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| 基于主动射流控制的高超声速进气道再起动性能研究（英文） 期刊论文
Transactions of Nanjing University of Aeronautics and Astronautics, 2022, 卷号: 39, 期号: 06, 页码: 651-662
Authors: 靳一超 ; 姚卫
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高超声速进气道 不起动 再起动 主动射流 流动控制 |
| 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) | Favorite | View/Download：297/71 | 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 |
| 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) | Favorite | View/Download：558/104 | 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 |
| Performance analysis of a strut-aided hypersonic scramjet by full-scale IDDES modeling 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 117, 页码: 14
Authors: Yao W(姚卫); Liu H(刘杭); Yue LJ(岳连捷); Xiao YB(肖雅彬)
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Hypersonic combustion Hydrogen Improved Delayed Detached Eddy Simulation (IDDES) Dynamic zone flamelet model Scramjet |
| Large eddy simulation of rest hypersonic combustor based on dynamic zone flamelet model 会议论文
AIAA Propulsion and Energy 2020 Forum, 24 August 2020 through 28 August 2020
Authors: Yao W(姚卫); Chen L(陈留)
Adobe PDF(2272Kb) | Favorite | View/Download：282/150 | Submit date：2021/06/11 |
| Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms 期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177
Authors: Yao W(姚卫)
Adobe PDF(9586Kb) | Favorite | View/Download：660/296 | Submit date：2019/12/17
Kerosene Supersonic combustion Large eddy simulation Skeletal mechanism Scramjet |
| Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 期刊论文
JOURNAL OF PROPULSION AND POWER, 2018, 卷号: 34, 期号: 3, 页码: 772-786
Authors: Yao W(姚卫); Yuan YM(袁越明); Li XP(李晓鹏); Wang J(王晶); Wu K(吴坤); Fan XJ(范学军)
Adobe PDF(807Kb) | Favorite | View/Download：360/114 | Submit date：2018/07/17 |
| Comparative Study of Elliptic and Round Scramjet Combustors Fueled by RP-3 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, PEOPLES R CHINA, MAR 06-09, 2017
Authors: Yao W(姚卫); Yuan YM(袁越明); Li XP(李晓鹏); Wang J(王晶); Wu K(吴坤); Fan XJ(范学军)
Adobe PDF(805Kb) | Favorite | View/Download：412/154 | Submit date：2018/06/06 |
| Development of zone flamelet model for scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017
Authors: Yao W(姚卫); Fan XJ(范学军)
Adobe PDF(623Kb) | Favorite | View/Download：273/94 | Submit date：2018/01/16
Combustion Cost Benefit Analysis Costs Mixtures Spacecraft Supersonic Aircraft |
| Development of zone flamelet modelfor scramjet combustor modeling 会议论文
21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017, Xiamen, China, March 6, 2017 - March 9, 2017
Authors: Yao W(姚卫); Fan XJ(范学军)
Adobe PDF(832Kb) | Favorite | View/Download：297/88 | Submit date：2018/11/08
Combustion Cost benefit analysis Costs Mixtures Ramjet engines Supersonic aircraft Computational costs Equivalence ratios Local flow conditions Scramjet combustors Statistics approaches Supersonic combustion Supersonic combustors Turbulent combustion |
