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    王革

    • 教授      博士生导师      硕士生导师
    • 教师英文名称:Wang Ge
    • 教师拼音名称:WG
    • 所在单位:航空航天学院
    • 性别:男
    • 学位:工学博士学位
    • 在职信息:在职
    • 学科:流体力学. 航空宇航科学与技术
    • 学科:流体力学
      航空宇航科学与技术

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    论文成果

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    • [81] Numerical investigations of corrugated tube and Fe3O4 nanoparticles on the mitigation effects of sup,International Journal of Heat and Mass Transfer,
    • [82] Numerical investigations of corrugated tube and Fe3O4 nanoparticles on the mitigation effects of sup,International Journal of Heat and Mass Transfer,
    • [83] 基于混合正交法的环喉式膨胀偏流喷管性能影响因素研究,固态火箭技术,2023,
    • [84] Numerical Investigation on Thrust Characteristics of an Annular Expansion-Deflection Nozzle,Physics of Fluids,2023,
    • [85] Numerical Investigation on Expansion-Deflection Nozzle Flow During an Ascending-Descending Trajector,Physics of Fluids,2023,
    • [86] 基于混合正交法的环喉式膨胀偏流喷管性能影响因素研究,固态火箭技术,2023,
    • [87] Wang G, Chen L, Guan B, et.al. Numerical Investigation on Thrust Characteristics of an Annular Expansion-Deflection Nozzle,Physics of Fluids,2023,
    • [88] Numerical Study on a Throttling Segregated Fuel-Oxidizer System using Quasi-One-Dimensional Internal,Acta Mech. Sin.,2023,
    • [89] 固体火箭发动机约束方式对内流场与结构共振影响数值研究,固态火箭技术,2023,
    • [90] 固体火箭发动机约束方式对内流场与结构共振影响数值研究,固态火箭技术,2023,
    • [91] Wang Ge,Zhang Kexin,Zhou Boche. 基于混合正交法的环喉式膨胀偏流喷管性能影响因素研究,固体火箭技术,2023,3:410-418
    • [92] Wang Ge,zhou Bocheng,Guan Ben*. Numerical Investigation on Expansion-Deflection Nozzle Flow During an Ascending-Descending Trajector,Physics of Fluids,2023,
    • [93] Wang limin ,Wang Fuqi,Wang zhi. Numerical Study on a Throttling Segregated Fuel-Oxidizer System using Quasi-One-Dimensional Internal,Acta Mech. Sin.,2023,
    • [94] Yang, Haiwei , Liu, Xue , Bian. Numerical Investigation on the Mechanism of Transpiration Cooling for Porous Struts Based on Local T,Energies,2022,6
    • [95] Yang H, Liu X, Bian Y, Wang G. Numerical Investigation on the Mechanism of Transpiration Cooling for Porous Struts Based on Local T,Energies,2022,
    • [96] 气动热载荷作用下固体火箭发动机热流固耦合振动研究,第六届空天动力联合会议暨中国航天第三专业信息网第四十二届技术交流会暨2021航空发动机技术发展高层论坛论文集(第二册),2022,:297-305
    • [97] 环喉式膨胀偏流喷管结构参数研究,第六届空天动力联合会议暨中国航天第三专业信息网第四十二届技术交流会暨2021航空发动机技术发展高层论坛论文集(第二册),2022,:327-334
    • [98] Numerical Investigation on the Mechanism of Transpiration Cooling for Porous Struts Based on Local T,Energies,2022,6
    • [99] Effects of interface diffusion and shock strength on shock-accelerated SF6 cylinder,Physics of Fluids,2022,
    • [100] Numerical study on the effects of supercritical CO2-based nanofluid on heat transfer deterioration,NUMERICAL HEAT TRANSFER PART A-APPLICATIONS,2022,5:193-216
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