氢能与航天推进技术学术团队是在国家能动领域的重大发展战略和技术布局指引下，围绕“氢能”和“航天推进技术”两个领域间的系统性和联合性所建立的新型学术团队。目前有教师3人，在读博士研究生3人，在读硕士研究生8人，由兴趣牵引的稳定自主科研本科生20人。孙作宇博士为团队氢能方向负责人，虞育松博士为团队航天项目负责人，刘建华高级工程师为团队工程技术顾问。

        氢能领域方面的研究主要包括但不限于：               

        氢能生产与储运：侧重于氢高压储运安全机制 

                氢燃料基础特性：侧重氢燃料火焰动力学特性

        氢能的工程应用：侧重于氢内燃机和燃料电池 

                氢能生态与经济：侧重于中国氢经济案例分析

        航天推进技术的研究主要包括但不限于：

                新概念航天推进技术：包含绿色无毒和无拖曳推进技术

                空间新型能源的利用：新型推进剂性能分析与利用技术

                微重力推进控制技术：包含卫星在轨虚拟仿真现实技术

为氢能和航天领域“培育后继力量”和“开展科研研究”是氢能与航天推进技术学术团队主要目标。在储备人才培养方面上取得了一定成果，近年来研究生就业去向如下：

2019级硕士研究生

        马东硕（男）：中国航天二院（北京）（毕业课题：氢能动力装置）

        任世勇（男）：中国航天二院（北京）（毕业课题：航天推进装置）

2018级硕士研究生（团队成立前）

        李    梁（男）：中国航天五院（北京）（毕业课题：大功率内燃机）

        王炜晴（女）：日   本   丰  田（广州）（毕业课题：乙醇的内燃机）

2017级硕士研究生（团队成立前）

        林伟迪（男）：美 国 康 明 斯（北京）（毕业课题：大功率内燃机）

近年来团队成员所主持的科研项目：

2021年新增

        “航天推进类”项目：动力学开闭环控制方式下的贮箱液体晃动联合仿真

        “航天推进类”项目：ADN基推进剂的微波点火与燃烧特性试验研究

2020年新增

“氢能技术类”项目：扩散点火理论下甲烷/氢气高压泄放自燃影响机制（国家自然科学基金）

“氢气技术类”项目：高压氢气自燃爆炸特性

“航天推进类”项目：微重力条件下的两相流运动仿真模块开发

“航天推进类”项目：液体晃动联合仿真接口模块开发

“航天推进类”项目：大姿态运动模式下的推进剂液体晃动机制研究

“航天推进类”项目：微型推力器多相反应流计算研究

“国防军工类”项目：超高压燃油雾化与油气快速混合机理的基础研究

“国防军工类”项目：受限空间内的燃烧加速技术研究

2019年新增

“氢能技术类”项目：气态掺氢混合燃料湍流火焰结构振荡特性的基础研究

“航天推进类”项目：液体晃动虚拟现实仿真模块

“航天推进类”项目：基于高温壁面环境的燃烧传热模型研究

“航天推进类”项目：空间站两相柜科学实验系统光学光测平台热设计

团队组建前（2015-2018年）

“氢能技术类”项目：不同湍流火焰模式下甲烷掺氢混合燃料预混火焰传播机制（国家自然科学基金）

“氢能技术类”项目：皱褶火焰模式氢气预混火焰传播过程影响机制（北京市自然科学基金）

“氢能技术类”项目：氢气富燃皱折湍流火焰基础燃烧特性的研究

“氢能技术类”项目：煤气化合成气湍流预混燃烧特性的基础研究

“航天推进类”项目：充液卫星联合数值仿真及晃动建模

“航天推进类”项目：辅助推进系统方案仿真分析

“航天推进类”项目：耦合NS/DSMC混合算法的无拖曳卫星冷气微推进系统闭环环境控制仿真研究

“航天推进类”项目：ADN基液体推进剂的雾化特性实验研究

“航天推进类”项目：ADN基液体推进剂催化机理研究及燃烧稳定性研究

“航天推进类”项目：***专项200N推力器催化分解仿真研究

“航天推进类”项目：双组元推力器喷注器雾化性能数值仿真分析

“航天推进类”项目：推进系统部件流动仿真及试验相似性研究

“航天推进类”项目：全尺度的无毒发动机仿真计算研究

国家自然科学基金：超高压燃油雾化及诱导激波引燃机理的基础研究

国家自然科学基金：超高压柴油射流雾化特性及前缘激波演变过程的实验研究

国家重点研发计划：面向主动安全的高速列车系统安全域分析理论方法研究

2021年

[01] Ma Y, Wang XR, Li T, Zhang J, Gao J, Sun ZY*. Hydrogen and ethanol: production, storage, and transportation. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY (2021) (SCI，IF=4.229).

[02] Wang XR, Ma Y, Gao J, Li T, Jiang GZ, Sun ZY*. Review on water management methods for proton exchange membrane fuel cells.  INTERNATIONAL JOURNAL OF HYDROGEN ENERGY (2021). 46: 12206-12229.  (SCI，IF=4.229).

[03] He D, Yu Y, Kuang Y, Wang C*. Model comparisons of flow and chemical kinetic mechanisms for methane-air combusiton for engineering applicaitons. APPLIED SCIENCES (2021) 11: No. 4107. (SCI, IF=2.679)

2020年

[01] Ma DS, Sun ZY*. The progress on the studies about NOx emission in PFI-H2ICE. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY (2020) 45: 10590-10591. (SCI，IF=4.229).

[02] Huang K, Sun ZY*, Tian YC, Wang KL. Turbulent combustion evolution of stoichiometric H2/CH4/air mixtures within a spherical space. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY  (2020). 45: 10613-10622. (SCI，IF=4.229). 

[03] Sun ZY*, Xu CS. Turbulent burning velocity of stoichiometric syngas flames with different hydrogen volumetric factions upon constant-volume method with multi-zone model. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY (2020) 45: 4969-4978. (SCI，IF=4.229).

[04] Sun ZY*. Laminar explosion properties of syngas. COMBUSTION SCIENCE AND TECHNOLOGY (2020) 192: 166-181. (SCI，IF=1.229).

[05]Yu YS*, Lin W, Li L, Zhang Z. Effects of hydrogen addition on the combusiton characteristics of diesel fuel jets under ultra-high injection pressures.  INTERNATIONAL JOURNAL OF HYDROGEN ENERGY (2020) 45: 10592-10601. (SCI，IF=4.229).

[06] Li L, Yu YS*, Lin W. Numerical investigation on the effects of load conditions and hydrogen-air ratio on the combusiton presscess of a HSDI engine. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY (2020) 45: 10602-10612. (SCI，IF=4.229).

[07] Zhang Z*, Wang F, Cai K, Yang S, Yu Y. Analysis and improvement of thermal conductive characteristics of bipropellant 25N thruster in pulse working mode |双组元25N推力器脉冲工作模式下的传热特性分析及改进. JOURNAL OF PROPULSION TECHNOLOGY/推进技术 (2020) 41: 92-100. (EI)

[08] Liu X*, Yu Y, Fu T, Zhang W, Gao C, Liu Y, Shen Y, Chen J, Wang M. Numerical simulation of effects of heat soak-back on micro-scale flwo through a capillary in ADN-based thruster|ADN基推力器热回浸对毛细管微尺度流动特性影响的数值模拟研究.  JOURNAL OF PROPULSION TECHNOLOGY/推进技术 (2020) 41: 101-108. (EI)

[09] Liu H, Wang C, Yu Y, Xu H*, Ma X. An experimental study on particle evolution in the exhaust gas of a direct injection SI engine. APPLIED ENERGY (2020) 260: NO. 114200. (SCI, IF=8.48)

[10] Wang XR, Zhang J, Wang G, Dai ML, Chen JX, Sun ZY*. A comprehensive review on the properties of nanofluid fuel and its additive effects to compression ignition engines. APPLIED SURFACE SCIENCE (2020). 504: No.144581. (SCI，IF=5.155) 

2019年

[01] Xie YL, Sun ZY*. Effect of external turbulence on centrally-ignited spherical unstable H2/CH4/air flames in the constant-volume combustion bomb. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY (2019). 44: 20452-20461 (SCI，IF=4.229).

[02] Wang WQ, Sun ZY*. Experimental studies on the explosive limits and minimum ignition energy of syngas: a comparative review. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY (2019). 44: 5640-5649. (SCI，IF=4.229).

[03] Sun ZY*. Experimental studies on the explosion indices in turbulent stoichiometric H2/CH4/air mixtures. INTERNATIONAL JOURNAL OF HYDROGEN ENERGY (2019). 44: 469-476. (SCI, IF=4.229; ESI@Jul.2019).

[04] Fu P, Hou L*, Ren Z,  Zhang Z, Mao X, Yu Y. A droplet/wall impact model and simulation of a bipropellant rocket engine. AEROSPACE SCIENCE AND TECHNOLOGY (2019) 88: 32-39. (SCI, IF=5.107)

[05] Wang X*, Li G, Chen J, Li H, Yu Y. Simulation study of filling and starting operation characteristics of nitrogen gas micro-propulsion system on a drag-free satellite |无拖曳卫星氮气微推进系统填充与开机工作特性的仿真研究. JOURNAL OF ASTRONAUTICS/宇航学报 (2019) 40: 1367-1374. (EI)

[06] Zhang Z*, Yu Y, Huo L, Fu P, Mao X, Wang F. Experimetnal study on mechanism of spray droplet interaction with coating wall and its influence | 喷雾液滴与涂层壁面作用的机理性试验及其影响研究.  JOURNAL OF PROPULSION TECHNOLOGY/推进技术 (2019) 40: 1560-1567. (EI)

[07]Yu Y*. Experimental study on effects of ethanol-diesel fuel blended on spray characteristics under ultra-high injection pressure up to 350 MPa. ENERGY (2019) 186: No. 115768. (SCI, IF=7.147)

团队组建前代表作（2015-2018年）

[01] Sun ZY*. Structure of turbulent rich hydrogen-air premixed flames. INTERNATIONAL JOURNAL OF ENERGY RESEARCH (2018). 42: 2845-2858. (SCI, IF=3.009).

[02] Sun ZY*. Explosion pressure measurement of 50%H2-50%CO synthesis gas-air mixtures in various turbulent ambience. COMBUSTION SCIENCE AND TECHNOLOGY (2018). 190: 1007-1022 (SCI, IF=1.229).

[03] Sun ZY*. Turbulent explosion characteristics of stoichiometric syngas. INTERNATIONAL JOURNAL OF ENERGY RESEARCH (2018) 42: 1225-1236. (SCI, IF=3.009；ESI@Nov.2018).

[04] Sun ZY*, Li GX. Turbulence influence on explosion characteristics of stoichiometric and rich hydrogen/air mixtures in a spherical closed vessel. ENERGY CONVERSION AND MANAGEMENT (2017) 149: 1526-1535. (SCI, IF=6.377).

[05] Li FS, Li GX, Sun ZY*. Explosion behaviour of 30% hydrogen/70% methane-blended fuels in a weak turbulent environment. ENERGIES (2017) 10: 915-930. (SCI, IF=2.676).

[06] Sun ZY*, Li GX. Propagation speed of wrinkled premixed flames within stoichiometric hydrogen-air mixtures under standard temperature and pressure. KOREAN JOURNAL OF CHEMICAL ENGINEERING (2017) 34: 1846-1857. (SCI, IF=2.007）

[07] Sun ZY*, Li GX. Propagation characteristics of laminar spherical flames within homogeneous hydrogen-air mixtures. ENERGY (2016) 116: 116-127. (SCI, IF=5.600；ESI@Jul.2018)

[08] Sun ZY*，Li GX. On reliability and flexibility of sustainable energy application route for vehicles in China. RENEWABLE & SUSTAINABLE ENERGY REVIEWS (2015) 51: 830-846. (SCI/SSCI, IF=8.050)

[09] Wang Y, Li G*, Yu Y, Ding J, Zhang T. Experimental study on effects of injection pressure on spray cone angle of coaxial swirl injector. JOURNAL OF PROPULSION TECHNOLOGY/推进技术 (2017) 38: 903-908. (EI)

[10] Chen J, Li G*, Zhang T, Wang M, Yu Y. Experimental investigaiton of thre catalytic decomposition and combustion characteristics of a non-toxic ammonium dinitramide (ADN)-based monopropellant thruster. ACTA ASTRONAUTICA (2016) 129: 367-373. (SCI, IF=2.413)

[11] Zhang T, Li G*, Chen J, Yu Y, Liu X. Effect of wall heat transfer characteristic on the micro solid thruster based on the AP/HTPB aerospace propellant. VACUUM (2016) 134: 9-19. (SCI, IF=3.627)

[12] Zhang T*, Li G, Chen J, Yu Y, Wei Y, Liu X, Zhou G.. Numerical simulation of combustion process of AP/HTPB solid micro thruster. JOURNAL OF SOLID ROCKET TECHNOLOGY/固体火箭技术 (2016) 39: 632-637. (EI)

[13] Zhang T, Li G*, Yu Y, Chen J, Wang M. Effect of catalytic bed thermal characteristics on liquid monopropellant decomposition and combustion characteristics within an eco-friendly thruster based on ammonium dinitramide. COMBUSTION SCIENCE AND TECHNOLOGY (2016) 188: 910-923.

[14] Zhang T, Li G*, Chen J, Yu Y, Wang M. Numerical simulation of comobustion process in non-toxic ADN-based aerospace thruster with considering thermal dispersion effect. CHINESE JOURNAL OF EXPLOSIVE AND PROPELLANTS/火炸药学报 (2016) 39: 98-101. 

[15] Yu Y, Li G*, Wang Y, Ding J. Modeling the atomization of high-pressure fuel spray by using a new breakup model. APPLIED MATHEMATICAL MODELLING (2016) 40: 268-283. (SCI, IF=5.129)

[16] Sun ZY, Li GX*, Wang L, Wang WH, Gao QX, Wang J. Effects of structure parameters on the static electromagnetic characteristics of solenoid valve for an electronic unit pump. ENERGY CONVERSION AND MANAGEMENT (2016) 113: 119-130. (SCI，IF=6.377)

[17] Sun ZY, Li GX*, Yu Y, Gao S, Gao G. Numerical investigation on transient flow and cavitation characteristic within nozzle during the oil drainage process for a high-pressure common-rail DI diesel engine. ENERGY CONVERSION AND MANAGEMENT (2015) 98: 507-517. (SCI，IF=6.377; ESI@Sept.2016)

[18] Sun ZY, Li GX*, Chen C, Yu Y, Gao G. Numerical investigation on effects of nozzle's geometric parameters on the flow and the cavitation characteristics within injector's nozzle for a high-pressure common-rail DI diesel engine. ENERGY CONVERSION AND MANAGEMENT (2015) 89: 843-861. (SCI, IF=6.377; ESI@Mar.2017)