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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
访问量：
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[41]
Effects of interface diffusion and shock strength on shock-accelerated SF6cylinder,Physics of Fluids,2022,34.0(7.0)
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[42]
Yang, Haiwei , Yang, Tianyang. Simulation on rarefied hypersonic flows using direct simulation Monte Carlo method,Proceedings of the International Astronautical Congress, IAC,2019,
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[43]
基于水平集方法和最小距离函数法的复杂装药燃面退移问题研究,兵工学报,2017,38(02):280-291
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[44]
Effects of interface diffusion and shock strength on shock-accelerated SF6cylinder,Physics of Fluids,2022,34.0(7.0)
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[45]
The space-time CESE method applied to phase transition of water vapor in compressible flows,COMPUTERS & FLUIDS,2007,36(7):1247-1258
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[46]
可渗透壁自适应高度补偿喷管工作机理数值研究,推进技术,2023,45(07):53-66
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[47]
高阶WENO格式数值粘性对模拟R-T不稳定性的影响,哈尔滨工程大学学报,2011,32(12):1563-1568+1587
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[48]
Yang, ZA,Lu, MY,Guan, B,Yang,. Numerical investigations of corrugated tube and Fe3O4 nanoparticles on the mitigation effects of sup,International Journal of Heat and Mass Transfer,
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[49]
小离地高度下翼型气动特性计算模型的研究,哈尔滨工程大学学报,2008,29(11):1160-1165
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[50]
燃烧室Al2O3熔渣运动对飞行器章动过程的影响分析,固体火箭技术,2012,36(02):195-199
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[51]
Flow and mixing in shock-accelerated elliptic helium gas cylinder process,ACTA PHYSICA SINICA,2018,67(18):200-214
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[52]
Numerical study on altitude-compensating mechanism of a permeable nozzle,Journal of Physics: Conference Series,2024,2746(1)
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[53]
冷凝器开缝肋片换热特性场协同原理分析,哈尔滨工程大学学报,2008,29(06):568-572
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[54]
Numerical investigation on expansion-deflection nozzle flow during an ascending-descending trajector,PHYSICS OF FLUIDS,2023,35(8)
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[55]
基于水平集方法和最小距离函数法的复杂装药燃面退移问题研究,兵工学报,2017,38(02):280-291
-
[56]
Numerical Investigation on the Mechanism of Solid Rocket Motor Instability Induced by Differences be,AEROSPACE,2024,11(3)
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[57]
Numerical simulation of flow fields induced by a supersonic projectile moving in tubes,SHOCK WAVES,2012,22(5):417-425
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[58]
Numerical investigation on thrust efficiency dropping phenomenon of annular expansion-deflection noz,PHYSICS OF FLUIDS,2021,33(12)
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[59]
可渗透喷管动态工作特性数值研究,兵器装备工程学报,2024,45(8):161-167
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[60]
可渗透喷管壁面开孔角度对推力性能影响的数值研究,固体火箭技术,2024,47(02):199-207
