熊峻江，男， 1966 年 4 月生，博士，教授。熊峻江1986 年獲西北工業大學工學學士學位，後於 1992 和 1995 年，分別獲北京航空航天大學工學碩士與博士學位； 1996 年 1 月至 1997 年 10 月，北京航空航天大學博士後流動站工作； 1997 年 11 月至今，北京航空航天大學工作，此間， 2003 年 4 月至 2004 年 4 月，英國南安普敦大學訪問研究。
基本介紹
- 中文名：熊峻江
- 外文名：Xiong junjiang
- 國籍：中國
- 出生日期：1966年4月
- 職業：大學教授
- 畢業院校：西北工業大學
主持課題,發表論文,
主持課題
先後主持國家自然科學基金與航空基金等各類基金項目8項，國防預研與型號課題10餘項，其中獲中國高校科技進步一等獎1項（第1獲獎人），部級科技進步二等獎2項（均為第2獲獎人），三等獎2項。作為第一作者，在國內外學術刊物上發表論文70餘篇，其中SCI收錄論文21篇，EI收錄論文32篇。出版教材專著4部，譯著3部，其中獲全國優秀科技圖書二等獎1部（第2獲獎人），國防優秀科技圖書獎1部（第3獲獎人）。主講過《材料力學（I）》、《材料力學（II）》、《疲勞可靠性》、《飛行器結構力學（I）》和《飛行器結構力學（II）》等本科生課程，《斷裂力學及其套用》、《可靠性設計》和《結構可靠性》等研究生課程。
發表論文
[1]Cheng X, Xiong JJ. A Novel Analytical Model for Predicting the Compression Modulus of 2D PWF Composites. Composite Structures, (doi:10.1016/j.compstruct.2008.04.005)
[2]Xiong JJ, Shenoi RA, Zhang Y. Effect of the mean strength on the endurance limit or threshold value of the crack growth curve and two-dimensional joint probability distribution. Journal of Strain Analysis for Engineering Design, 2008; 43(4):243-257
[3]Xiong JJ, Shenoi RA. A Load History Generation Approach for Full-scale Accelerated Fatigue Tests. Engineering Fracture Mechanics, 2008; 75(10): 3226-3243
[4]Xiong JJ, Li YY, Zeng BY. A Strain-based Residual Strength Model of Carbon Fibre/Epoxy Composites Based on CAI and Fatigue Residual Strength Concepts. Composite Structures, 2008; 85: 29-42
[5]Xiong JJ, Shenoi RA. Integrated Experimental Screening of Bonded Composites Patch Repair Schemes to Notched Aluminum-alloy Panels Based on Static and Fatigue Strength Concepts. Composite Structures, 2008; 83: 266-272
[6]Xiong JJ, Shenoi RA. A Practical Randomization Approach of Deterministic Equation to Determine Probabilistic Fatigue and Fracture Behaviours Based on Small Experimental Data Sets. International Journal of Fracture, 2007; 145: 273-283
[7]Xiong JJ, Yu X. Helicopter Rotor-Fuselage Aeroelasticity Modeling and Solution using the Partition-Iteration Method. Journal of Sound and Vibration, 2007; 302(4-5): 821-840
[8]Xiong JJ, Shenoi RA. Single-point Likelihood Method to Determine a Generalized S-N Surface. Proceedings of the I Mech E, Part C: Journal of Mechanical Engineering Science, 2006; 220(10): 1519-1529
[9]Xiong Jun-Jiang. A nonlinear fracture differential kinetic model to depict chaotic atom motions at a fatigue crack tip based on the differentiable manifold methodology. Chaos, Solitons & Fractals, 2006; 29(5): 1240-1255
[10]Xiong JJ, Shenoi RA. An Integrated and Practical Reliability-based Data Treatment System for Actual Load History. Fatigue and Fracture of Engineering Materials and Structures, 2005; 28(10): 875-889
[11]Xiong JJ, Shenoi RA, Qiu H Y. Reliability-based Minimal Sample Factor Formulation for Corrosion Damage Assessment. Journal of Strain Analysis for Engineering Design, 2005; 40(8): 801-816
[12]Xiong JJ, Shenoi RA. Two new practical models for estimating reliability-based fatigue strength of composites. Journal of Composite Materials, 2004; 38(14): 1187-1209(23)
[13]Xiong JJ, Shenoi RA, Wang SP, Wang WB. On Static and Fatigue Strength Determination of Carbon Fibre/Epoxy Composites. Part II: Theoretical Formulation. Journal of Strain Analysis for Engineering Design, 2004; 39(5): 541-548
[14]Xiong JJ, Shenoi RA, Wang SP, Wang WB. On Static and Fatigue Strength Determination of Carbon Fibre/Epoxy Composites. Part I: Experiments. Journal of Strain Analysis for Engineering Design, 2004; 39(5): 529-540
[15]Xiong JJ, Shenoi RA. A two-stage theory on fatigue damage and life prediction of composites. Composites Science and Technology, 2004; 64(9): 1331-1343
[16]Xiong J, Shenoi RA and Gao Z. Small sample theory for reliability design. Journal of Strain Analysis for Engineering Design, 2002; 37(1): 87-92
