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中国科学院力学研究所机构知识库
Knowledge Management System of Institue of Mechanics, CAS
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姚卫 [5]
岳连捷 [2]
张政 [2]
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Creator:姚卫
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Date Issued:2022
Community:高温气体动力学国家重点实验室
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Effect of helical fins on the combustion performance in a micro-step combustor
期刊论文
FUEL, 2022, 卷号: 319, 页码: 13
Authors:
Zhang Z(张政)
;
Shen WBY
;
Yao W(姚卫)
;
Wang Q(汪球)
;
Zhao W(赵伟)
Adobe PDF(11881Kb)
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View/Download:270/38
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Submit date:2022/05/17
Micro-combustion
Helical fin
Combustion performance
Conjugate heat transfer
Mixing
基于动态分区概念的高超声速燃烧大涡模拟
期刊论文
力学学报, 2022, 卷号: 54, 期号: 04, 页码: 954-974
Authors:
姚卫
;
刘杭
;
张政
;
肖雅彬
;
岳连捷
Adobe PDF(1875Kb)
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View/Download:290/68
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Submit date:2022/06/10
高超声速燃烧
动态分区火焰面
分区自适应化学
分区并行自适应建表
改进延迟分离涡模拟
Improved delayed detached eddy simulation of supersonic combustion fueled by liquid kerosene
期刊论文
FUEL, 2022, 卷号: 313, 页码: 13
Authors:
Shen, Wubingyi
;
Huang, Yue
;
Yao W(姚卫)
;
Liu, Hedong
;
You, Yancheng
Adobe PDF(9915Kb)
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View/Download:177/41
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Submit date:2022/05/17
Improved delayed detached eddy simulation
Liquid kerosene
Skeletal reaction mechanism
Equivalence ratio
Cavity-based scramjet combustor
Supersonic combustion
高马赫数超燃冲压发动机技术研究进展
期刊论文
力学学报, 2022, 卷号: 54, 期号: 02, 页码: 263-288
Authors:
岳连捷
;
张旭
;
张启帆
;
陈科挺
;
李进平
;
陈昊
;
姚卫
;
仲峰泉
;
李飞
;
王春
;
陈宏
Adobe PDF(2622Kb)
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View/Download:557/103
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Submit date:2022/03/16
高马赫数
超燃冲压发动机
热化学非平衡
超声速燃烧
低雷诺数流动
激波风洞
飞行试验
Nonequilibrium Effects in Hypersonic Combustion Modeling
期刊论文
JOURNAL OF PROPULSION AND POWER, 2022, 页码: 18
Authors:
Yao W(姚卫)
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Submit date:2022/03/05