[1] 雷娟棉*, 高毅, 勇政. 旋转导弹横向喷流干扰特性数值模拟[J]. 兵工学报, 2024, 45 (01): 105-121.
[2] 雷娟棉*, 朱沛宇. 高超声速再入双锥飞行器横向喷流控制效率数值研究[J]. 北京航空航天大学学报, 1-19.
[3] Liu Qi, Lei Juanmian*, Yu Yong, et al. Aeroelastic Response of Spinning Projectiles with Large Slenderness Ratio at Supersonic Speed[J]. Aerospace, 2023, 10(7): 646.
[4] Zhang Boqian, Lei Juanmian*. Numerical Study on Suction Control for Rotor Blade Airfoil Under Martian Atmosphere[J]. 2023.
[5] 雷娟棉*, 吴志翔, 解文洋. 掠海导弹触水滑跳运动特性数值模拟研究[J]. 北京航空航天大学学报, 1-12.
[6] Gao Yi, Lei Juanmian*. Numerical Investigation on Transient Effect of Jet Interference Characteristics of Lateral-Jet-Controlled Spinning Missile[J]. Aerospace, 2022, 9(8): 430.
[7] Gao Yi, Lei Juanmian*, Yin J. Magnus Effect over Aerodynamic Components of Spinning Missile[J]. International Journal of Aeronautical and Space Sciences, 2022, 23(3): 447-460.
[8] 雷娟棉*, 郭牧天, 赵小见等. 机翼表面脉动压力的空间和频域特性数值研究[J]. 北京理工大学学报, 2022, 42 (08): 834-841.
[9] 雷娟棉*, 曹家伟. 高超声速圆锥边界层转捩反转数值研究[J]. 北京理工大学学报, 2022, 42 (10): 991-1001.
[10] 刘清扬, 雷娟棉*, 刘周等. 适用于可压缩流动的γ-Re_t-f_(Re)转捩模型[J]. 航空学报, 2022, 43 (08): 327-337.
[11] Yin Jintao, Lei Juanmian*, et al. The aerodynamic characteristics and its estimation method of finned missile experiencing spin-deformation coupling motion[J]. Aerospace Science and Technology, 2021, 115.
[12] Zhang Jiawei, Lei Juanmian*, Niu Jianping. Numerical investigation of aerodynamic characteristics of free-spinning tail projectile with canards roll control[J]. Proceedings of the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, 2021, 235(6): 687-702.
[13] 雷娟棉*, 解文洋, 于勇等. 圆盘水漂运动特性数值模拟研究[J]. 北京理工大学学报, 2021, 41 (07): 687-695.
[14] 刘清扬, 雷娟棉*. 跨速域大后掠角近距耦合翼气动干扰特性[J]. 兵工学报, 2021, 42 (07): 1412-1423.
[15] Lei Juanmian*, Zhang Jiawei, Niu Jianping. Effect of active oscillation of local surface on the performance of low Reynolds number airfoil[J]. Aerospace Science and Technology, 2020, 99, 105774. 2020
[16] He Jiandong ,Lei Juanmian* . A GPU-Accelerated TLSPH Algorithm for 3D Geometrical Nonlinear Structural Analysis[J]. International Journal of Computational Methods, 16(7):1850114. 2019
[17] Lei Juanmian*, Qingyang Liu and Tao Li. Suction control of laminar separation bubble over an airfoil at low Reynolds number[J]. Proceedings of the Institution of Mechanical Engineers Part G-Journal of Aerospace Engineering, 233(1): 81-90. 2019
[18] Niu Jianping , Lei Juanmian*, Lu Tianyu . Numerical research on the effect of variable droop leading-edge on oscillating NACA 0012 airfoil dynamic stall[J]. Aerospace Science and Technology, 2018, 72: 476-485. 2018
[19] Yin Jintao, Wu Xiaosheng, Lei Juanmian, et al. (2018). Canards interference on the Magnus effect of a fin-stabilized spinning missile[J]. Advances in Mechanical Engineering 2018, 10(7): 1-16. 2018
[20] Lu Tianyu, Wu Xiaosheng, Lei Juanmian, Yin, et al. Numerical study on the aerodynamic coupling effects of spinning and coning motions for a finned vehicle[J]. Aerospace Science and Technology, 2018,77,399-408. 2018
[21] 雷娟棉*, 张嘉炜, 谭朝明. 小攻角下船尾外形对旋转弹丸马格努斯效应影响的数值研究[J]. 兵工学报, 38(9): 1705-1715. 2017
[22] Yin Jintao, Wu Xiaosheng, Lei Juanmian. Body-fin interference on the Magnus effect of spinning projectile in supersonic flows[J]. Engineering Applications of Computational Fluid Mechanics, 11(1): 496-512. 2017
[23] Lu Tianyu, Lei Juanmian*, Wu Xiaosheng, Yin, Jintao. Application of harmonic balance method to aerodynamic characteristics prediction of spinning vehicle[J]. Aircraft Engineering and Aerospace Technology,89(2):347-357. 2017
[24] 雷娟棉*, 谭朝明. 基于Transition SST模型的高雷诺数圆柱绕流数值研究[J]. 北京航空航天大学学报. 43(2)207-217. 2017
[25] Niu Jianping, Lei Juanmian*, He Jiandong. Radial basis function mesh deformation based on dynamic control points[J]. Aerospace Science and Technology, 64: 122-132. 2017
[26] Zhang Jiawei, Lei Juanmian*. Flow mechanism analysis of the Magnus effect for spinning finned projectile. 5th International Conference and Exhibition on Mechanical and Aerospace Engineering. Las Vegas, Nevada, USA, 2017
[27] Yin Jintao, Lei Juanmian*. Effect of elastic deformation on the aerodynamic characteristics of a spinning projectile. 5th International Conference and Exhibition on Mechanical and Aerospace Engineering. Las Vegas, Nevada, USA, 2017
[28] Lei Juanmian*, Peng Xueying. Improved kernel gradient free-smoothed particle hydrodynamics and its applications to heat transfer problems[J]. Chin. Phys. B, 25(2): 26-38. 2016
[29] Lei Juanmian*, He Jiandong. Adjoint-Based Aerodynamic Shape Optimization for Low Reynolds Number Airfoils[J]. Journal of Fluids Engineering, 138(2): 021401. 2016
[30] 雷娟棉*, 彭雪莹, 黄灿等. 应用FPM方法模拟封闭方腔自然对流[J]. 北京理工大学学报, 36(8): 771-776. 2016
[31] Zheng Zhiwei, Lei Juanmian*, Wu Xiaosheng. Numerical Simulation of the Negative Magnus Effect of a Two-Dimensional Spinning Circular Cylinder[J]. Flow Turbulence and Combustion, 98(1): 109-130. 2016
[32] Lei Juanmian*, Zhao Shuai, Wang Suozhu. Numerical study of aerodynamic characteristics of FSW aircraft with different wing positions under supersonic condition[J]. Chinese Journal of Aeronautics, 29(4): 914-923. 2016
[33] 雷娟棉*, 牛健平, 王锁柱, 周奇.初始分离条件对航弹与载机分离安全性影响的数值模拟研究[J]. 兵工学报, 37(2): 357-366. 2016
[34] Yin Jintao, Lei Juanmian, Wu Xiaosheng, Lu Tianyu. Aerodynamic characteristics of a spinning projectile with elastic deformation[J]. Aerospace Science and Technology, 51: 181-191. 2016
[35] Zheng Zhiwei, Lei Juanmian*. Application of the gamma-Re (theta) transition model to simulations of the flow past a circular cylinder[J]. Flow Turbulence and Combustion, 97(2): 401-426. 2016
出版专著及教材
1、 吴甲生，雷娟棉. 《制导兵器气动布局与气动特性》，国防工业出版社，2008年
2、 雷娟棉，吴甲生. 《制导兵器气动特性工程计算方法》，北京理工大学出版社，2015年
3、 雷娟棉，吴小胜，吴甲生. 《空气动力学》，北京理工大学出版社，2016年
4、 于勇，雷娟棉. 《流体力学基础》，北京理工大学出版社，2017年
5、 吴小胜，雷娟棉，吴甲生. 《弹箭旋转空气动力效应》，北京理工大学出版社，2020年
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