（1）飞行器结构耐久性与损伤容限设计:飞机整体结构止裂分析，强化研究；

（2）复合材料和结构的设计与分析：复合材料冲击损伤容限，复合材料整体结构设计；

（3）结构健康监测: 结构健康监测方法与实验。

 国家自然科学青年基金：“空间缝合泡沫夹芯复合材料结构破坏机理分析和优化设计”（项目编号：10602035），主持已结题；

（1）Wang Xing, Xu Wu, Zhang Xiaojing, Zhang Lina, Hu Benrun,”Numerical Prediction and Experimental Verification of Fatigue Life of TC4 Plate Strengthened by Cold Expansion,” Journal of Zhejiang University(Engineering Science), Vol. 51, No. 8, pp. 1610-1618, 2017.

（2）Jin Zhuyu, Zhang Xiaojing,”Numerical Analysis of Reinforcement Effect of Z-Pins with Special-Shaped Cross-Section Under Mode I Delamination,” Journal of Shanghai Jiao Tong University, Vol. 50, No. 2, pp. 169-175,2016.

（3）Jin Zhuyu , Zhang Xiaojing , Wang Hai,” Numerical Simulations for the Mix-Mode Bending Test of the Stitched Laminates,” Engineering Mechanics, Vol. 33, No. 2, pp. 232-241+256, 2016.

（4）He Zhiming, Zhang Xiaojing, Liu Tianqi, Yang Shuxun,”Numerical Simulation of Whole Process of Cold Expansion in 300M Steel Lug,” Journal of Zhejiang University(Engineering Science), Vol. 50, No. 4, pp. 783-791, 2016.

（5）Liao Yu, Zhang Xiaojing, Zhang Lina,”Fatigue Life Prediction Based On Crack Closure For Shot Peening AI-Li Alloy SENT Specimen under Variable Amplitude Loading,” Journal of Shanghai Jiao Tong University, Vol. 50, No. 8, pp. 1233-1240, 2016.

（6）He Shijiu, Zhang Xiaojing, Wang Hai,”Analytical Methodology of Predicting Mode I Stress Intensity Factor for Cracked Panels with Bonded Stiffener,” Journal of Shanghai Jiao Tong University, Vol. 50, No. 2, pp. 251-257, 2016.

（7）Sun Jingjing, Zhang Xiaojing,Gong Zhanfeng, Wang Hai,”Failure Mechanism Study on Omega Stringer Debonding,” Acta Aeronautica et Astronautica Sinica, Vol. 34, No. 7, pp. 1616-1626, 2013.

（8）Tan Jianshe, Zhang Xiaojing, Zhang Junqi, Wang Hai,”Simulation of Impact Force and Energy Response of Composite Laminate Subjected to Low Velocity Impact,”Acta Materiae Compositae Sinica, Vol. 31, No. 4, pp. 970-980,2014.

（9）Xu Wu, Wang Hai, Wu Xueren, Zhang Xiaojing, Bai Guojuan, Huang Xianglong, “A novel method for residual strength prediction for sheets with multiple site damage: Methodology and experimental validation,” International Journal of Solids and Structures, Vol. 51, No. 3-4, pp. 551-565, 2014.

（10）Wang Yifei, Zhang Xiaojing, Wang Hai,”Low-velocity Impact Response of Composite Laminate and Its Relationship With Damage Parameters,” Chinese Journal of Solids and Mechanics, Vol. 34, No. 1, pp. 63-72, 2013.

（11）Huang Xianglong, Zhang Xiaojing, Bai Guojuan, Xu Wu, Wang Hai,”Residual Strength Prediction of Thin-Walled Structures With Multiple Site Damage Based on Crack Tip Opening Angle Method,”Journal of Shanghai Jiao Tong University, Vol. 47, No. 4, pp. 519-524+531,2013.

（12）Xiaojing. Zhang, Z. Jin, C. Chen, H. Wang, “Mechanical characteristic and strength prediction of filled-hole composite laminate under compression loading,” 19^th international conference on composite materials. Montreal, Canada. Aug.2013

（13）Xiaojing Zhang, Jianshe Tan, Yifei Wang, Zhefeng Yu, Hai Wang. “An Experimental and Numerical Study on Impact Response and Damage of CompositeOmega Stringer,” 15^th Australian International Aerospace Congress. Melbourne, Australian. Feb. 2013