氢原子百科 
人物经历
1996.09-2000.07南京理工大学机械学院火箭武器本科
2000.09-2005.07南京理工大学机械工程学院兵器发射理论与技术专业博士
2005.07-南京理工大学机械工程学院教师（期间：2008.04副研究员，2010.05-2011.04加拿大McMasterUniversity博士后，2011.06-2011.09加拿大McMasterUniversity访问教授，2011.11南京理工大学机械工程学院院长助理兼航空宇航系副主任、主任，2011.05-2012.08挂职科技处处长助理）
中文论文
固体火箭冲压发动机含硼推进剂燃烧性能实验研究[J].赵瑞杰，张淋清，蔡文祥，任建德，王禄浩，陈雄.推进技术.
NEPE推进剂在氮气/空气中的点火燃烧特性[J].涂乘崟，陈雄，周长省，张北辰，李连波.含能材料.
基于热力学理论的固体推进剂粘弹-粘损伤本构模型[J].李辉，范兴贵，许进升，陈雄，刘家铭.推进技术.
热老化改性双基推进剂拉伸力学性能及强度主曲线[J].刘家铭，许进升，陈雄，李辉，范兴贵.含能材料.2021(09)
NEPE推进剂低高应变率下改进的黏-超弹本构模型[J].孙政伟，许进升，周长省，陈雄，杜红英.爆炸与冲击.2021(03)
HTPB推进剂疲劳特性试验研究[J].许进升，杨晓红，陈雄，杜红英，李辉.火炸药学报.2021(03)
不同能量分配下的双脉冲发动机外弹道特性研究[J].刘万励，李映坤，陈雄.兵工自动化.2020(10)
旋转爆震发动机与涡轮机的集成[J].李连波，陈雄，周长省，周胜兵.科学技术与工程.2020(26)
[9]推进剂组分对固体燃料冲压发动机性能的影响[J].邱爽，苏莹莉，杨海涛，陈雄，周长省.航空动力学报.2020(09)
基于舵机位置环的自适应模糊滑模复合控制[J].王献策，陈雄，柴金宝，冯恺鹏.计算机仿真.2020(08)
聚能射流对固体火箭发动机的冲击起爆[J].庞嵩林，陈雄，许进升，王永平.爆炸与冲击.2020(08)
[12]碳黑对固体燃料冲压发动机旋流燃烧特性影响[J].汤长俊，陈国光，陈雄，李唯暄.航空动力学报.2020(07)
可变流量燃气发生器压强自适应控制方法研究[J].周景亮，陈雄，柴金宝，周长省.计算机仿真.2020(07)
复合固体推进剂颗粒与基体初始界面有无缺陷的细观模型对比[J].侯宇菲，许进升，周长省，陈雄，李宏文.兵工学报.2020(09)
固体推进剂用碳纤维HTDE接枝改性及其表面性能研究[J].曹迪，汪路路，陈雄，许进升.塑料工业.2020(05)
长尾喷管传热及烧蚀特性研究[J].杨玉龙，郑健，陈雄，周长省.推进技术.2021(05)
固体火箭冲压发动机流量可调燃气发生器控制算法[J].周景亮，陈雄，柴金宝，李心怡，李旭东，周长省.航空动力学报.2020(05)
高超声速流场支杆射流减阻降热的流热耦合[J].马坤，朱亮，陈雄，李映坤，周长省.航空动力学报.2020(04)
基于流固耦合的斜激波冲击作用下曲壁板气动弹性分析[J].李映坤，陈雄，许进升.航空动力学报.2020(04)
基于扩张状态观测器的燃气舵舵机位置控制[J].王献策，陈雄，葛中杰，马睿.推进技术.2020(10)
一种软隔层双脉冲固体火箭发动机点火冲击仿真分析[J].王坚，陈雄，许进升，李宏文.南京理工大学学报.2019(06)
[22]双脉冲发动机Ⅱ脉冲点火瞬态工作特性研究[J].黄波，李映坤，陈雄.弹道学报.2019(04)
旋流与炭黑对聚乙烯固体燃料冲压发动机工作性能的影响[J].李唯暄，杨海涛，陈雄，薛素林.推进技术.2020(06)
基于高分辨率数据重构的固体燃料冲压发动机燃料平均燃速测试[J].邱爽，李映坤，李唯暄，陈雄，王禄浩.航空动力学报.2019(11)
前台阶内型面对固体燃料冲压发动机燃烧性能的影响[J].苏莹莉，陈雄，李唯暄，邱爽.固体火箭技术.2019(05)
温度载荷下长径比与m数对组合装药结构影响分析[J].王晨飞，许进升，陈雄.弹箭与制导学报.2019(06)
考虑颗粒形状的复合固体推进剂细观损伤分析[J].侯宇菲，许进升，陈雄，周长省，朱亮.固体火箭技术.2019(04)
[28]双脉冲发动机EDPM软隔层含率相关能量限制器的黏超弹本构模型[J].范兴贵，许进升，陈雄.固体火箭技术.2019(03)
基于热解过程的EPDM变热物性数值传热[J].黄波，李映坤，陈雄，薛海峰.航空动力学报.2019(06)
高校基层学术组织改革的实践研究[J].乔莉，何勇，陈雄.南京理工大学学报(社会科学版).2019(03)
旋流燃烧室对固体燃料冲压发动机药柱表面传热以及燃速的影响[J].李唯暄，陈雄，周长省，MUSAOmer.航空动力学报.2019(04)
铝镁贫氧推进剂中铝颗粒团聚特性[J].李连波，陈雄，周长省，朱敏，赖华锦.含能材料.2019(09)
基于人工蜂群算法优化的燃气发生器压强自适应模糊免疫PID控制[J].柴金宝，陈雄，周景亮，何坤.推进技术.2019(02)
应力控制下HTPB推进剂的疲劳损伤及寿命研究[J].梁蔚，陈雄，许进升.化工新型材料.2018(11)
跟踪微分器在变流量燃气发生器上的应用研究[J].柴金宝，陈雄，何坤，周景亮，李旭东.推进技术.2019(05)
复合固体推进剂颗粒/基体界面参数反演优化[J].封涛，许进升，陈雄，周长省.计算机仿真.2018(09)
[37]双脉冲发动机EPDM软隔层黏超弹本构模型[J].范兴贵，许进升，陈雄，杜红英，李映坤，张中水.航空学报.2018(11)
循环加载下复合推进剂的能量耗散[J].童心，陈雄，许进升，杜红英，周长省.航空学报.2018(11)
HTPB推进剂温度相关性失效准则[J].李辉，许进升，周长省，陈雄，郑健.含能材料.2018(09)
含初始缺陷的复合固体推进剂力学性能[J].封涛，许进升，韩龙，陈雄，周长省.航空材料学报.2018(03)
旋流燃烧室构型对固体燃料冲压发动机自持燃烧性能影响[J].李唯暄，陈雄，周长省，杜红英.推进技术.2018(06)
考虑初始缺陷的HTPB推进剂粘超弹本构模型[J].封涛，许进升，范兴贵，韩龙，陈雄，周长省.含能材料.2018(04)
循环载荷下HTPB推进剂温度演化及疲劳性能预测[J].梁蔚，童心，许进升，陈雄.含能材料.2018(04)
基于Fuzzy-PI双模控制器的燃气发生器压强控制算法研究[J].柴金宝，陈雄，余业辉，崔二伟.推进技术.2018(05)
基于模糊神经网络PID的舵机控制系统[J].卜庆伟，陈雄，柴金宝，崔二伟.计算机与现代化.2018(03)
固体火箭推进剂过保温后力学性能试验研究[J].王鸿丽，许进升，陈雄，周长省.弹道学报.2018(01)
初始缺陷对复合固体推进剂力学性能影响的数值研究[J].封涛，许进升，韩龙，陈雄，周长省.功能材料.2018(02)
应力水平对HTPB推进剂疲劳特性的影响[J].梁蔚，许进升，陈雄.功能材料.2018(02)
细观结构对HTPB推进剂力学性能影响的数值研究[J].封涛，许进升，韩龙，陈雄，周长省.功能材料.2018(01)
侧向喷流对超声速流动中支杆减阻降热特性影响的研究[J].朱亮，陈雄，周长省，李映坤.推进技术.2018(02)
固冲发动机燃气发生器流量调节优化控制[J].柴金宝，陈雄，周景亮，何坤.计算机仿真.2019(02)
不同环境压强下炭黑含量对聚乙烯点火和燃烧性能的影响[J].杨海涛，陈雄，相恒升，巩伦昆，黄波.含能材料.2017(12)
膏体推进剂火箭发动机点火特性[J].叶小兵，陈雄，单新有，周长省，秦振杨.含能材料.2017(12)
炭/酚醛燃气舵烧蚀性能[J].薛海峰，陈雄，郑健，周长省.固体火箭技术.2017(06)
推力矢量发动机燃气舵系统设计与分析[J].卜庆伟，陈雄，崔二伟.科学技术与工程.2017(33)
负压环境下铝镁贫氧推进剂激光点火及燃烧特性[J].赖华锦，陈雄，周长省，相恒升.含能材料.2017(10)
流量可调燃气发生器压强控制仿真[J].余业辉，陈雄，郑健，刘慧莉，曾庆德，何坤.弹道学报.2017(03)
[58]双脉冲发动机点火过程三维数值模拟[J].严登超，陈雄，李映坤，朱亮，孙姗.固体火箭技术.2017(05)
全基因组关联研究中的遗传位点分析方法[J].卜庆伟，杨雨诗，葛方丽，陈雄.科学技术与工程.2017(17)
神经网络PI控制算法在燃气发生器上的应用[J].何坤，陈雄，余业辉，严登超.兵工自动化.2017(06)
锥阀设计对燃气发生器的控制性能影响[J].何坤，陈雄，余业辉，刘梦达.兵工自动化.2017(06)
旋流对固体燃料冲压发动机燃烧过程的影响[J].李唯暄，吕庆山，陈雄，巩伦昆，薛海峰.航空动力学报.2017(05)
HTPB推进剂的低温疲劳特性[J].童心，王永平，许进升，职世君，陈雄，郑亚.航空动力学报.2017(05)
火箭冲压发动机燃气发生器燃气流量控制设计[J].何坤，陈雄，余业辉，郑健.计算机仿真.2017(05)
环境氧含量和压力对铝镁贫氧推进剂燃烧性能的影响[J].相恒升，陈雄，周长省，赖华锦.含能材料.2017(03)
温度对HTPB推进剂疲劳特性的影响[J].梁蔚，吕庆山，陈雄，许进升，童心，闫晓晶.含能材料.2017(03)[2]
英文论文
Bionic optimization of MFCC features based on speaker fast recognition[J]. Lin Zhaodong，Di Changan，Chen Xiong. Applied Acoustics.
Numerical Investigation of Inlet Thermodynamic Conditions on Solid Fuel Ramjet Performances[J]. Li Weixuan，Zhao Dan，Chen Xiong，Zhu Liang，Ni Siliang，Ling William Yeong Liang. International Journal of Aerospace Engineering.
Experimental Research on Tensile Mechanical Properties of NEPE Propellant under Confining Pressure[J]. Li Hui，Wang ShiXin，Li Meng，Xu JinSheng，Fan XingGui，Chen Xiong. Propellants， Explosives， Pyrotechnics. 2020(11)
Fluid–structure coupled simulation of ignition transient in a dual pulse motor using overset grid method[J]. Li Yingkun，Chen Xiong，Cheng Honggang，Zhao Zemin. Acta Astronautica.
Microstructural simulations of debonding， nucleation， and crack propagation in an HMX-MDB propellant[J]. Hou Yufei，Xu Jinsheng，Zhou Changsheng，Chen Xiong. Materials & Design. 2021(prepublish)
Acoustic recognition method in low SNR based on human ear bionics[J]. Lin Zhaodong，Di Changan，Chen Xiong，Hou Yahui. Applied Acoustics.
Experimental Investigation and Modeling the Compressive Behavior of NEPE Propellant under Confining Pressure[J]. Li Hui，Xu Jinsheng，Chen Xiong，Hou Yufei，Fan Xinggui，Li Meng，Li Hongwen. Propellants， Explosives， Pyrotechnics. 2021(7)
Investigations on Internal Ballistic Characteristics of Pasty Propellant Rocket Engine[J]. Shan Xinyou，Li Yingkun，Chen Xiong，Wu Yan，He Yong，Li Weixuan，Concilio Antonio. International Journal of Aerospace Engineering.
Microstructural simulation of initial particle-matrix interfacial defect in HTPB solid propellants[J]. Hou Yufei，Xu Jinsheng，Zhou Changsheng，Chen Xiong. Journal of Physics: Conference Series. 2021(1)
Numerical investigations on solid-fueled ramjet inlet thermodynamic properties effects on generating self-sustained combustion instability[J]. Li Weixuan，Zhao Dan，Chen Xiong，Sun Yuze，Ni Siliang，Guan Di，Wang Bing. Aerospace Science and Technology.
Crack propagation velocity and fracture toughness of hydroxyl-terminated polybutadiene propellants: Experiments and simulations[J]. Wang Tingyu，Xu Jinsheng，Li Hui，Ding Wu，Liu Jiaming，Chen Xiong. Engineering Fracture Mechanics.
Dual Nozzle Weapon Power Couple Vibration Controller With Delayed Rear Nozzle[J]. Chen Xiong，Qiu Ming，Song Jie，Ma Longxu，Liao Zhenqiang. Journal of Physics: Conference Series. 2021(1)
Constitutive Model of N15 Propellant considering the Confining Pressure Effect[J]. Li Tianpeng，Han Junli，Wang Shixin，He Yong，Chen Xiong，Lu Bang，Xu Jinyang. International Journal of Aerospace Engineering.
Proper orthogonal and dynamic mode decomposition analyses of nonlinear combustion instabilities in a solid-fuel ramjet combustor[J]. Li Weixuan，Zhao Dan，Zhang Linqing，Chen Xiong. Thermal Science and Engineering Progress.
Experimental Investigation on Combustion Characteristics and Agglomeration of Al/NEPE Propellants[J]. Zhang Beichen，Xu Jinsheng，Feng Yaya，Zhang Anjie，Chen Xiong，Cai Wengxiang，Yingkun Li，Zhu Min. Propellants， Explosives， Pyrotechnics. 2021(1)
Numerical Analysis of Solid Fuel Regression Rate Distribution Characteristics in Solid-fuel Ramjet with Different Fuel Types[J]. Omer Musa，Chen Xiong，Liao Wenhe，Li Yingkun. IOP Conference Series: Materials Science and Engineering. 2019(1)
Combustion characteristics of a novel design of solid-fuel ramjet motor with swirl flow[J]. Omer Musa，Chen Xiong，Li Weixuan，Liao Wenhe. Aerospace Science and Technology.
Experimental investigation on the effect of swirling flow on combustion characteristics and performance of solid fuel ramjet[J]. Omer Musa，Li Weixuan，Chen Xiong，Gong Lunkun，Liao Wenhe. Acta Astronautica.
Investigations on the influence of swirl intensity on solid-fuel ramjet engine[J]. Omer Musa，Chen Xiong，Zhou Chang-sheng，Li Ying-kun，Liao Wen-He. Computers and Fluids.
Combustion characteristics and turbulence modeling of swirling reacting flow in solid fuel ramjet[J]. Omer Musa，Chen Xiong，Zhou Changsheng. Acta Astronautica.
Experimental and numerical investigation on the ignition and combustion stability in solid fuel ramjet with swirling flow[J].
Effect of inlet conditions on swirling turbulent reacting flows in a solid fuel ramjet engine[J]. Omer Musa，Chen Xiong，Zhou Changsheng，Weixuan Li. Applied Thermal Engineering.
Assessment of the modified rotation/curvature correction SST turbulence model for simulating swirling reacting unsteady flows in a solid-fuel ramjet engine[J]. Omer Musa，Chen Xiong，Zhou Changsheng，Gong Lunkun. Acta Astronautica.
Prediction of swirling cold flow in a solid-fuel ramjet engine with a modified rotation/curvature correction SST turbulence model[J]. Omer Musa，Zhou Changsheng，Chen Xiong，Gong Lunkun. Applied Thermal Engineering.
Effect of Anode Structure on the Plasma Jet Characteristics of Arcjet Thruster[J]. Du Zhenzhi，Chen Xiong，Li Yingkun，Zhou Changsheng. MATEC Web of Conferences.
A Couple Approach for a Conjugate Heat Transfer Investigation of the Shape-Change Effects in a Composite Nozzle[J]. Liu Rui，Chen Xiong，Zhou Chang-Sheng，Li Ying-Kun. Numerical Heat Transfer， Part A: Applications. 2015(11)
A Thermovisco-Hyperelastic Constitutive Model of NEPE Propellant Over a Large Range of Strain Rates[J]. Zhang Junfa，Zheng Jian，Chen Xiong，Sun Chaoxiang，Xu Jinsheng. Journal of Engineering Materials and Technology. 2014(3)
Numerical Simulation of Cold Swirl Field for Solid Fuel Ramjet with NACA Airfoil[J]. Yu Jie，Chen Xiong，Li Hong Wen. Applied Mechanics and Materials. 2014(716-717)
The Application of MATLAB in Computational Fluid Dynamic Visualization Processing[J]. Zheng Jian，Zhou Chang Sheng，Chen Xiong. Applied Mechanics and Materials. 2011(117-119)
Swirling effect on thermodynamic performance in a solid fueled ramjet with paraffin-polyethylene[J]. Li Weixuan，Chen Xiong，Zhao Dan，Wang Bin，Ma Kun，Cai Tao. Aerospace Science and Technology.[2]