熊峻江，工学博士，长聘教授，博士生导师，教育部航空运输与工程教学指导分委员会委员。
1986获西北工业大学工程力学专业工学学士学位，1986至1989年中国直升机设计研究所工作，1992和1995年分别获北京航空航天大学固体力学专业工学硕士与博士学位，1996年至今，北京航空航天大学工作（此间，曾在英国南安普顿大学合作研究2年），先后任副教授（1997）、教授（2000）、博士生导师（2006）、长聘教授（2018）。长期从事飞机结构适航性教学与科研工作，发表SCI收录论文60余篇、EI收录论文47篇；获部级科技进步一等奖1项、二等奖2项、三等奖2项；出版专著/教材7部， 获全国优秀科技图书二等奖1部、国防优秀科技图书奖2部。
主讲课程
[1] 大学一年级通识课：《大飞机适航概论》
[2] 本科专业核心课：《飞机结构适航力学基础》
[3] 研究生专业必修课：《飞机系统与结构安全性》
出版著作
[1] 熊峻江. 飞机结构适航力学基础. 北京：北京航空航天大学出版社，2020
[2] 熊峻江，白江波. 平面编织复合材料飞行器结构力学. 北京：科学出版社，2020
[3] Xiong JJ, Shenoi RA. Faitgue and Fracture Reliability Engineering. London: Springer, 2011
[4] 熊峻江. 疲劳断裂可靠性工程学. 北京：国防出版社，2008
[5] 熊峻江. 飞行器结构疲劳与寿命设计. 北京：北京航空航天大学出版社，2004
[6] 高镇同，熊峻江. 疲劳可靠性. 北京：北京航空航天大学出版社，2000
[7] 高镇同，蒋新桐，熊峻江等. 疲劳性能试验设计与数据处理. 北京：北京航空航天大学出版社，1999
发表主要论文
[1] Wan AS, Xu YG, Xiong JJ*. Notch effect on strength and fatigue life of woven composite laminates. INT J FATIGUE, 2019; 127: 275-290
[2] Bai J B*, Chen D, Xiong JJ*, Shenoi R A. A corrugated flexible composite skin for morphing applications. COMPOS PART B-ENG, 2017; 131: 134-143
[3] Bai JB, Xiong JJ*, Shenoi RA, Zhu YT. Analytical solutions for predicting tensile and in-plane shear strengths of triaxial weave fabric composites. INT J SOLIDS STRUCT, 2017; 120: 199-212
[4] Lv ZY, Xiong JJ*, Tong L, Zhu YT. A practical approach for evaluating safe fatigue life of hydraulic actuator in helicopter based on a nominal force concept and minimal datasets. AEROSP SCI TECHNOL, 2017;62: 158-164
[5] Liu MD, Xiong JJ*, Liu JZ, Tian BJ. Modified model for evaluating fatigue behaviors and lifetimes of notched aluminum-alloys at temperatures of 25ºC and -70ºC. INT J FATIGUE, 2016；93: 122-132
[6] Wang CQ, Xiong JJ*, Shenoi RA, Liu MD, Liu JZ. A modified model to depict corrosion fatigue crack growth behaviour for evaluating residual lives of aluminium alloys. INT J FATIGUE, 2016; 83: 280-287
[7] Tian BJ, Xiong JJ*, Liu JZ. A new approach for evaluating fatigue lives of multi-fastener mechanical joints based on a nominal stress concept and minimal datasets. INT J FATIGUE, 2015; 80: 257-265
[8] Xiong JJ*, Bai JB, Chen L. Simplified analytical model for predicting the temperature of balloon on high-altitude. INT J THERM SCI, 2014; 76: 82-89
[9] Bai JB, Xiong JJ*, Gao JP, Yi XS. Analytical solutions for predicting in-plane strain and interlaminar shear stress of ultra-thin-walled lenticular collapsible composite tube in fold deformation. COMPOS STRUCT, 2013; 97: 64-75
[10] Xiong JJ, Shenoi RA*, Gao J. An analytical model to predict residual thermal stress in 2D orthogonal plain weave fabric composites. INT J SOLIDS STRUCT, 2009; 46: 1872-1883
[11] Xiong JJ, Shenoi RA*, Cheng X. A modified micromechanical curved beam analytical model to predict the tension modulus of 2D plain weave fabric composites. COMPOS PART B-ENG, 2009; 40: 776-783
[12] Xiong JJ, Shenoi RA*. A durability model incorporating safe life methodology and damage tolerance approach to assess first inspection and maintenance period for structures. RELIAB ENG SYST SAFE, 2009; 94: 1251-1258
[13] Xiong JJ, Shenoi RA*. A load history generation approach for full-scale accelerated fatigue tests. ENG FRACT MECH, 2008; 75: 3226-3243
[14] Xiong JJ, Shenoi RA*. A practical randomization approach of deterministic equation to determine probabilistic fatigue and fracture behaviours based on small experimental data sets. INT J FRACTURE, 2007; 145: 273-283
[15] Xiong JJ, Shenoi RA*. A two-stage theory on fatigue damage and life prediction of composites. COMPOS SCI TECHNOL, 2004; 64: 1331-1343
