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Professor Supervisor of Doctorate Candidates Supervisor of Master's Candidates

Paper Publications

[31]Dechuan Sun, wangbo, XIA Guangqing.流动参数对固液发动机燃料退移速率的影响[J],固体火箭技术,2022,4:496-499,510
[32]Dechuan Sun, 张梦龙.波瓣型燃气/空气混合装置的设计与模拟[J],推进技术,2022,6:893-898
[33]Dechuan Sun, 向伟彬.温度和压力对煤油燃烧反应诱导时间的影响[J],航空兵器,2022,6:60-65
[34]Dechuan Sun, 冯强.单组元发动机催化床内工作过程仿真综述[A],2021
[35]Dechuan Sun, 罗天佑.超声波测量固体推进剂燃速的关键技术[A],2021
[36]孙得川, 姚天亮.硝酸羟胺基单组元液体火箭发动机起动过程的模拟[J],推进技术,2020,41(1):58-64
[37]Sun, Dechuan, Luo, Tianyou, Feng, Qiang, DC (reprint author), Dalian Univ Technol, Sch Aeronaut & Astronaut, Dalian 116024, Peoples R China., Sun, Key Lab Adv Technol Aerosp Vehicles, Liaoning.New Contour Design Method for Rocket Nozzle of Large Area Ratio[J],INTERNATIONAL JOURNAL OF AEROSPACE ENGINEERING,2019,2019
[38]Sun, De-chuan, Xiang, Wei-bin, DC (reprint author), Dalian Univ Technol, Sch Aeronaut & Astronaut, Dalian 116024, Liaoning, Peoples R China..Simplified numerical simulation model for hydroxyl ammonium nitrate-based monopropellant rocket...[J],AEROSPACE SCIENCE AND TECHNOLOGY,2019,95
[39]Sun, Dechuan, Yu, Zeyou.Numerical simulation of the start process of a han-based mono-propellant rocket thruster[A],2017,2:1244-1250
[40]孙得川, 向伟彬.温度和压力对煤油燃烧反应诱导时间的影响[J],航空兵器,2018,6:60-65

total61 4/7

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