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王革
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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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[1]
Study on Permeable Nozzle Optimization Using NSGA-II Algorithm,Advances in Astronautics,()
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[2]
On shock evolution and thrust variation of a rocket permeable nozzle in an ascent-descent operation,ACTA MECHANICA SINICA,42(3)
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[3]
Experimental Investigation on Porous Media Permeable Nozzle,Advances in Transdisciplinary Engineering,68():649-655
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[4]
On shock evolution and thrust variation of a rocket permeable nozzle in an ascent-descent operation,Acta Mech. Sin.,[J].2026,42
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[5]
Numerical study on the effects of drastic variations in thermal conductivity on the supercritical CO,INTERNATIONAL JOURNAL OF THERMAL SCIENCES,[J].2026,224
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[6]
Effects of helium injection on thrust performance of a solid-gas hybrid rocket motor under two-phase,AEROSPACE SCIENCE AND TECHNOLOGY,[J].2026,173
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[7]
Numerical investigation on a shock-accelerated heavy gas reactive concentric cylinder,PHYSICS OF FLUIDS,37(12)
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[8]
Numerical investigation on effect of helium on solid-gas hybrid rocket motor with AP/HTPB propellant,CHINESE JOURNAL OF AERONAUTICS,[J].2026,39(1)
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[9]
Effects of helium injection scheme on the thrust performance of solid-gas hybrid rocket motor,AEROSPACE SCIENCE AND TECHNOLOGY,[J].2025,168(E)
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[10]
Numerical study of interface dynamics and material transport on shock-accelerated heavy gas cylinder,PHYSICS OF FLUID,[J].2025,37(6)
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[11]
Experimental study on startup-shutdown process of a planar expansion deflection nozzle,CHINESE JOURNAL OF AERONAUTICS,[J].2025,38(7)
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[12]
Numerical investigation of annular expansion-deflection nozzle flow under varying backpressure chang,CHINESE JOURNAL OF AERONAUTICS,[J].2025,38(5)
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[13]
Specific impulse gain mechanism of swirling helium-injected solid-gas hybrid rocket motor,Physics of Fluids,[J].2025,37(0361132)
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[14]
Numerical investigation and convenient prediction of vortex behavior induced by shock interacting wi,JOURNAL OF AERONAUTICS ASTRONAUTICS AND AVIATION,[J].2025,57(6)
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[15]
王革. Numerical Investigation on the Factors Influencing Local Supersonic Ring in the Micronozzle,2nd Asian Aerospace and Astronautics Conference,[C].2024,
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[16]
Numerical investigation on the transient performance of solid–gas hybrid rocket motors during the s,Phys. Fluids,[J].2025,37(096146)
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[17]
Numerical investigation on the transient performance of solid-gas hybrid rocket motors during the st,PHYSICS OF FLUIDS,37(9)
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[18]
微孔注氦型固-气混合火箭发动机比冲增益机制,航空学报,46(16):77-87
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[19]
空调房间送风射流与回风气流相互作用的数值模拟,应用能源技术,2007,(07):31-33
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[20]
液滴与壁面碰撞模型研究,哈尔滨工程大学学报,2009,30(03):267-270
