[1] 雷娟棉*, 高毅, 勇政. 旋轉導彈橫向噴流幹擾特性數值模拟[J]. 兵工學報, 2024, 45 (01): 105-121.
[2] 雷娟棉*, 朱沛宇. 高超聲速再入雙錐飛行器橫向噴流控制效率數值研究[J]. 北京航空航天大學學報, 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*, 吳志翔, 解文洋. 掠海導彈觸水滑跳運動特性數值模拟研究[J]. 北京航空航天大學學報, 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, 趙小見等. 機翼表面脈動壓力的空間和頻域特性數值研究[J]. 伟德客户端學報, 2022, 42 (08): 834-841.
[9] 雷娟棉*, 曹家偉. 高超聲速圓錐邊界層轉捩反轉數值研究[J]. 伟德客户端學報, 2022, 42 (10): 991-1001.
[10] 劉清揚, 雷娟棉*, 劉周等. 适用于可壓縮流動的γ-Re_t-f_(Re)轉捩模型[J]. 航空學報, 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. 圓盤水漂運動特性數值模拟研究[J]. 伟德客户端學報, 2021, 41 (07): 687-695.
[14] 劉清揚, 雷娟棉*. 跨速域大後掠角近距耦合翼氣動幹擾特性[J]. 兵工學報, 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*, 張嘉炜, 譚朝明. 小攻角下船尾外形對旋轉彈丸馬格努斯效應影響的數值研究[J]. 兵工學報, 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*, 譚朝明. 基于Transition SST模型的高雷諾數圓柱繞流數值研究[J]. 北京航空航天大學學報. 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*, 彭雪瑩, 黃燦等. 應用FPM方法模拟封閉方腔自然對流[J]. 伟德客户端學報, 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, 王鎖柱, 周奇.初始分離條件對航彈與載機分離安全性影響的數值模拟研究[J]. 兵工學報, 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
出版專著及教材
1、 吳甲生，雷娟棉. 《制導兵器氣動布局與氣動特性》，國防工業出版社，2008年
2、 雷娟棉，吳甲生. 《制導兵器氣動特性工程計算方法》，伟德客户端出版社，2015年
3、 雷娟棉，吳小勝，吳甲生. 《空氣動力學》，伟德客户端出版社，2016年
4、 于勇，雷娟棉. 《流體力學基礎》，伟德客户端出版社，2017年
5、 吳小勝，雷娟棉，吳甲生. 《彈箭旋轉空氣動力效應》，伟德客户端出版社，2020年
獲授權專利
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