在航空動(dòng)力系統(tǒng)總體設(shè)計(jì)與優(yōu)化、智能設(shè)計(jì)理論與方法、發(fā)動(dòng)機(jī)健康管理算法開發(fā)與系統(tǒng)設(shè)計(jì)等領(lǐng)域開展了具有顯著學(xué)術(shù)及應(yīng)用價(jià)值的研究工作,主持30項(xiàng)研究課題,含2項(xiàng)國家自然基金,4項(xiàng)國家級重點(diǎn)/重大項(xiàng)目專題。在國內(nèi)外航空期刊及會(huì)議上發(fā)表中英文論文60篇;第一完成人獲得中國航空學(xué)會(huì)2014年度科學(xué)技術(shù)獎(jiǎng)二等獎(jiǎng);獲2017年北航青年教師教學(xué)基本功大賽一等獎(jiǎng),2017年北京市青年教師基本功大賽最佳教案獎(jiǎng), 2017年北京市青年教師基本功大賽三等獎(jiǎng);指導(dǎo)學(xué)生獲2017年美國AIAA本科生發(fā)動(dòng)機(jī)設(shè)計(jì)大賽冠軍。代表性研究成果發(fā)表于Aerospace Science and Technology,AIAA Journal,ASME J. Gas Turbines Power,Applied Energy,Applied Thermal Engineering等國際航空及能源學(xué)術(shù)期刊。 [1] Min Chen, Liangquan Hu, Hailong Tang. An Approach for Optimal Measurements Selection on Gas Turbine Engine Fault Diagnosis[J]. Journal of Engineering for Gas Turbines and Power-Transactions of the ASME, 2015, 137: 1-9. [2] Pengcheng Dong, Hailong Tang, Min Chen, Zhengping Zou. Overall performance design of paralleled heat release and compression system for hypersonic aeroengine[J]. Applied Energy, 2018, 220: 36-46. [3] Min Chen, Jiyuan Zhang, Hailong Tang, Interval Analysis of the Standard of Adaptive Cycle Engine Component Performance Deviation[J]. Aerospace Science and Technology, 2018, 81: 179-191. [4] Shanxuan Tang, Hailong Tang, Min Chen. Transfer-learning based gas path analysis method for gas turbines[J]. Applied Thermal Engineering, 2019, 155: 1-13. [5] Jiyuan Zhang, Pengcheng Dong, Hailong Tang, Junchao Zheng, Jingkai Wang, Min Chen. A General Design Method of Control Law for Adaptive Cycle Engine Mode Transition[J]. AIAA Journal, 2021, 1-15. (In press)