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基本信息 The basic information
姓名: 万方义

学院: 航空学院


学历: 博士研究生毕业

学位: 工学博士


职称: 副教授

职务: 副院长


学科: 航空宇航科学与技术









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工作经历 Work Experience
2003.12-2006.12，西北工业大学，博士后
2005.12-2006.6，美国弗吉尼亚州立理工学院（Virginia Tech），访问****
2013.3-2014.3，比利时列日大学（ULg），访问****
2007.1-至今，? 西北工业大学，副教授?





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教育经历 Education Experience
1992.9-1996.7，西安理工大学，水利电力动力工程，本科生
1996.9-1999.4，西安理工大学，印刷工程（印刷机械），硕士生
1999.3-2003.12，西安交通大学，力学，博士生





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教育教学 Education And Teaching
1.生命保障技术，本科生课程，48学时
2.飞行器健康管理原理与技术，本科生课程，24学时
3.飞行器救生技术，硕士生课程，40学时
4.飞行器故障诊断与健康管理理论与应用，硕士生课程，40学时
5.飞行器结构系统健康管理技术，硕士生课程，40学时





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招生信息 Admission Information
研究方向1)飞行器综合测试与健康管理
2)飞行器结构/机构健康管理及演示实验
3) 无人机综合测试与控制
4) 飞行器安全性分析与设计
硕士研究生招生学科
1.飞行器设计
2.飞行器控制与信息工程
3. 航空航天安全工程
4. 航空工程







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荣誉获奖 Awards Information
2019年度西北工业大学“三育人”先进个人

2018年度西北工业大学校级优秀教学成果奖二等奖
2018年“创青春”全国大学生创业大赛国家级铜奖指导老师

2017年第四届粤港澳台大学生创新创业大赛亚军指导老师

2017（洛阳）直通硅谷创新创业大赛优秀创业导师
2016年度第二届江西省“互联网+”大学生创新创业大赛（金奖）优秀指导老师
2016年度航空学院本科生最满意教师、学院保密工作先进个人、学院先进个人
航空学院2015年度，2016年度教学工作先进个人、科研工作先进个人
2013年度，2014年度，2015年度陕西省“三秦人才奖”
2010年省部级科技二等进步奖1项（排名第三）









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科学研究 Scientific Research
2005CG010001
科研项目（国家自然科学基金青年项目）
8.0
2005-01-01到2005-12-31

2007DN010001
科研项目（国家863项目）
20.0
2007-08-01到2008-06-30

2008DN010001
科研项目（国家863项目）
20.0
2008-08-01到2009-07-30

2009DH010001
科研项目（国家863项目）
30.0
2009-08-01到2010-07-30

2010DH010001
科研项目（国家863项目）
20.0
2010-08-01到2011-06-30

2011DH010001
科研项目（国家863项目）
30.0
2011-08-01到2012-06-30

2012DH010001
科研项目（国家863项目）
60.0
2012-08-01到2013-06-30

2013DH010005
科研项目（国家863项目）
50.0
2013-08-01到2014-06-30

2014KC010161
健康管理系统试验研究（国家863项目）
60.0
2014-06-01到2015-09-30

2014MC010048
数据包络分析研究
10.2
2013-01-03到2014-05-30

2015KC010181
健康管理试验（国家863项目）
50.0
2015-08-01到2016-06-30

2016MC010064
连接匹配设计及试验研究
65.35
2016-06-20到2017-07-30

2016MC010119
机电系统通用自动化测试方法研究
20.0
2016-05-23到2017-11-01

2016ME010057
应急撤离人员轨迹测试与分析系统开发
35.0
2016-06-15到2017-12-31

2016ME010060
可用性评估指标研究项目
45.0
2016-06-15到2017-04-30

2017KE010217
长航时工业无人机及测绘系统产业化
10.0
2017-01-01到2018-12-31

2017MC010035
翼身连接开口密封带研发试验
48.0
2017-01-01到2017-12-30

2017MC010064
人机工效评估验证系统
30.0
2017-03-01到2017-12-01

2017MC010197
某人机功效仿真评价优化系统
84.9
2017-06-01到2019-06-01

2017MC100079
PHM软件验证设备
394.0
2017-09-10到2018-09-09

2018MC010229
陆战舱室人-机-环系统效能提升虚拟优化技术
19.8
2018-09-05到2018-12-30

2018ME010284
直升机驾驶舱人机工效试验与评估
35.0
2018-11-10到2018-12-30








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学术成果 Academic Achievements

期刊论文/ Journals Articles
[1] Wan, F.; Tran, M.-P.; Leblanc, C.; Béchet, E.; Plougonven, E.; Léonard, A.; Detrembleur, C.; Noels, L.; Thomassin, J.-M.; Nguyen, V.-D. Experimental and computational micro-mechanical investigations of compressive properties of polypropylene/multi-walled carbon nanotubes nanocomposite foams[J]. Mechanics of Materials, 2015, 91: 95-118. (WOS:008, EI: 20**5, DOI: 10.1016/j.mechmat.2015.07.004)
[2] 万方义，宋笔锋，许庆余，喻天翔.非线性裂纹转子系统碰摩故障时参变特性的研究 [J]. 机械强度，2006, 28(5):633-638. (EI：870).
[3] 万方义，宋笔锋，许庆余，万婧，郝俊霞. 裂纹转子系统虚拟状态监测[J]. 机械科学与技术，2005，24(12):1469-1471.
[4] Fangyi Wan, Qingyu Xu, Songtao Li, Vibration Analysis of Cracked Rotor–Sliding-Bearing System with Rotor-Stator Rubbing by Harmonic Wavelet Transform [J]. Journal of Sound and Vibration, 2004,271(3-5), 507~518. (WOS:002，EI：20，它引27次) DOI: 10.1016/S0022-460X(03)00277-3
[5] 万方义，许庆余，宋笔锋，张小龙. 滑动轴承_转子系统非线性裂纹故障特征及其实验研究[J]. 应用力学学报，2004，21(3): 38～42. (EI：20)
[6] 万方义，许庆余，李松涛.谐波小波变换在转子—轴承系统多故障监测中的应用[J]. 工程力学，2004，21(1):102~106. (EI：)
[7] 万方义，许庆余，张小龙，许清源. 油膜支承转子系统动静件碰摩特征分析[J]. 应用力学学报，2003,20(2):17～21. (EI：)
[8] 万方义，华军，许庆余. 二维小波变换及其在机械碰摩故障诊断中的应用[J]. 机械强度,2002,24(2):168～171. (EI：)
[9] 万方义，许庆余，华军.非线性油膜支承裂纹转子动力特性分析[J].航空学报，2002,23(3):237～240.
[10] 万方义,许庆余. 柔性递纸机构的动态设计方法研究[J].机械科学与技术.2001，20(3)：239～241. (EI：)
[11] Chunlin Zhang, Yuling Liu, Fangyi Wan et al. Multi-faults diagnosis of rolling bearings via adaptive customization of flexible analytical wavelet bases [J]. Chinese Journal of Aeronautics. (DOI: https://doi.org/10.1016/j.cja.2019.03.014)
[12] Chunlin Zhang ; Yuling Liu ; Fangyi Wan ; Binqiang Chen ; Jie Liu. Isolation and identification of compound faults in rotating machinery via windowed correlated kurtosis enhanced by modified empirical wavelet transform [J]. IEEE Access. (DOI: 10.1109/ ACCESS.2019.**)
[13] Guo,Qing; Wan, Fangyi. Complete synchronization of the global coupled dynamical network induced by Poisson noises[J]. PLoS ONE, 2017, 12(12): e**. (WOS:0004**, DOI : 10.1371/journal.pone.**)
[14] Guo,Qing; Guo, Peirong; Wan, Fangyi. Strong convergence in the pth-mean of an averaging principle for two-time-scales SPDEs with jumps[J]. Advances In Difference Equations, 2017. (WOS:002, DOI: 10.1186/s13662-017-1333-9)
[15] 于琦,万方义,郭英男,赵阳. 故障注入技术在飞行器非电系统中的应用进展[J]. 航空工程进展, 2013, 4(3):261-267.
[16] 秦增,万方义. 基于杆件柔性的舱门机构动力学特性影响分析[J]. 机械与电子,2013,(11): 15-19.
[17] 李鹏飞,万方义,崔卫民，宋笔锋. FBG传感器在飞行器结构健康监控中的可行性研究[J]. 机械强度, 2011, 33(4): 624-628.
[18] 郝俊霞,万方义,宋笔锋.基于小概率事件的飞行器结构健康监控[J].机械设计与制造, 2007, (12):87-88
[19] 张茂，万方义，宋笔锋. 基于小波包的碰摩信号能量特征辨识[J]. 机械设计与制造，2006, (9):143-145.
[20] 万婧,万方义,宋笔锋,冯蕴雯. 虚拟仪器技术在飞机燃油系统健康监控中的应用[J]. 机械设计与制造，2005，(11):153-154.
[21] Jun Hua, Fangyi Wan, Qingyu Xu. Numerical and Experimental Studies on Nonlinear Dynamic Behaviors of a Rotor-Fluid Film Bearing System with Squeeze Film Dampers [J]. Trans. ASME J. of Vibration and Acoustics. 2001,123(3),297～302 (WOS:000**2).
[22] 尚柏林, 宋笔锋, 万方义. 光纤传感器在飞行器结构健康监测中的应用[J]. 光纤与电缆及其应用技术, 2008,(03):7-10
[23] 尚柏林, 宋笔锋, 万方义. 飞行器结构健康监控系统研究进展及关键技术[J]. 测控技术,2008, 27(7): 1-3
[24] 喻天翔，宋笔锋，万方义，冯蕴雯. 机械可靠性试验技术研究现状和展望[J].机械强度，2007, 29(2):256-263. （EI：182）
[25] 喻天翔，宋笔锋，万方义，冯蕴雯. 零件多失效模式可靠度计算理论研究[J]. 机械强度，2006, 28(4):508-511. （EI：844）
[26] 李松涛，许庆余，万方义等，宫密封不平衡子转子动力系统的稳定性与分岔[J]. 应用数学与力学，2003,24(11),1141～1150.
[27] LI Song-tao，XU Qing-yu，WAN Fang-yi et al. Stability and Bifurcation of Unbalance Rotor/Labyrinth Seal System[J]. Applied Mathematics and Mechanics, 2003,24(11),1290～1301. (SCI三区：766RZ) (EI：)
[28] 李松涛，许庆余，万方义，迷宫密封转子系统非线性动力稳定性的研究[J]. 应用力学学报，2002,19(2), 27～30. (EI：)
[29] 张劲夫，许庆余，万方义等，考虑摩擦的机械手逆动力学问题的研究[J].工程力学，2002, 19(4), 104～108.
[30] 侯乔乔,崔卫民,喻天翔,万方义. 考虑弹性变形的开环机构运动精度分析[J]. 机械强度, 2013, 35(1): 111-115.




会议论文/ ConferenceProceedings
[1] Jiangni Lei,Fangyi Wan, Weimin Cui, Wenheng Li. Testability Modeling of Hydraulic System Based on Multi-signal Flow Model[C]. 2017 International Conference on Sensing, Diagnostics, Prognostics, and Control (SDPC). p361-366, 16-18 Aug. 2017, Shanghai, China. (DOI: 10.1109/SDPC.2017.75)
[2] Wenhao Zong; Fangyi Wan; Yishui Wei. Real-time monitoring for the actuator mechanism of the aileron[C]. 2017 Prognostics and System Health Management Conference (PHM- Harbin), p1-5, 9-12 July 2017, Harbin, China. (DOI: 10.1109/PHM.2017.**, EI: 20**5)
[3] Wan Fangyi,Yu, Xingliang,Yu, Qi. Research on Optimal Sensor Placement for Aircraft Structural Health Management [C]. 2017 IEEE International Conference on Prognostics and Health Management, ICPHM 2017, p160-166, June 19 - 21, 2017, Dallas, TX, United states. (DOI: 10.1109/ICPHM.2017.**, EI: 20**2 )
[4] YU xingliang, WAN Fangyi, GUO yingnan. Micromechanics Modeling of Skin Panel with Pitting Corrosion for Aircraft Structural Health Monitoring [C]. 2016 IEEE International Conference on Prognostics and Health Management, p1-8, June 20-22, 2016, Ottawa, ON, Canada. (DOI: 10.1109/ICPHM.2016.**, EI: 20**3)
[5] YANG Hui, WAN Fangyi, CUI Weimin. Failure simulation and identification of shock absorber in carrier-based aircraft landing gear [C]. 2016 IEEE International Conference on Prognostics and Health Management, p1-6, June 20 -22, 2016, Ottawa, ON, Canada. (DOI: 10.1109/ICPHM.2016.**, EI: 20**5)
[6] Yu Qi, Wan Fangyi, Guo Yingnan, Cui Weimin. A model-based fault injection system for aerocraft wing structure[C], 2014 International Conference on Prognostics and Health Management,p1-6, June 22-25, 2014, Cheney, WA, USA (DOI: 10.1109/ ICPHM. 2014. **, EI: 20**1)
[7] Wan Fangyi, Qin, Zeng. Virtual health monitoring system for wing structure[C]. Advanced Materials Research, 2013 International Conference on MEMS and Mechanics, MEMSM 2013, March 15-16, 2013, Wuhan, China. (DOI: 10.4028/www.scientific.net/AMR.705.534, EI: 20**7)
[8] Guo Yingnan, Wan Fangyi. Research on Modal Parameters Identification of Wing Structures with NExT-ERA[C]. 2012 3rd International Conference on Applied Mechanics and Mechanical Engineering, ICAMME 2012, November 14- 15, 2012, Macau, China. Applied Mechanics and Materials, 249-259(201): 1025-1029. (DOI: 10.4028/ www.scientific.net/ AMM.249-250.1025,EI: 20**1)
[9] Sun Mingming, Wan Fangyi, Qin Zeng. Health monitoring for propagating crack faults[C]. Proceedings of IEEE 2012 Prognostics and System Health Management Conference, PHM-2012. P1-6, May 23-25, 2012, Beijing, China. (DOI:10.1109/PHM.2012.**, EI: 178).
[10] Wang Haifeng, Song Bifeng, WAN Fangyi. Research on fault pattern recognition for aircraft fuel system with its performance simulation[C]. 2011 2nd International Conference on Artificial Intelligence, Management Science and Electronic Commerce, AIMSEC 2011 - Proceedings, p 4231-4235, 2011, August 8-10, 2011, Zhengzhou, China (DOI:10.1109/ AIMSEC.2011.**, EI: 201**)
[11] Hou Qiaoqiao, Cui Weimin,Yu Tianxiang, Wan Fangyi, Song Bifeng. An analysis of mechanism kinematics accuracy based on linear elastic [C]. Proceedings of 2011 9th International Conference on Reliability, Maintainability and Safety, p 404-408, ICRMS'2011. June 12 - 15, 2011. Guiyang, China. (DOI: 10.1109/ICRMS.2011.**,EI: 201**)
[12] Wang Haifeng, Song Bifeng, WAN Fangyi. A simulation software of prognostics and health management for aircraft fuel system[C]. Proceedings of 2011 international conference on Quality, Reliability. Risk, Maintenance and Safety Engineer, DOI: 10.1109/ICQR2MSE.2011.**, June 17-19, 2011, Xi’an, China. （EI：201**）
[13] Yingnan GUO, Fangyi WAN, Ling WU, Hanjie JIANG. Research of Structural Health Monitoring Based on Mode Analysis for UAV Wings[C]. 2011 Prognostics and system heath Management Conference. DOI: 10.1109/PHM.2011.**, May 23-25, Shenzhen, China. （EI：201**）.
[14] Yun WU, FangYi WAN, MingMing SUN. Simulation on the faults mechanism of wing structure[C]. 2011 Prognostics and system heath Management Conference. P 1 - 7, May 23-25, Shenzhen, China. （DOI: 10.1109/PHM.2011.** ,EI：201**）.
[15] Xuhui CUI, Fangyi WAN, Mingming SUN. Virtual Damages Simulation of the Metallic Thermal Protection System Panel[C]. 2011 Prognostics and system heath Management Conference. DOI: 10.1109/PHM.2011.**; May 24-25, 2011,Shenzhen, China. （EI：201**）.
[16] Ting SHEN, Fangyi WAN, Bifeng SONG, Yun WU. Damage Location and Identification of the Wing Structure with Probabilistic Neural Networks[C]. 2011 Prognostics and system heath Management Conference. P1 - 6, May 23-25, Shenzhen, China. （DOI: 10.1109/PHM.2011.** ,EI：201**）.
[17] Weimin CUI, Fangyi WAN, TianxiangYU, Bifeng SONG. Optimization Design of Sensor Logic Structure for Safety Monitoring Systems[C]. 2011 Prognostics and system heath Management Conference. May 23-25, Shenzhen, China.
[18] Ting SHEN, Fangyi WAN, Weimin CUI, Bifeng SONG. Application of Prognostic and Health Management Technology on Aircraft Fuel System[C]. 2010 Prognostics and system heath Management Conference. DOI:10.1109/PHM.2010.**, Jan 12-14, Macau, China.（WOS:064, EI：345）.
[19] Fangyi WAN, Weiping YANG, Ting SHEN, Bifeng SONG. Application of Harmonic Wavelet Transform on Aerocraft Structure Health Monitoring[C]. Asia Pacific Symposium on Safety 2009 Conference Proceedings :206-209. Oct.20-23 Osaka, Japan
[20] Weimin CUI, Tianxiang YU, Fangyi WAN, Bifeng SONG. A New Method of Reliability Test and Assessment in High Reliability Design of Valves[C]. Asia Pacific Symposium on Safety 2009 Conference Proceedings :143-146. Oct.20-23 Osaka, Japan
[21] Yu Tianxiang, Song Bifeng, Feng Yunwen, Wan Fangyi, Research on the Accelerated Reliability Growth Model (ARGM) in Constant Stress[C]. Asia Pacific Symposium on Safety 2005 Conference Proceedings :1991-1996. Nov.2-4 Shaoxing, China(WOS:126)
[22] Yu Tianxiang, Song Bifeng, Wan Fangyi, Feng Yunwen. Simulation Validation of Reliability Growth Model for Multi-Systems Development Testing[C]. Asia Simulation Conf./ the 6th Int. Conf. on System Simulation and Scientific Computing, Conference Proceedings : 1299-1303. Oct. 24-27, 2005,Beijing, China（WOS:278, EI: 20**5）
[23] Wan Fang-yi, Song Bi-feng, Xu qing-yu, Yu Tian-xiang. Based on virtual instrument to monitor cracked rotor-bearing system by harmonic wavelet transform[C]. ISTM/2005: 6TH International Symposium On Test And Measurement, Vols 1-9, Conference Proceedings : 1166-1169, June 1-4, 2005, Dalian: （WOS:042）
[24] 万方义，许庆余. 裂纹转子－滑动轴承系统动静件碰摩故障的谐波小波分析[C]. 2002年全国振动工程技术及应用学术会议论文集，北京：111～116.
[25] F.Y.Wan, Q.Y.Xu, L.Zhang. Research on Dynamic Characteristics of Flexible Transfer Mechanism [C]. Proceedings of International Conference Advanced Problems in Vibration Theory and Application , June 2000, Xi’an：707～710.
专利及软件著作权/ Patents and software copyrights
[1] 结构PHM故障仿真软件[简称：故障注入软件]V1.0 登记号：2019SR**
[2] 结构PHM故障诊断软件[简称：故障诊断软件]V1.0 登记号：2019SR**
[3] 万方义 戴维 李文衡 崔卫民 郭英男 郭庆 李陶； 一种基于模块化组合涵道式旋翼无人机 (Modular combined duct type rotor wing unmanned aerial vehicle ), 申请号: CN0.5
[4] 郭腾 崔卫民 万方义 雷江妮 李文衡 符超 秦大顺 王景卓；一种航空舱门锁变加载试验装置（Aerial cabin door lock variable loading test device），申请号：2.6












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学术文献 Academic Literature
1.Application of Prognostic and Health Management Technology on Aircraft Fuel System,IEEE,2010,,415-421 ,DOI:10.1109/PHM.2010.**, ISSN:
2.A Simulation Software of Prognostics and Health Management for Aircraft Fuel System,IEEE,2011,,492-496 ,DOI:10.1109/ICQR2MSE.2011.**, ISSN:
3.基于小波包的碰摩信号能量特征辨识,2006,(9),143-145 ,DOI:10.3969/j.issn.1001-3997.2006.09.062, ISSN:1001-3997
4.基于小概率事件的飞行器结构健康监控,2007,(12),87-88 ,DOI:10.3969/j.issn.1001-3997.2007.12.037, ISSN:1001-3997
5.故障注入技术在飞行器非电系统中的应用进展,2013,4(3),261-267 ,DOI:10.3969/j.issn.1674-8190.2013.03.001, ISSN:1674-8190
6.FBG传感器在飞行器结构健康监控中的可行性研究,2011,33(4),624-628 ,DOI:, ISSN:1001-9669
7.考虑弹性变形的开环机构运动精度分析,2013,35(1),111-115 ,DOI:, ISSN:1001-9669
8.裂纹转子系统虚拟状态监测,2005,24(12),1469-1471,1501 ,DOI:10.3321/j.issn:1003-8728.2005.12.023, ISSN:1003-8728
9.Research on fault pattern recognition for aircraft fuel system with its performance simulation,IEEE Computer Society, 445 Hoes Lane - P.O.Box 1331, Piscataway, NJ 08855-1331, United States,2011,,4231-4235 ,DOI:10.1109/AIMSEC.2011.**, ISSN:66
10.Research on calculating the reliability of mechanical component with correlated failure modes,Journal of Mechanical Strength, Zhengzou, Henan, China,2006,28(4),508-511 ,DOI:, ISSN:**
11.Research on the characteristics of variable parameters in nonlinear cracked rotor system with rub-impact faults,Journal of Mechanical Strength, Zhengzou, Henan, China,2006,28(5),633-638 ,DOI:, ISSN:**
12.Health monitoring for propagating crack faults,IEEE Computer Society, 2001 L Street N.W., Suite 700, Washington, DC 20036-4928, United States,2012, ,DOI:10.1109/PHM.2012.**, ISSN:
13.Research on modal parameters identification of wing structures with NExT-ERA,Trans Tech Publications, P.O. Box 1254, Clausthal-Zellerfeld, D-38670, Germany,2013,249-250,1025-1029 ,DOI:10.4028/www.scientific.net/AMM.249-250.1025, ISSN:77
14.A model-based fault injection system for aerocraft wing structure,Institute of Electrical and Electronics Engineers Inc.,2015, ,DOI:10.1109/ICPHM.2014.**, ISSN:26
15.Virtual damages simulation of the metallic thermal protection system panel,IEEE Computer Society, 445 Hoes Lane - P.O.Box 1331, Piscataway, NJ 08855-1331, United States,2011, ,DOI:10.1109/PHM.2011.**, ISSN:11
16.Simulation on the faults mechanism of wing structure,IEEE Computer Society, 445 Hoes Lane - P.O.Box 1331, Piscataway, NJ 08855-1331, United States,2011, ,DOI:10.1109/PHM.2011.**, ISSN:11
17.Research of structural health monitoring based on mode analysis for UAV wings,IEEE Computer Society, 445 Hoes Lane - P.O.Box 1331, Piscataway, NJ 08855-1331, United States,2011, ,DOI:10.1109/PHM.2011.**, ISSN:11
18.Present state and prospects for mechanical reliability testing technique study,Journal of Mechanical Strength, Zhengzou, Henan, China,2007,29(2),256-263 ,DOI:, ISSN:**
19.Research on accelerated reliability growth model (ARGM) in constant stress,SCIENCE PRESS BEIJING,2005,5,1991-1996 ,DOI:, ISSN:
20.Simulation validation of reliability growth model for multi-systems development testing,INTERNATIONAL ACADEMIC PUBLISHERS LTD,2005,,1299-1303 ,DOI:, ISSN:
21.Based on virtual instrument to monitor cracked rotor-bearing system by harmonic wavelet transform,INTERNATIONAL ACADEMIC PUBLISHERS LTD,2005,,1166-1169 ,DOI:, ISSN:
22.Virtual health monitoring system for wing structure,Trans Tech Publications Ltd, Kreuzstrasse 10, Zurich-Durnten, CH-8635, Switzerland,2013,705,534-539 ,DOI:10.4028/www.scientific.net/AMR.705.534, ISSN:94
23.An analysis of mechanism kinematics accuracy based on linear elastic,IEEE Computer Society, 445 Hoes Lane - P.O.Box 1331, Piscataway, NJ 08855-1331, United States,2011,,404-408 ,DOI:10.1109/ICRMS.2011.**, ISSN:44
24.Damage location and identification of the wing structure with Probabilistic Neural Networks,IEEE Computer Society, 445 Hoes Lane - P.O.Box 1331, Piscataway, NJ 08855-1331, United States,2011, ,DOI:10.1109/PHM.2011.**, ISSN:11
25.滑动轴承-转子系统非线性裂纹故障特征及其实验研究,2004,21(3),38-42 ,DOI:10.3969/j.issn.1000-4939.2004.03.008, ISSN:1000-4939
26.基于杆件柔性的舱门机构动力学特性影响分析,2013,(11),15-19 ,DOI:10.3969/j.issn.1001-2257.2013.11.004, ISSN:1001-2257
27.飞行器结构健康监控系统研究进展及关键技术,2008,27(7),1-3,14 ,DOI:10.3969/j.issn.1000-8829.2008.07.001, ISSN:1000-8829
28.机械可靠性试验技术研究现状和展望,Journal of Mechanical Strength, Zhengzou, Henan, China,2007,29(2),256-263 ,DOI:10.3321/j.issn:1001-9669.2007.02.017, ISSN:1001-9669
29.机械零件多失效模式相关可靠度算法研究,Journal of Mechanical Strength, Zhengzou, Henan, China,2006,28(4),508-511 ,DOI:10.3321/j.issn:1001-9669.2006.04.008, ISSN:1001-9669
30.非线性裂纹转子系统碰摩故障参变特性研究,Journal of Mechanical Strength, Zhengzou, Henan, China,2006,28(5),633-638 ,DOI:10.3321/j.issn:1001-9669.2006.05.001, ISSN:1001-9669
31.虚拟仪器技术在飞机燃油系统健康监控中的应用,2005,(11),153-154 ,DOI:10.3969/j.issn.1001-3997.2005.11.072, ISSN:1001-3997
32.光纤传感器在飞行器结构健康监测中的应用,2008,(3),7-10 ,DOI:10.3969/j.issn.1006-1908.2008.03.003, ISSN:1006-1908
33.基于自然激励技术与本征系统实现算法的飞行器结构健康监测研究,2012,(中国陕西西安),1 ,DOI:, ISSN:





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