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基本信息 The basic information
姓名: 刘佩进

学院: 航天学院


学历: 博士研究生毕业

学位: 工学博士


职称: 教授

职务: 副院长


学科: 航空宇航科学与技术





教育经历 Education Experience
1990~1994 西北工业大学航天学院，本科生
1994~1997 西北工业大学航天学院，硕士生
1997~2002 西北工业大学航天学院，博士生



教育教学 Education And Teaching
研究方向：
1. 火箭基组合推进（RBCC）
2. 火箭发动机燃烧不稳定：火箭发动机燃烧稳定性分析与抑制，推进剂燃烧响应，金属与含能材料燃烧
3. 激光燃烧诊断:数字全息，吸收光谱


讲授课程：
研究生：燃烧诊断学，燃烧不稳定理论
本科生：航天推进理论基础，领域导论



招生信息 Admission Information
招生航空宇航推进理论与工程，工程热物理的硕士与博士研究生，专业型硕士。



荣誉获奖 Awards Information
1.国家技术发明二等奖，第四获奖人，2011年
2.国防技术发明二等奖，第二获奖人，2016年



学术成果 Academic Achievements
教材与专著
1.刘佩进，唐金兰主编，航天推进理论基础（工信部“十二五”规划教材），西北工业大学出版社，2016.2
2.刘佩进，何国强等，固体火箭发动机燃烧不稳定及控制技术，西北工业大学出版社，2015.01
3.唐金兰，刘佩进主编，固体火箭发动机原理，国防工业出版社，2013.02
发表论文（Selected）
1.PeijinLiu,Muxin Wang(王牧昕),Wenjing Yang(杨文婧),Vikrant Gupta,Yu Guan(关昱),Larry K.B. Li,Modified computation of the nozzle damping coefficient in solidrocket motors,Acta Astronautica,143 (2018),391–397
2.Pei-jin Liu,Lin-linLiu*(刘林林),Guo-qiang He(何国强), Effect of solid oxidizers on the thermal oxidation and combustionperformance of amorphous boron,J Therm Anal Calorim, 2016,124:1587-1593
3.刘佩进，金秉宁，魏祥庚，杨文婧，刘鑫，纪晓婷,固体推进剂非线性压强耦合响应特性分析,推进技术，2016，37(9):1601-1608
4.金秉宁，刘佩进，徐冠宇，AP多粒度级配固体推进剂非稳态燃烧响应模型，含能材料，2020，28(4)：291-299（封面文章）
5.金秉宁，王志新，刘佩进*，徐庚，同轴数字全息用于铝燃烧颗粒的测量研究，推进技术，2019，40(6):1399-1408
6.金秉宁，刘佩进*，魏少娟，固体推进剂非线性压强耦合响应特性实验研究，含能材料，2019，27(4)：290-296
7.金秉宁，刘佩进*，HichemRezaiguia，魏少娟，徐冠宇,固体推进剂速度耦合响应函数测量实验方法研究,推进技术，2019，40(1):192-198
8.Wei He(何伟), Wen Ao,Pei-jin Liu*,Qi-Long Yan*,et. al.,Metastable energetic nanocomposites of MOF-activated aluminum featuredwith multi-level energy releases，Chemical Engineering Journal 381 (2020) 122623，ESI高被引
9.Lei Shi(石磊),Peijin Liu* , Fei Qin, et. al.,Research and development on inlets for rocket based combinedcycle engines, Progress in Aerospace Sciences 117 (2020) 100639
10. Bing-ning Jin(金秉宁), Zhi-xin Wang, Geng Xu, Wen Ao, Pei-jin Liu *a Three-dimensional spatial distributions of agglomerated particles on and near the burning surface of aluminized solid propellant using morphological digital in-line holography，Aerospace Science and Technology 106 (2020) 106066
11. Wei He, Jie-Yao Lyu, De-Yun Tang, Guo-Qiang He*, Pei-Jin Liu*, Qi-Long Yan*,Control the combustion behavior of solid propellants by using core-shell Al-based composites,Combustion and Flame 221 (2020) 441–452
12.Wen Ao*(敖文),Pei-jin Liu*, Huan Liu,et. al., Tuning the agglomeration and combustion characteristics of aluminizedpropellants via a new functionalized fluoropolymer, Chemical Engineering Journal 382 (2020) 122987
13.Guanyu Xu(徐冠宇),Peijin Liu*, Wen Ao, Bingning Jin,Interactions between turbulent flow and diffusion flame of compositepropellant in a solid rocket motor with sidewall mass injection, Aerospace Science and Technology 102 (2020) 105872
14.Zhuopu Wang(王琢璞),Peijin Liu*, Wen Ao,A reduced-order model of thermoacoustic instability in solid rocketmotors, Aerospace Science and Technology 97 (2020) 105615
15.Huan Liu(刘欢), Wen Ao*,Peijin Liu*,et. al., Effect of RDX content on the agglomeration, combustion and condensedcombustion products of an aluminized HTPB propellant, Acta Astronautica 170 (2020) 198–205
16.Yang Li(李阳), Zhuopu Wang*, and Peijin Liu,On the grid dependence of hydrodynamicstability analysis in solid rocket motors, Phys. Fluids 32, 034103 (2020)
17.De-Yun Tang（唐德云）, Jieyao Lyu, Wei He, Jin Chen, Guangcheng Yang,Peijin Liu*, Qi-Long Yan,Metastable intermixed Core-shell Al@M(IO3)x nanocomposites withimproved combustion efficiency by using tannic acid as a functionalinterfacial lay, Chemical Engineering Journal 384 (2020) 123369
18.Wei He , Bowen Tao , Zhijian Yang, Guangcheng Yang, Xiang Guo ,Pei-jin Liu*,Qi-Long Yan*,Mussel-inspired polydopamine-directed crystal growth of core-shell n-Al@PDA@CuO metastable intermixed composites，Chemical Engineering Journal 369 (2016) 1093-1101，ESI高被引
19. Guanyu Xu,Peijin Liu*, Wen Ao, Bingning JinTheoretical study of the flame describing function of AP/HTPB propellantflame based on sandwich model, Acta Astronautica 162 (2019) 207–215
20.Beilin Zuo(左蓓璘),Peijin Liu*,Qi-Long Yan*, et. al.,Fabrication of Si@AP/NC metastable intermixed nanocomposites(MICs) by electrospray method and their thermal reactivity, Advanced Composites and Hybrid Materials, 2019, https://doi.org/10.1007/s42114-019-00098-4
21.Wei He,Pei-jin Liu*, Qi-LongYan*, et. al., Tuning the Reactivity of MetastableIntermixed Compositen-Al/PTFE by Polydopamine Interfacial Control,ACS Appl. Mater. Interfaces,2018, 10, 38, 32849-32858
22.Qi-Long Yan(严启龙),Pei-Jin Liu*, Michael Gozin*,et. al.,Photosensitive but mechanically insensitivegrapheneoxide-carbohydrazide-metal hybrid crystalline energetic nanomaterials,Chemical Engineering Journal,338 (2018) 240–247
23.HichemRezaiguia,Peijin Liu*,Tianhao Yang,Flame response of solid propellant AP/Al/HTPB to a longitudinal acoustic wave,International Journal of Spray and Combustion Dynamics, 2017,9(4), 241-259
24.WenAo, Xin Liu(刘鑫), Hichem Rezaiguia, Huan Liu, Zhixin Wang,Peijin Liu*,Aluminum agglomeration involving the second mergence of agglomerates on the solid propellants burning surface: Experiments and modeling,Acta Astronautica 136 (2017) 219–229
大会报告
1.Combustion Instability in SRMs: Combustion Response and Triggering (Keynote speech)，International Symposium on Combustion Instabilities,北京，清华大学，2017年1月5日-9日
2.Combustion instability in SRM/LRE: Methods and Progress (Keynote speech),中国航天第三专业信息网第37届技术交流,，西安，2016年8月17-20日.
3.Fundamental Researches on Rocket-Based Combined-Cycle Propulsion Technology (Keynote speech), International Symposium on Innovation and Prospect of Liquid Propulsion Technology，西安，2016年9月4日-6日
4.Research Progress in Rocket Based Combined Cycle in China-an overview (Keynote speech on Space Propulsion Symposium), the 66^thInternational Astronautical Congress（IAC）,以色列，耶路撒冷，2015年11月12日-16日





社会兼职 Social Appointments
中国航空学会会员
陕西省工程热物理学会副理事长
《推进技术》期刊编委



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