国家科技进步二等奖；全军科技进步二等奖、三等奖（2次）；工信部一等奖；航空航天部科技进步三等奖（2次）；兵工部科技进步三等奖（2次）；海军等其他省部级奖励若干……
[1]主编国家出版基金项目专著《发射气体动力学》；
[2]主编国家出版基金项目专著《发射动力学》；
1 Inhibition Effect of Water Injection on Afterburning of Rocket Motor Exhaust Plume 中国航空学报（英文版） 姜毅；马艳丽；王伟臣；邵立武 2010 SCI、EI
2 舰载导弹垂直发射系统燃气流场的三维数值计算 12博BET官方网站学报 姜毅 2002 核心
3 双喷管火箭发动机燃气流场的三维数值计算与试验 12博BET官方网站学报 姜毅；刘琪；王刚 2002 核心
4 机载导弹发射时燃气流场的数值 弹箭与制导学报 姜毅；张晓琳；刘琪 2002 核心
5 冲压式舵机腔内工作压力随飞行速度变化规律的数值仿真 兵工学报 姜毅；刘琦；张晓琳 2004 EI
6 斜喷管燃气射流气动干扰数值模拟 宇航学报 傅德彬；姜毅；张杰 2004 EI
7 燃气射流气固两相数值模拟与颗粒冲刷分析 弹箭与制导学报 傅德彬；姜毅 2004 核心
8 燃气射流气固两相流场研究 12博BET官方网站学报 傅德彬；姜毅；袁增凤 2004 EI
9 同心筒自力发射燃气排导优化设计 弹箭与制导学报 傅德彬；姜毅；陈建伟；刘琦 2004 核心
10 发射装置刚柔耦合仿真分析 弹箭与制导学报 傅德彬；姜毅；刘琦 2004 核心
11 燃气射流对发射车轮胎作用仿真 弹箭与制导学报 刘群；姜毅；郝继光；傅德彬 2005 核心
12 燃气流作用对车载箱式发射的动力学影响 导弹与航天运载技术 傅德彬；姜毅；刘琦 2006 核心
13 导弹头部气动加热的流固耦合数值模拟 弹箭与制导学报 郝继光；姜毅；刘琦 2006 核心
14 同心筒垂直发射装置排导燃气流的改进 12博BET官方网站学报 姜毅；郝继光 2007 EI
15 用动网格方法模拟导弹发射过程中的燃气射流流场 宇航学报 傅德彬；姜毅 2007 EI
16 一种新的动网格更新技术及其应用 弹道学报 郝继光；姜毅； 韩书永; 廖庆 2007 EI
17 液压系统半实物仿真平台设计 系统仿真学报 傅德彬；姜毅； 张强 2007 EI
18 燃气射流对发射车天线影响分析 弹箭与制导学报 刘群；姜毅；郝继光 2007 EI
19 某导弹易碎盖的开启过程 固体火箭技术 傅德彬；姜毅 2007 EI
20 Compensator design for aspheric testing using virtual glass model 3rd International Symposium on Advanced Optical Manufacturing and Testing Technologies 姜毅；王萍；齐月静；魏楠 2007 EI
21 某型导弹发动机推进剂恶劣工况下温度仿真研究 兵工学报 刘群；姜毅；郝继光 2007 EI
22 基于FPGA的非标准二次群路的分接处理 2007仪表、自动化及先进集成技术大会论文集 姜毅；齐月静 2008 EI
23 新型“引射同心筒”垂直发射装置理论及试验研究 宇航学报 姜毅；郝继光；傅德彬；耿峰 2008 EI
24 导弹发动机推进剂恶劣工况下温度分析 中北大学学报 姜毅；王艳彬；刘群 2008 EI
25 液压系统半实物仿真通信过程实施 系统仿真学报 傅德彬；姜毅；张强 2008 EI
26 固体火箭发动机尾喷焰复燃流场计算 宇航学报 姜毅；傅德彬 2008 EI
27 导弹发射过程三维非定常数值模拟 兵工学报 姜毅；郝继光；傅德彬 2008 EI
28 导弹发射筒盖开启过程数值计算及试验 弹道学报 姜毅；耿峰；张强 2008 EI
29 基于刚柔耦合模型的发射装置动力学仿真分析 系统仿真学报 傅德彬；姜毅 2009 EI
30 基于MSDM方法的粒子-固壁侵蚀效应研究 固体火箭技术 傅德彬；姜毅 2009 EI
31 Numerical simulation of the erecting system for large device 2009 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2009 姜毅；张强；傅德彬；席运阳 2009 EI
32 基于容腔节点法的液压起竖系统仿真 机床与液压 张强；姜毅；傅德彬；席运阳 2010 核心
33 某低空低速飞行器气动特性计算 战术导弹技术 马艳丽；姜毅；郝继光 2010 核心
34 固体发动机燃气射流对发射平台冲击效应研究 固体火箭技术 马艳丽；姜毅；郝继光；赵刚练 2010 EI
35 湿式同心筒自力垂直热发射技术降温效果研究 弹道学报 马艳丽；姜毅；王伟臣；颜凤；郝继光 2010 EI
36 Optimization design of the rocket launching facilities and the thermal protection 2nd IEEE International Conference on Advanced Computer Control, ICACC 2010 姜毅；马艳丽；王伟臣；郝继光 2010 EI
37 12博BET官方网站学报（英文版） 马艳丽；姜毅；郝继光；刘伯伟 2010 EI
38 湿式独立自排导垂直发射技术研究 导弹与航天运载技术 马艳丽；姜毅；王伟臣；刘伯伟；颜凤 2011 核心
39 同心筒发射过程燃气射流冲击效应研究 固体火箭技术 马艳丽；姜毅；王伟臣；郝继光；赵刚练 2011 EI
40 固体火箭发动机尾焰注水流场实验研究 弹箭与制导学报 姜毅；周帆；张学文 2011 EI
41 舰载导弹垂直弹射出筒姿态影响因素分析 弹箭与制导学报 陈余军；姜毅 2011 EI
42 炮射导弹气动特性数值计算 12博BET官方网站学报 郭庆阳；姜毅；郭利强；石庚辰 2011 EI
43 喷水对火箭发动机羽流红外特性的抑制作用研究 12博BET官方网站学报 马艳丽；姜毅；王伟臣；郝继光；赵刚练 2011 EI
44 新型舰载同心筒发射过程流场研究 导弹与航天运载技术 邵立武；姜毅；马艳丽；王伟臣 2011 核心
45 超声速高温冲击射流注水流场实验研究 实验流体力学 姜毅；周帆；张学文 2011 EI
46 含侧喷流炮射导弹绕流场数值计算 12博BET官方网站学报 郭庆阳；姜毅；于天朋；石庚辰 2011 EI
47 舰载导弹发射数值模拟与点火时机研究 固体火箭技术 陈余军；姜毅；赵刚练 2011 EI
48 车载导弹行进间发射动力学仿真 弹箭与制导学报 陈余军；姜毅 2011 EI
49 Simulation and optimize design for deflector plate of the Vehicle mounted Vertically Thermal Launched missile Advanced Materials Research 于邵祯；姜毅；马艳丽；马艳艳；刘伯伟 2012 EI
50 火箭发动机尾焰流场注水降温效果初探 推进技术 周帆；姜毅；郝继光 2012 EI
51 基于有限状态机的多级液压缸仿真分析 机床与液压 邵立武；姜毅；傅德彬；马艳艳 2012 核心
52 车载导弹发射过程姿态模拟 弹道学报 陈余军；姜毅； 2012 EI
53 Parametric design of parts in an integrated simulation system based on asynchronous mode of pro/TOOLKIT Advanced Mechanical Design 赵刚练；姜毅；陈余军；马艳丽 2012 EI
54 Research on the jet influence on the mechanical launcher of various ignition height Lecture Notes in Electrical Engineering 贺卫东；姜毅；马艳丽 2012 EI
55 Study on the deployment process of low attitude interception net Advances in Intelligent and Soft Computing 周笑飞；姜毅；李永远 2012 EI
56 Numerical simulation on the influence of altitude on jet flow field Lecture Notes in Electrical Engineering 刘伯伟；姜毅；宋洋；于邵祯 2012 EI
57 Optimization design for launch box based on the effect of the shock wave Lecture Notes in Electrical Engineering 于邵祯；姜毅；邓佳；刘伯伟；赵刚练 2012 EI
58 Study on the Firing Table Compiling of a new type of the very low altitude interception device Advanced Research on Engineering Materials, Energy, Management and Control 钟洲；姜毅；李永远；张冲 2012 EI
59 火箭发动机射流复杂噪声测量数据时频分析 弹箭与制导学报 周帆；姜毅；张学文；郝继光 2012 EI
60 A new method of integrate simulation based on ADAMS and pro/ENGINEER 4th International Conference on Mechanical and Electrical Technology, ICMET 2012 赵刚练；姜毅；陈余军；马艳丽 2012 EI
61 Analysis of concentric canister wall roughness effect on jet flow based on fluid dynamics 2012 International Conference on Applied Mechanics and Manufacturing System, AMMS 2012 拜云山；姜毅；周东默 2013 EI
62 Research on the initial disturbance of vehicular missile with system vibration analysis 2012 International Conference on Mechanics, Dynamic Systems and Material Engineering, MDSME 2012 张冲；姜毅 2013 EI
63 Launching dynamics simulation of ship-board rocket gun 2012 International Conference on Mechanics, Dynamic Systems and Material Engineering, MDSME 2012 曾伟；姜毅 2013 EI
64 Mechanics analysis with different open lid time on shockwaves in launch box 2013 3rd International Conference on Automation, Communication, Architectonics and Materials, ACAM 2013 曹全峥；姜毅；杨征然；于邵祯 2013 EI
65 Deflecting features of gas from double-faced deflector and structure optimization of deflector 2013 International Conference on Applied Mechanics, Materials and Mechanical Engineering, AMME 2013 史少岩；姜毅；董晓彤 2013 EI
66 Failure analysis of a composite frangible cover based on transient dynamics 3rd International Conference on Advanced Design and Manufacturing Engineering, ADME 2013 曾伟；姜毅 2013 EI
67 间接法求解具有最大横程的再入轨迹 12博BET官方网站学报 李永远；姜毅;；高伟涛；黄春平 2013 EI
68 考虑导轨间隙的在轨分离动力学计算方法 力学学报 赵刚练；姜毅；陈余军；董晓彤 2013 EI
69 考虑圆柱铰链间隙的多刚体系统动力学计算方法 振动与冲击 赵刚练；姜毅；郝继光；陈余军；龚俊斌 2013 EI
70 汽化效应对燃气蒸汽式弹射气液两相流场的影响 固体火箭技术 刘伯伟；姜毅 2013 EI
71 基于遗传算法的导弹发射系统设计参数优化 弹箭与制导学报 曾伟；姜毅 2013 核心
72 车载防空导弹行进发射过程动力学数值分析 兵工学报 钟洲；姜毅；刘群 2013 EI
73 基于FFT算法的舰载导弹发射弹位研究 振动与冲击 钟洲；姜毅 2013 EI
74 Dynamic simulation analysis of shipborne missile launching under high-wave-level environment 2012 International Conference on Advanced Materials Design and Mechanics, ICAMDM 2012 钟洲；姜毅；李永远；张冲 2013 EI
75 导轨排气孔对发射箱内流场影响的计算分析 固体火箭技术 牛钰森；姜毅；史少岩 2013 EI
76 挠性航天器在轨分离冲击缓冲模糊滑模控制研究 固体火箭技术 赵刚练；姜毅；陈余军；刘冬 2013 EI
77 An improved rollover index based on BP neural network for hydropneumatic suspension vehicles,MATHEMATICAL PROBLEMS IN ENGINEERING. 文献号: 7859521 DOI: 10.1155/2018/7859521 出版年: 2018
78 Detection Probability for Moving Ground Target of Normal Distribution Using an Imaging Satellite.CHINESE JOURNAL OF ELECTRONICS 卷: 27 期: 6 页: 1309-1315 DOI: 10.1049/cje.2018.08.005 出版年: NOV 2018
79 Rollover threshold investigation of a heavy-duty vehicle during cornering based on multi-body dynamics. ADVANCES 80 IN MECHANICAL ENGINEERING卷: 10 期: 7 文献号: 1687814018789505 DOI: 10.1177/1687814018789505 出版年: JUL 19 2018
81 The Impact of Concrete Pavement Field Floor to Vehicle Missile Launching Process. INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING 文献号: 1624107 DOI: 10.1155/2017/1624107 出版年: 2017
82 The coupling effects of the missile launcher and the ground in vehicle-mounted missile erecting. ADVANCES IN MECHANICAL ENGINEERING 卷: 8 期: 7 文献号: 1687814016656106 DOI: 10.1177/1687814016656106 出版年: JUL 2016
83 Cooling Effect of Water Injection on a High-Temperature Supersonic Jet. ENERGIES 卷: 8 期: 11 页: 13194-13210 DOI: 10.3390/en81112363 出版年: NOV 2015
84 Mobile Network Computer Can Better Describe The Future of Information Society. CHINA COMMUNICATIONS 卷: 13 期: 12 页: 90-96 DOI: 10.1109/CC.2016.7897558 出版年: DEC 2016
85 Mobile Network Computers Should be the Terminal of Mobile Communication Networks. WIRELESS PERSONAL COMMUNICATIONS 卷: 85 期: 4 页: 1895-1904 DOI: 10.1007/s11277-015-2878-0 出版年: DEC 2015
86 Research on the Simulation Method of Missile Adapter's Separation Based on Combined Calculation. INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING 文献号: 9804190 DOI: 10.1155/2019/9804190 出版年: 2019
87 Horizontal Backward Launch Dynamics Modeling and Analysis. INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING 文献号: 4098398 DOI: 10.1155/2019/4098398 出版年: 2019
88 Assessing Turbulence Models on the Simulation of Launch Vehicle Base Heating. INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING 文献号: 1624107 DOI: 10.1155/2019/1624107 出版年: 2019
89 The effect of thrust eccentric and erection cylinder anchor position on the initial disturbances. Advanced Materials Research, v 889-890, p 165-169, 2014
90 Analysis of a missile's initial disturbance. Advanced Materials Research, v 889-890, p 152-155, 2014
Coupling of missile-launcher in vertical thermal launch process. Zhendong yu Chongji/Journal of Vibration and Shock, v 33, n 1, p 89-94, January 15, 2014
91 Study on the cooling effect of water injection on flame of vertical launch system. Guti Huojian Jishu/Journal of Solid Rocket Technology, v 38, n 5, p 628-634, October 1, 2015
92 Numerical analysis of fragile back cover opening process coupling with jet flow. Binggong Xuebao/Acta Armamentarii, v 36, n 1, p 87-93, January 1, 2015
93 Dynamics numerical analysis of vehicle-mounted antiaircraft missile launching on the move. Binggong Xuebao/Acta Armamentarii, v 35, n 1, p 83-87, January 2014
94 Analysis on the effect of shipborne missile launch position based on fast Fourier transform. Zhendong yu Chongji/Journal of Vibration and Shock, v 33, n 13, p 210-214, July 15, 2014
95 Numerical calculation on the influence of missile exhaust plume with mechanical properties to the double-launch box. Advanced Materials Research, v 978, p 101-105, 2014
96 Influence of vaporization effect on gas-liquid two-phase flow field of ejection in combustion gas and vapor mode. Guti Huojian Jishu/Journal of Solid Rocket Technology, v 37, n 2, p 156-160, April 2014
97 Calculation and analysis about the impact of guide vents on the flow field inside the launching canister. Guti Huojian Jishu/Journal of Solid Rocket Technology, v 37, n 2, p 161-166, April 2014
98 Research on Efficiency of Additional Thrust of Thermal Launching. Binggong Xuebao/Acta Armamentarii, v 37, n 6, p 1038-1043, June 10, 2016
99 Effect of Rocket Engine Jet Flow with Water Injection on Air-flow Exhaust of Gas-flow-guided Channel. Binggong Xuebao/Acta Armamentarii, v 38, n 1, p 97-105, January 13, 2017
100 Research on distribution of flow field in launching canister with the effect of nozzle closure. Binggong Xuebao/Acta Armamentarii, v 35, n 11, p 1805-1812, November 1, 2014
