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.Chen D, Cheng ZQ, Cunningham PR*, Xiong JJ. Fatigue life prediction of 2524-T3 and 7075-T62 thin-sheet aluminium-alloy with an initial impact dent under block spectrum loading. FATIGUE FRACT ENG M, DOI: 10.1111/ffe.13416
.Zhu YT, Xiong JJ*, Luo CY, Du YS. Progressive damage characteristics of screwed single-lap CFRPI-metal joint under tensile loading at RT and 350 °C. J COMPOS MATER, doi: 10.1177/0021998320985595
.Xiong Jun-jiang*, Zhu Yun-tao, Luo Chu-yang, Li Yu-sheng. Fatigue-driven failure criterion for progressive damage modelling and fatigue life prediction of composite structure. INT J FATIGUE, https://doi.org/10.1016/j.ijfatigue.2020.106110
.Wan Ao-Shuang, Xu Yi-Geng, Xue Li-Heng, Xu Ming-Rui, Xiong Jun-Jiang*. Finite element modeling and fatigue life prediction of helicopter composite tail structure under multipoint coordinated Loading spectrum. COMPOS STRUCT, 2021; 255: 112900
.Wan AS, Xiong JJ, Xu YG*. Fatigue Life Prediction of Woven Composite Laminates with Initial Delamination. FATIGUE FRACT ENG M, 2020; 43(9): 2130-2146
.Cheng ZQ, Xiong JJ*. Progressive Damage Behaviors of LVI, TAI and CAI for Woven Composite Laminates. CHINESE J AERONAUT, 2020; 33(10): 2807-2823,2020
.Zhu YT, Xiong JJ*. High temperature effect on mechanical performance of CFRP-Ti alloy joints. J COMPOS MATER, 2020; 54(17): 2245-2260,2020
.Zhu YT, Akkerman R, Xiong JJ*, Luo CY, Du YS. Evaluation of insert design on the performance of repaired composite-Ti alloy joints. COMPOS STRUCT, 2019; 230: 11506,2020
.Wan AS, Xu YG, Xiong JJ*. Notch effect on strength and fatigue life of woven composite laminates. INT J FATIGUE, 2019; 127: 275-290,2020
.Wan AS, Xiong JJ*. Effect of stress ratio on HCF and VHCF properties at temperatures of 20 °C and 700 °C for nickel-based wrought superalloy GH3617M. CHINESE J AERONAUT, 2019; 32(9): 2199-2210,2020
.Bai JB, Chen D, Xiong JJ*, Shenoi RA. Folding analysis of thin-walled deployable composite boom. ACTA ASTRONAUT, 2019; 159: 622–636,2020
.Jiang-Bo Bai*, Di Chen, Jun-Jiang Xiong*, Chen-Hao Dong. A semi-analytical model for predicting nonlinear tensile behaviour of corrugated flexible composite skin. COMPOS PART B-ENG, 2019; 168: 312-319,2020

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