熊峻江

熊峻江

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。

基本信息

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

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