1. Li Guangli, Cui Kai, Xu Yingzhou, Wang Haoxiang, Yang Jing, Xu Xiangui，Experimental investigation of a hypersonic I-shaped configuration with a waverider compression surface，SCIENCE CHINA Physics, Mechanics & Astronomy63(5), 254721,2020
2. 王浩祥, 李广利，徐应洲，崔凯，高压捕获翼构型跨声速流动特性初步研究，空气动力学学报，38（3）：441-447，2020
3. Kai Cui*, Yao Xiao, Yingzhou Xu and Guang Li Li*，Hypersonic I-shaped aerodynamic configurations，Science China Physics Mechanics Astronomy，Science China Physics Mechanics Astronomy，2018 Vol. 61 No. 2: 024722
4. Kai Cui*, Guang Li Li, Yao Xiao, Ying-Zhou Xu，High-Pressure Capturing Wing Configurations，AIAA Journal, 2017, Vol.55: 1909-1919
5. Kai Cui*, Shouchao Hu, Guangli Li, Qu Zhipeng, Ming Situ，Conceptual design and aerodynamic evaluation of hypersonic airplane with double flanking air inlets，Science China Technological Sciences, 56（8）：1980-1988，2013
6. Gao TaiYuan; Cui Kai*; Wang XiuPing;Hu Shouchao，Aerodynamic optimization and evaluation for the three-dimensional afterbody/nozzle integrated configuration of hypersonic vehicles，Chinese Science Bulletin，57 （8）: 849-857，2012
7. Kai Cui*, Guo-Wei Yang，Shape Optimization for Hypersonic Arc-Wing Missiles，Journal of Spacecraft and Rockets, 47: 694-700, 2010
8. Guowei Yang, Dawei Chen, Kai Cui*, Response Surface Technique for Static Aeroelastic Optimization on a High-Aspect-Ratio Wing, Journal of Aircraft, 2009, Vol.46: 1444-1450
9. Cui Kai*, Zhao Dongxu, Yang Guowei, Waverider configurations derived from general conical flowfields, Acta Mechanica Sinica, 2007，23(3): 247-255
10. Cui Kai*, Yang GuoWei, The effect of conical flowfields on the performance of waveriders at Mach 6, CHINESE SCIENCE BULLETIN, 2007, 52(1): 57-64
11. Cui Kai*，Yang GuoWei, A Continuation Method of Parameter Inversion for Non-Equilibrium Convection-Dispersion Equation, Chinese Physics Letters, Vol. 22, No. 11, 2005, 2738-2741
12. Li Guang-li, Kai Cui*, Xiao Yao, Yingzhou Xu，Effects of Shock Impingement on Aerothermal and Aerodynamic Performance for High-pressure Capturing Wings ，AIAA 2017-2199，2017
13. Yingzhou Xu, Kai Cui*, Li Guang-li, Xiao Yao，Study on Compression Surface Deformation of Waveriders，AIAA 2017-2200，2017
14. Xiao Yao, Kai Cui*, Li Guang-li, Yingzhou Xu，Preliminary Study of Aerodynamic Performance for Waverider-based Hypersonic Vehicles with Dorsal Mounted Engines，AIAA 2017-2315，2017
15. Kai Cui*, Guangli Li, Yao Xiao，Aerodynamic performance study of high pressure zone capture wing configurations，AIAA-2015-3388，2015
16. Kai Cui*, Shouchao Hu, Guangli Li, Yao Xiao, Ming Situ，A Conceptual Design of Next Generation Hypersonic Air-breathing Airplanes with Dual Waveriders Forebody，AIAA-2015-3646，2015
17. Kai Cui*, Shouchao Hu，Shape design to minimize the peak heat-flux of blunt leading-edge，AIAA-2013-233，2013
18. Cui Kai*, Wang Xiuping, Hu Shouchao, Gao Taiyuan, Yang Guowei，Shape optimization of high-speed train with the speed of 500kph，Lecture Notes in Electrical Engineering, 148：187-197, 2011
19. 崔凯,徐应洲, 广利,肖尧,王浩祥，升阻比对可重复使用运载器爬升特性影响，中国科学: 技术科学, 49卷, 8期: 891-900(2019)
20. 崔凯*，徐应洲，李广利，肖尧, 乘波体压缩面变化对其气动性能影响分析, 力学学报,2017,49(1):75-83
21. 胡守超，崔凯*，李广利，肖尧，司徒明, 基于实验设计方法的高超声速飞机前缘型线优化分析, 力学学报,2016,48(2):290-299
22. 李广利，崔凯*，肖尧，徐应洲, 高压捕获翼位置设计方法研究, 力学学报,2016,48(3):576-584
23. 李广利，崔凯*，肖尧，徐应洲, 高压捕获翼前缘型线优化和分析, 力学学报,2016,48(4): 877-885
24. 高太元，崔凯*，胡守超，王秀平, 高超声速飞行器上壁面多目标优化及性能分析, 力学学报,2013,45(2):193-201
25. 崔凯*，李广利，胡守超，屈志朋, 高速飞行器高压捕获翼气动布局概念研究, 中国科学 物理学 力学 天文学,2013,43(5):652-661
26. 崔凯*，胡守超，李广利，屈志朋，司徒明, 双旁侧进气高超声速飞机概念设计与评估, 中国科学 技术科学,2013,43(10):1085-1093
27. 高太元，崔凯*，胡守超，王秀平, 高超声速飞行器上壁面多目标优化及性能分析, 力学学报,2013,45(2):193-201
28. 崔凯*，李广利，胡守超，屈志朋, 高速飞行器高压捕获翼气动布局概念研究, 中国科学 物理学 力学 天文学,2013,43(5):652-661
29. 崔凯*，胡守超，李广利，屈志朋，司徒明, 双旁侧进气高超声速飞机概念设计与评估, 中国科学 技术科学,2013,43(10):1085-1093
30. 高太元，崔凯*，王秀平，胡守超，杨国伟，任亮, 三维后体/尾喷管一体化构型优化设计及性能分析, 科学通报,2012,57(4):239-247
31. 张锋涛，崔凯*，杨国伟, 基于神经网络技术的乘波体优化设计, 力学学报,2009,41(3):418-424
