANG Dahai,FEI Qingguo. Effect of bird geometry and impact orientation in bird striking on a rotary jet-engine fan analysis using SPH method[J]. Aerospace Science and Technology,2016,54: 320-329. doi: 10.1016/j.ast.2016.05.003
    [20]
    ZHANG Zhuo,LI Liang,ZHANG Dingguo. Effect of arbitrary yaw/pitch angle in bird strike numerical simulation using SPH method[J]. Aerospace Science and Technology,2018,81: 284-293. doi: 10.1016/j.ast.2018.08.010
    [21]
    LI Junjie,LOU Yunfeng,YU Gaoyuan,et al. Effect of bird yaw/pitch angles on soft impact damage of a fan assembly[J]. Complexity,2021,2021(1): 1-13.
    [22]
    AIROLDI A,CACCHIONE B. Modelling of impact forces and pressures in Lagrangian bird strike analyses[J]. International Journal of Impact Engineering,2006,32(10): 1651-1677. doi: 10.1016/j.ijimpeng.2005.04.011
    [23]
    ZHANG Yong,LI Yu,ZHANG Hong. A method to identify bird constitutive model and its parameters[J]. Applied Mechanics and Materials,2013,302: 686-693. doi: 10.4028/www.scientific.net/AMM.302.686
    [24]
    MCCALLUM S,SHOJI H,AKIYAMA H. Development of an advanced multi-material bird-strike model using the smoothed particle hydrodynamics method[J]. International Journal of Crashworthiness,2013,18(6): 579-597. doi: 10.1080/13588265.2013.843498
    [25]
    LIU Jun,LI Yulong,GAO Xiaosheng. Bird strike on a flat plate: experiments and numerical simulations[J]. International Journal of Impact Engineering,2014,70: 21-37. doi: 10.1016/j.ijimpeng.2014.03.006
    [26]
    GUAN Yupu,ZHAO Zhenhua,CHEN Wei,et al. Foreign object damage to fan rotor blades of aeroengine:Part Ⅱ numerical simulation of bird impact[J]. Chinese Journal of Aeronautics,2008,21(4): 328-334. doi: 10.1016/S1000-9361(08)60043-6
    [27]
    LAKSHMAN N,RAJ R,MUKKAMALA Y. Bird strike analysis of jet engine fan blade[C]//2014 IEEE Aerospace Conference. Piscataway,US: IEEE,2014: 1-7.
    [28]
    赵海欧. LS-DYNA动力分析指南[M]. 中国: 兵器工业出版社,2003. ZHAO Haiou,LS-DYNA Dynamic Analysis Guidelines[M],Ordnance Industry Press,2003. (in Chinese

    ZHAO Haiou, LS-DYNA Dynamic Analysis Guidelines[M], Ordnance Industry Press, 2003. (in Chinese)
    [29]
    GUAN Yupu,ZHAO Zhenhua,CHEN Wei,et al. Foreign object damage to fan rotor blades of aeroengine: Part Ⅰ experimental study of bird impact[J]. Chinese Journal of Aeronautics,2007,20(5): 408-414. doi: 10.1016/S1000-9361(07)60062-4
    [30]
    MAO R H,MEGUID S A,NG T Y. Finite element modeling of a bird striking an engine fan blade[J]. Journal of Aircraft,2007,44(2): 583-596. doi: 10.2514/1.24568
    [31]
    MAO R H,MEGUID S A,NG T Y. Effects of incidence angle in bird strike on integrity of aero-engine fan blade[J]. International Journal of Crashworthiness,2009,14(4): 295-308. doi: 10.1080/13588260802671415
    [32]
    SINHA S K,TURNER K E,JAIN N. Dynamic loading on turbofan blades due to bird-strike[J]. Journal of Engineering for Gas Turbines and Power,2011,133(12): 1.
    [33]
    SINHA S K. Transient vibratory response of turbofan engine rotor impacted by bird strike[J]. Journal of Aerospace Engineering,2021,34(4): 04021027. doi: 10.1061/(ASCE)AS.1943-5525.0001250
    [34]
    HOWARD S A,HAMMER J T,CARNEY K S,et al. Jet engine bird ingestion simulations: comparison of rotating to non-rotating fan blades[M]. Ohio: American Society of Mechanical Engineers,2013.
    [35]
    PRAKASH R,CHANNEGOWDA H,KALIYAPERUMAL A. A study on bird impact damages on shrouded fan blades of an aero-engine [R]. Bangalore,Karnataka,India : Gas Turbine India Conference,2013.
    [36]
    ZENG Chuan,JIANG Xianghua,CHAI Xianghai,et al. TC4 hollow fan blade structural optimization based on bird-strike analysis[J]. Procedia Engineering,2015,99: 1385-1394. doi: 10.1016/j.proeng.2014.12.674
    [37]
    蒋向华,王延荣,桂幸民. 鸟撞作用下的叶片丢失及包容数值模拟[J]. 航空动力学报,2008,23(12): 2208-2213. JIANG Xianghua,WANG Yanrong,GUI Xingmin. Numerical simulation on blade loss caused by bird-impact and casing containment[J]. Journal of Aerospace Power,2008,23(12): 2208-2213. (in Chinese

    JIANG Xianghua, WANG Yanrong, GUI Xingmin. Numerical simulation on blade loss caused by bird-impact and casing containment[J]. Journal of Aerospace Power, 2008, 23(12): 2208-2213. (in Chinese)
    [38]
    刘建明,蒋向华. 材料参数对叶片鸟撞动响应影响数值模拟[J]. 航空发动机,2010,36(5): 36-38,31. LIU Jianming,JIANG Xianghua. Numerical simulation of blade material effect on dynamic response of bird impact on flat blade[J]. Aeroengine,2010,36(5): 36-38,31. (in Chinese doi: 10.3969/j.issn.1672-3147.2010.05.009

    LIU Jianming, JIANG Xianghua. Numerical simulation of blade material effect on dynamic response of bird impact on flat blade[J]. Aeroengine, 2010, 36(5): 36-38, 31. (in Chinese) doi: 10.3969/j.issn.1672-3147.2010.05.009
    [39]
    刘建明,蒋向华,秦银雷,等. 采用流固耦合的实体元空心叶片鸟撞数值模拟[J]. 航空动力学报,2010,25(10): 2211-2216. LIU Jianming,JIANG Xianghua,QIN Yinlei,et al. Numerical simulation of bird impact on solid-element hollow blades by using fluid-solid coupling method[J]. Journal of Aerospace Power,2010,25(10): 2211-2216. (in Chinese

    LIU Jianming, JIANG Xianghua, QIN Yinlei, et al. Numerical simulation of bird impact on solid-element hollow blades by using fluid-solid coupling method[J]. Journal of Aerospace Power, 2010, 25(10): 2211-2216. (in Chinese)
    [40]
    刘建明,蒋向华,武卉,等. 基于流固耦合的实体元空心叶片鸟撞数值模拟[J]. 航空发动机,2011,37(2): 8-11,4. LIU Jianming,JIANG Xianghua,WU Hui,et al. Numerical simulation of bird impact on solid-element hollow blades based on fluid-solid coupling[J]. Aeroengine,2011,37(2): 8-11,4. (in Chinese doi: 10.3969/j.issn.1672-3147.2011.02.003

    LIU Jianming, JIANG Xianghua, WU Hui, et al. Numerical simulation of bird impact on solid-element hollow blades based on fluid-solid coupling[J]. Aeroengine, 2011, 37(2): 8-11, 4. (in Chinese) doi: 10.3969/j.issn.1672-3147.2011.02.003
    [41]
    柴象海,侯亮,王志强,等. 航空发动机宽弦风扇叶片鸟撞损伤模型标定[J]. 航空动力学报,2016,31(5): 1032-1038. CHAI Xianghai,HOU Liang,WANG Zhiqiang,et al. Bird strike model calibration for an aero engine wide-chord fan blade[J]. Journal of Aerospace Power,2016,31(5): 1032-1038. (in Chinese

    CHAI Xianghai, HOU Liang, WANG Zhiqiang, et al. Bird strike model calibration for an aero engine wide-chord fan blade[J]. Journal of Aerospace Power, 2016, 31(5): 1032-1038. (in Chinese)
    [42]
    LETELLIER A,BUNG H,BERTHILLIER M,et al. Bird impact on fan blade analysis using SPH method coupled with finite element[R]. Orlando,US: Symposium on Structures under Extreme Loading Conditions,1997.
    [43]
    AUDIC S,BERTHILLIER M,BONINI J,et al. Prediction of bird impact in hollow fan blades: AIAA 2000-3201 [R]. Reston,Virigina: AIAA,2000.
    [44]
    SIDDENS A,BAYANDOR J. A discrete meshless lagrangian based approach for soft impact damage modeling in advanced propulsion systems[R]. Vancouver: ASME International Mechanical Engineering Congress and Exposition,2010.
    [45]
    SIDDENS A,BAYANDOR J. Multidisciplinary impact damage prognosis methodology for hybrid structural propulsion systems[J]. Computers & Structures,2013,122: 178-191.
    [46]
    SIDDENS A,BAYANDOR J,CELESTINA M L. Detailed post-soft impact progressive damage assessment for hybrid structure jet engines[R]. Ohio: National Aeronautics and Space Administration,2014.
    [47]
    LIU Jun,LI Yulong. Numerical simulation of a rotary engine primary compressor impacted by bird[J]. Chinese Journal of Aeronautics,2013,26(4): 926-934. doi: 10.1016/j.cja.2013.06.006
    [48]
    LIU Jun,ZHONG Dudu,LI Yulong,et al. Numerical simulation and test on damage of rotary engine blades impacted by bird[J]. International Journal of Crashworthiness,2019,24(1): 106-120. doi: 10.1080/13588265.2018.1452548
    [49]
    VIGNJEVIC R,ORŁOWSKI M,DE VUYST T,et al. A parametric study of bird strike on engine blades[J]. International Journal of Impact Engineering,2013,60: 44-57. doi: 10.1016/j.ijimpeng.2013.04.003
    [50]
    PUNEETH M L,JAYAPRAKASH D. Influence of bird mass and impact height on the fan-blade of an aero-engine[J]. Materials Today: Proceedings,2021,44: 1028-1038. doi: 10.1016/j.matpr.2020.11.175
    [51]
    杨瑞进,姜楠,池剑虹,等. 基于SPH方法鸟撞航空发动机进气风扇的数值分析[J]. 航空科学技术,2012,23(6): 35-37. YANG Ruijin,JIANG Nan,CHI Jianhong,et al. Numerical analysis based on the SPH for bird strike aeroengine intake fan[J]. Aeronautical Science & Technology,2012,23(6): 35-37. (in Chinese doi: 10.3969/j.issn.1007-5453.2012.06.012

    YANG Ruijin, JIANG Nan, CHI Jianhong, et al. Numerical analysis based on the SPH for bird strike aeroengine intake fan[J]. Aeronautical Science & Technology, 2012, 23(6): 35-37. (in Chinese) doi: 10.3969/j.issn.1007-5453.2012.06.012
    [52]
    张闻东. 涡扇发动机风扇叶片鸟击机械损伤仿真研究[D]. 天津: 中国民航大学,2015. ZHANG Wendong. Simulation study on mechanical damage of fan blade of turbofan engine caused by bird strike[D]. Tianjin: Civil Aviation University of China,2015. (in Chinese

    ZHANG Wendong. Simulation study on mechanical damage of fan blade of turbofan engine caused by bird strike[D]. Tianjin: Civil Aviation University of China, 2015. (in Chinese)
    [53]
    张卓. 基于光滑粒子法与有限元法耦合的鸟撞发动机叶片响应分析[D]. 南京: 南京理工大学,2018. ZHANG Zhuo. Response analysis of bird impact engine blade based on coupling of smoothed particle hydrodynamics method and finite element method[D]. Nanjing: Nanjing University of Science and Technology,2018. (in Chinese

    ZHANG Zhuo. Response analysis of bird impact engine blade based on coupling of smoothed particle hydrodynamics method and finite element method[D]. Nanjing: Nanjing University of Science and Technology, 2018. (in Chinese)
    [54]
    王浪,孙有朝,周亚东,等. 复合材料层合板鸟弹撞击损伤分析[J]. 航空发动机,2022,48(2): 19-24. WANG Lang,SUN Youchao,ZHOU Yadong,et al. Analysis of bird impact damage of composite laminate[J]. Aeroengine,2022,48(2): 19-24. (in Chinese

    WANG Lang, SUN Youchao, ZHOU Yadong, et al. Analysis of bird impact damage of composite laminate[J]. Aeroengine, 2022, 48(2): 19-24. (in Chinese)
    [55]
    曹源,侯亮,胡寿丰. 航空发动机鸟撞分析的人工鸟本构参数研究[R]. 北京: 中国航空学会,2015. CAO Yuan,HOU Liang,HU Shoufeng. Constitutive models of gelatin bird for bird strike in aero engine[R]. Beijing: Aviation Society of China,2015. in Chinese

    CAO Yuan, HOU Liang, HU Shoufeng. Constitutive models of gelatin bird for bird strike in aero engine[R]. Beijing: Aviation Society of China, 2015. in Chinese)
    [56]
    GOYAL V K,HUERTAS C A,VASKO T J. Bird-strike modeling based on the lagrangian formulation using LS-DYNA[J]. American Transactions on Engineering & Applied Sciences,2013,2(2): 57-81.
    [57]
    GOYAL V K,HUERTAS C A,VASKO T J. Arbitrary lagrange eulerian approach for bird-strike analysis using LS-DYNA[J]. American Transactions on Engineering & Applied Sciences,2013,2(2): 109-32.
    [58]
    GOYAL V K,HUERTAS C A,VASKO T J. Smooth particle hydrodynamics for bird-strike analysis using LS-DYNA[J]. American Transactions on Engineering & Applied Sciences,2013,2(2): 83-107.
    [59]
    CERQUAGLIA M L,DELIÉGE G,BOMAN R,et al. Reprint of: the particle finite element method for the numerical simulation of bird strike[J]. International Journal of Impact Engineering,2017,110: 72-84. doi: 10.1016/j.ijimpeng.2017.09.002
    [60]
    CERQUAGLIA M L,DELIÉGE G,BOMAN R,et al. Preliminary assessment of the possibilities of the particle finite element method in the numerical simulation of bird impact on aeronautical structures[J]. Procedia Engineering,2017,173: 101-108. doi: 10.1016/j.proeng.2016.12.043
    [61]
    WANG Z L, KONIETZKY H, HUANG R Y. Elastic-plastic-hydrodynamic analysis of crater blasting in steel fiber reinforced concrete[J]. Theoretical & Applied Fracture Mechanics, 2009, 52(2):111-116.
    [62]
    JENQ S T,HSIAO F B,LIN I C,et al. Simulation of a rigid plate hit by a cylindrical hemi-spherical tip-ended soft impactor[J]. Computational Materials Science,2007,39(3): 518-526. doi: 10.1016/j.commatsci.2006.08.008
    [63]
    ROISMAN I V. Hydrodynamic model of a collision of a spherical plastic ice particle with a perfectly rigid substrate[J]. International Journal of Impact Engineering, 2021(4):104019.
    [64]
    NAGARAJ V,VELMURUGAN T. Numerical bird strike impact simulation of aircraft composite structure[J]. Journal of Mechanical and Civil Engineering,2007,1(1): 1-10.
    [65]
    张永康,李玉龙. 鸟体力学模型仿真研究[J]. 计算机仿真,2011,28(9): 67-70. ZHANG Yongkang,LI Yulong. Simulation research on bird body mechanics model[J]. Computer Simulation,2011,28(9): 67-70. (in Chinese

    ZHANG Yongkang, LI Yulong. Simulation research on bird body mechanics model[J]. Computer Simulation, 2011, 28(9): 67-70. (in Chinese)
    [66]
    MCCARTHY M A,XIAO J R,MCCARTHY C T,et al. Modelling of bird strike on an aircraft wing leading edge made from fibre metal laminates: Part 2 modelling of impact with SPH bird model[J]. Applied Composite Materials,2004,11(5): 317-340. doi: 10.1023/B:ACMA.0000037134.93410.c0
    [67]
    ASLAM M A,BIN RAYHAN S,KE Zhange,et al. Ballistic gelatin Lagrange Mooney-Rivlin material model as a substitute of bird in finite element bird strike case studies[J]. Latin American Journal of Solids and Structures,2020,17(6): 1-15.
    [68]
    PERNAS-SÁNCHEZ J,ARTERO-GUERRERO J,VARAS D,et al. Artificial bird strike on Hopkinson tube device: experimental and numerical analysis[J]. International Journal of Impact Engineering,2020,138: 103477.
    [69]
    刘军,李玉龙,石霄鹏,等. 鸟体本构模型参数反演Ⅱ: 模型参数反演研究[J]. 航空学报,2011,32(5): 812-821. LIU Jun,LI Yulong,SHI Xiaopeng,et al. Parameter inversion of bird body constitutive model Ⅱ research on model parameter inversion[J]. Acta Aeronautica et Astronautica Sinica,2011,32(5): 812-821. (in Chinese

    LIU Jun, LI Yulong, SHI Xiaopeng, et al. Parameter inversion of bird body constitutive model Ⅱ research on model parameter inversion[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(5): 812-821. (in Chinese)
    [70]
    单斌. 基于刚性靶冲击试验的人工鸟材料参数识别研究[D]. 南京: 南京航空航天大学,2014. SHAN Bin. Research on material parameter identification of artificial bird based on rigid target impact test[D]. Nanjing: Nanjing University of Aeronautics and Astronautics,2014. (in Chinese

    SHAN Bin. Research on material parameter identification of artificial bird based on rigid target impact test[D]. Nanjing: Nanjing University of Aeronautics and Astronautics, 2014. (in Chinese)
    [71]
    李振友,朱书华,周华闯,等. 基于遗传算法的鸟体本构参数优化研究[J]. 航空计算技术,2017,47(1): 47-50. LI Zhenyou,ZHU Shuhua,ZHOU Huachuang,et al. Optimization of bird body constitutive parameters based on genetic algorithm[J]. Aviation Computing Technology,2017,47(1): 47-50. (in Chinese

    LI Zhenyou, ZHU Shuhua, ZHOU Huachuang, et al. Optimization of bird body constitutive parameters based on genetic algorithm[J]. Aviation Computing Technology, 2017, 47(1): 47-50. (in Chinese)
    [72]
    NANDLALL D,GAKWAYA A. On the determination of the shock and steady state parameters of gelatine from cylinder impact experiments[J]. International Journal of Impact Engineering,2018,116: 22-33. doi: 10.1016/j.ijimpeng.2018.02.001
    [73]
    TAHERI-BEHROOZ F,MOGHADDAM H S. Nonlinear numerical analysis of the V-notched rail shear test specimen[J]. Polymer Testing,2018,65: 44-53. doi: 10.1016/j.polymertesting.2017.11.008
    [74]
    TAHERI-BEHROOZ F,SHAMAEI KASHANI A R,HEFZABAD R N. Effects of material nonlinearity on load distribution in multi-bolt composite joints[J]. Composite Structures,2015,125: 195-201. doi: 10.1016/j.compstruct.2015.01.047
    [75]
    NISHIKAWA M,HEMMI K,TAKEDA N. Finite-element simulation for modeling composite plates subjected to soft-body,high-velocity impact for application to bird-strike problem of composite fan blades[J]. Composite Structures,2011,93(5): 1416-1423. doi: 10.1016/j.compstruct.2010.11.012
    [76]
    HOU J P,PETRINIC N,RUIZ C,et al. Prediction of impact damage in composite plates[J]. Composites Science and Technology,2000,60(2): 273-281. doi: 10.1016/S0266-3538(99)00126-8
    [77]
    LIU Haibao,LIU Jun,KABOGLU C,et al. The behaviour of fibre-reinforced composites subjected to a soft impact-loading: an experimental and numerical study[J]. Engineering Failure Analysis,2020,111: 104448. doi: 10.1016/j.engfailanal.2020.104448
    [78]
    HASHIN Z,ROTEM A. A fatigue failure criterion for fiber reinforced materials[J]. Journal of Composite Materials,1973,7(4): 448-464. doi: 10.1177/002199837300700404
    [79]
    HASHIN Z. Failure criteria for unidirectional fiber composites[J]. Journal of Applied Mechanics,1980,47(2): 329-334. doi: 10.1115/1.3153664
    [80]
    金峰,刘璐璐,朱信颖,等. 钛合金包边复合材料风扇叶片的鸟撞数值仿真[J]. 航空发动机,2024,50(4): 107-113. JIN Feng,LIU Lulu,ZHU Xinying,et al. Numerical simulation on bird impact of composite fan blade with titanium leading edge[J]. Aeroengine,2024,50(4): 107-113. (in Chinese

    JIN Feng, LIU Lulu, ZHU Xinying, et al. Numerical simulation on bird impact of composite fan blade with titanium leading edge[J]. Aeroengine, 2024, 50(4): 107-113. (in Chinese)
    [81]
    HEIMBS S,BERGMANN T. High-velocity impact behaviour of prestressed composite plates under bird strike loading[J]. International Journal of Aerospace Engineering,2012,2012: 372167.
    [82]
    ZHOU Yadong,SUN Youchao,HUANG Tianlin,et al. SPH-FEM simulation of impacted composite laminates with different layups[J]. Aerospace Science and Technology,2019,95: 105469. doi: 10.1016/j.ast.2019.105469
    [83]
    ZHOU Yadong,SUN Youchao,CAI Wenchao. Bird-striking damage of rotating laminates using SPH-CDM method[J]. Aerospace Science and Technology,2019,84: 265-272. doi: 10.1016/j.ast.2018.10.009
    [84]
    HASAN M Z. Interface failure of heated GLARETM fiber–metal laminates under bird strike[J]. Aerospace,2020,7(3): 28. doi: 10.3390/aerospace7030028
    [85]
    LIU Lulu,YANG Zongzhi,JI Jian,et al. Development and experimental verification of a modified constitutive model for 3D orthogonal woven composite under bird impact[J]. Composite Structures,2023,303: 116305. doi: 10.1016/j.compstruct.2022.116305
    [86]
    黄志勇,陈伟,赵海欧,等. 评定叶片鸟撞击损伤的参数与方法[J]. 航空发动机,2005,31(1): 28-30. HUANG Zhiyong,CHEN Wei,ZHAO Haiou,et al. Parameters and methods for evaluating bird impact damage of fan/compressor blade[J]. Aeroengine,2005,31(1): 28-30. (in Chinese doi: 10.3969/j.issn.1672-3147.2005.01.007

    HUANG Zhiyong, CHEN Wei, ZHAO Haiou, et al. Parameters and methods for evaluating bird impact damage of fan/compressor blade[J]. Aeroengine, 2005, 31(1): 28-30. (in Chinese) doi: 10.3969/j.issn.1672-3147.2005.01.007
    [87]
    罗刚,陈伟,赵振华,等. 航空发动机吸鸟适航验证关键参数分析方法[J]. 机械科学与技术,2016,35(11): 1774-1779. LUO Gang,CHEN Wei,ZHAO Zhenhua,et al. Analysis method of critical parameters on aircraft engines bird ingestion airworthiness certification[J]. Mechanical Science and Technology for Aerospace Engineering,2016,35(11): 1774-1779. (in Chinese

    LUO Gang, CHEN Wei, ZHAO Zhenhua, et al. Analysis method of critical parameters on aircraft engines bird ingestion airworthiness certification[J]. Mechanical Science and Technology for Aerospace Engineering, 2016, 35(11): 1774-1779. (in Chinese)
    [88]
    HOU Naidan,LI Yulong,LIU Jun. Numerical simulation of bird impact on hollow blades of titanium fan assembly[J]. Journal of Aerospace Engineering,2019,32(4): 1-15.
    [89]
    YAN Jun,ZHANG Chenguang,HUO Sixu,et al. Experimental and numerical simulation of bird-strike performance of lattice-material-infilled curved plate[J]. Chinese Journal of Aeronautics,2021,34(8): 245-257. doi: 10.1016/j.cja.2020.09.026
    [90]
    李迪,廖连芳,陈璐璐,等. 宽弦空心风扇叶片大鸟撞击试验研究[J]. 航空发动机,2020,46(3): 66-70. LI Di,LIAO Lianfang,CHEN Lulu,et al. Study on big bird strike test of wide-chord hollow fan blade[J]. Aeroengine,2020,46(3): 66-70. (in Chinese

    LI Di, LIAO Lianfang, CHEN Lulu, et al. Study on big bird strike test of wide-chord hollow fan blade[J]. Aeroengine, 2020, 46(3): 66-70. (in Chinese)
    [91]
    NISHIKAWA M,HEMMI K,PARK S,et al. Finite element analysis on the impact-induced damage of composite fan blades subjected to a bird strike[J]. Transactions of Japan Society fir Aeronautical and Space Sciences,2011,54(185/186): 238-245.
    [92]
    LIU Lulu,LUO Gang,CHEN Wei,et al. Dynamic behavior and damage mechanism of 3D braided composite fan blade under bird impact[J]. International Journal of Aerospace Engineering,2018,2018: 5906078.
    [93]
    LIU Lulu,SHAO Hongyan,ZHU Xinying,et al. Development and experimental verification damage mechanism of 3D orthogonal woven composite aeroengine blades[J]. Composite Structures,2023,304: 116311. doi: 10.1016/j.compstruct.2022.116311
    [94]
    宋长远,唐旭,陈大玮,等. 复合材料风扇叶片鸟撞损伤的精细化分析方法[J]. 航空发动机,2022,48(2): 25-32. SONG Changyuan,TANG Xu,CHEN Dawei,et al. Refined analysis method for bird impact damage of composite fan blade[J]. Aeroengine,2022,48(2): 25-32. (in Chinese

    SONG Changyuan, TANG Xu, CHEN Dawei, et al. Refined analysis method for bird impact damage of composite fan blade[J]. Aeroengine, 2022, 48(2): 25-32. (in Chinese)
    [95]
    KUZMIN M V,KIRSANOV A R. Validation of aircraft gas-turbine engine inlet bird throw-in simulation model[J]. Naučnyj Vestnik MGTU GA,2015,2015(212): 120-126.
    [96]
    KUZMIN M V,KIRSANOV A R. Predictive estimation of gas-turbine engine damageability in the event of birds ingression into gas-turbine engine inlet[J]. Naučnyj Vestnik MGTU GA,2015(212): 127-132.
    [97]
    张海洋,王相平,杜少辉,等. 航空发动机风扇叶片的抗鸟撞设计[J]. 航空动力学报,2020,35(6): 1157-1168. ZHANG Haiyang,WANG Xiangping,DU Shaohui,et al. Design for anti-bird impact of aero-engine fan blade[J]. Journal of Aerospace Power,2020,35(6): 1157-1168. (in Chinese

    ZHANG Haiyang, WANG Xiangping, DU Shaohui, et al. Design for anti-bird impact of aero-engine fan blade[J]. Journal of Aerospace Power, 2020, 35(6): 1157-1168. (in Chinese)
    [98]
    黄福增,刘永泉,张东明,等. 发动机风扇转子旋转状态下鸟撞试验研究[J]. 实验力学,2020,35(6): 1136-1146. HUANG Fuzeng,LIU Yongquan,ZHANG Dongming,et al. Investigation on bird-strike test of gas turbine rotating fan blade[J]. Journal of Experimental Mechanics,2020,35(6): 1136-1146. (in Chinese doi: 10.7520/1001-4888-19-085

    HUANG Fuzeng, LIU Yongquan, ZHANG Dongming, et al. Investigation on bird-strike test of gas turbine rotating fan blade[J]. Journal of Experimental Mechanics, 2020, 35(6): 1136-1146. (in Chinese) doi: 10.7520/1001-4888-19-085
    [99]
    杨杰,陈伟,罗刚. 基于LS-DYNA的鸟撞风扇数值仿真研究[R]. 安徽: 第九届中国CAE工程分析技术年会,2013. YANG Jie,CHEN Wei,LUO Gang. Numerical simulation research on bird impact fan based on LS-DYNA[R]. Anhui: 9th China CAE Engineering Analysis Technology Annual Conference,2013. (in Chinese

    YANG Jie, CHEN Wei, LUO Gang. Numerical simulation research on bird impact fan based on LS-DYNA[R]. Anhui: 9th China CAE Engineering Analysis Technology Annual Conference, 2013. (in Chinese)
    [100]
    马力,姜甲玉,薛庆增. 航空发动机第1级风扇叶片鸟撞研究[J]. 航空发动机,2014,40(2): 65-69. MA Li,JIANG Jiayu,XUE Qingzeng. Research on bird impact of aeroengine first stage fan[J]. Aeroengine,2014,40(2): 65-69. (in Chinese

    MA Li, JIANG Jiayu, XUE Qingzeng. Research on bird impact of aeroengine first stage fan[J]. Aeroengine, 2014, 40(2): 65-69. (in Chinese)
    [101]
    CHANNEGOWDA H,PRAKASH R V,KALIYAPERUMAL A. A study on the effect of bird hit damage on the dynamic response of aero-engine fan blade[R]. San Diego: American Society of Mechanical Engineers,2013.
    [102]
    BADSHAH S,NAEEM A,FARHAN RAFIQUE A,et al. Numerical study on the critical frequency response of jet engine rotors for blade-off conditions against bird strike[J]. Applied Sciences,2019,9(24): 5568. doi: 10.3390/app9245568
    [103]
    LUO Gang,MA Chi,CHEN Wei,et al. Transient analysis and safety assessment of turbofan engine structures during bird ingestion[J]. International Journal of Aerospace Engineering,2020,2020: 7404587.
    [104]
    WOJTYCZKA C,AMIN S,TUNGA V,et al. Fan blade optimization under medium bird strike load[R]. California: US Virtual Product Development Conference MSC,2004.
    [105]
    CHEN Wei,LUO Gang,ZHANG Sheng,et al. Development strategy of engine bird ingestion certification technology[J]. Transactions of Nanjing University of Aeronautics & Astronautics,2015,32(5): 485-94.
    [106]
    SHORR B F,MATSARENKO V S,SEREBRYAKOV N N. Experimental design of a device for bird strike bench tests of non-rotating fan blades[J]. VESTNIK of the Samara State Aerospace University,2015,14(3): 88.
    [107]
    ALLAEYS F,LUYCKX G,VAN PAEPEGEM W,et al. Development and validation of a set-up to measure the transferred multi-axial impact momentum of a bird strike on a booster vane[J]. International Journal of Impact Engineering,2017,99: 102-110. doi: 10.1016/j.ijimpeng.2016.09.011
    [108]
    ALLAEYS F,LUYCKX G,VAN PAEPEGEM W,et al. Characterization of real and substitute birds through experimental and numerical analysis of momentum,average impact force and residual energy in bird strike on three rigid targets: a flat plate,a wedge and a splitter[J]. International Journal of Impact Engineering,2017,99: 1-13. doi: 10.1016/j.ijimpeng.2016.08.009
    [109]
    康飞,盛腾,许明文,等,涡轴发动机吞鸟试验方法研究[J]. 科技视界,2020(26): 115-117. KANG Fei,SHENG Teng,XU Mingwen,et al. Research on bird swallowing test method for turboshaft engine[J] Technology Perspective,2020 (26): 115-117. (in Chinese

    KANG Fei, SHENG Teng, XU Mingwen, et al. Research on bird swallowing test method for turboshaft engine[J] Technology Perspective, 2020 (26): 115-117. (in Chinese)
    [110]
    张永飞,贾宗芸,陈玮,等,某型涡轴发动机吞鸟试验及验证[J]. 航空发动机,2017. 43(5): 62-68. ZHANG Yongfei,JIA Zongyun,CHEN Wei,et al. Bird swallowing test and verification of a certain type of turboshaft engine[J] Aviation Engine,2017 43 (5): 62-68. (in Chinese

    ZHANG Yongfei, JIA Zongyun, CHEN Wei, et al. Bird swallowing test and verification of a certain type of turboshaft engine[J] Aviation Engine, 2017 43 (5): 62-68. (in Chinese)
    [111]
    彭迎风,辛勇. 冲击式滑阀开炮机构的研究和设计[J]. 机械制造,2006,44(4): 26-28. PENG Yingfeng,XIN Yong. Research and design of trigger device of air cannon with impact slide valve gear[J]. Machinery,2006,44(4): 26-28. (in Chinese doi: 10.3969/j.issn.1000-4998.2006.04.009

    PENG Yingfeng, XIN Yong. Research and design of trigger device of air cannon with impact slide valve gear[J]. Machinery, 2006, 44(4): 26-28. (in Chinese) doi: 10.3969/j.issn.1000-4998.2006.04.009
    [112]
    KOKA T R,MATHEW A T. Design of sabot &catcher system of single stage gas gun for bird and hailstone impact test[J]. Materials Today: Proceedings,2018,5(5): 11827-11837. doi: 10.1016/j.matpr.2018.02.153
    [113]
    刘闯,魏峰,陈国栋,等. 鸟撞试验弹托脱壳过程模拟与试验验证[J]. 航空发动机,2022,48(2): 14-18. LIU Chuang,WEI Feng,CHEN Guodong,et al. Simulation and test verification of sabot separation during bird impact test[J]. Aeroengine,2022,48(2): 14-18. (in Chinese

    LIU Chuang, WEI Feng, CHEN Guodong, et al. Simulation and test verification of sabot separation during bird impact test[J]. Aeroengine, 2022, 48(2): 14-18. (in Chinese)
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