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Document Type:期刊论文
Community:高温气体动力学国家重点实验室
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Influence of non-thermal plasma and electric field on non-premixed methane flame
期刊论文
THERMAL SCIENCE AND ENGINEERING PROGRESS, 2024, 卷号: 47, 页码: 15
Authors:
Zhang YF(张玉锋)
;
Li T(李腾)
;
Wei XL(魏小林)
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Submit date:2024/03/11
Non -thermal plasma
Coaxial micro -tube burner
Methane flame
Combustion stability
激波风洞两级入轨飞行器纵向级间分离试验技术
期刊论文
航空学报, 2023, 卷号: 44, 期号: 17, 页码: 128126
Authors:
王粤
;
汪运鹏
;
姜宗林
Adobe PDF(6797Kb)
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View/Download:401/40
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Submit date:2022/12/01
两级入轨
轨迹捕获
激波风洞
多体分离
动态试验
试验技术
机体尾缘形状对高压捕获翼构型亚声速特性影响
期刊论文
航空学报, 2023, 卷号: 44, 期号: 06, 页码: 10.7527/S1000-6893.2022.27215
Authors:
王浩祥
;
肖尧
;
张凯凯
;
李广利
;
常思源
;
田中伟
;
崔凯
Adobe PDF(2111Kb)
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Submit date:2022/10/17
高压捕获翼
亚声速
流动特性
流动分离
数值模拟
一种并联两级入轨飞行器纵向分离方案的数值研究
期刊论文
航空学报, 2023, 卷号: 44, 期号: 11, 页码: 127634
Authors:
王粤
;
汪运鹏
;
王春
;
姜宗林
Adobe PDF(4901Kb)
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Submit date:2022/07/11
两级入轨
高超声速
纵向分离
气动干扰
非定常流动
Numerical Investigation on Longitudinal Stage Separation of Spiked Two-Stage-to-Orbit Vehicle
期刊论文
Journal of Spacecraft and Rockets, 2023, 卷号: 60, 期号: 1, 页码: 215-229
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
Adobe PDF(5479Kb)
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Submit date:2022/08/24
Multistage Launch Vehicle
Aerodynamic Characteristics
Shock Wave Interaction
Angle of Attack
Waverider
Boundary Layer Flow
Total Variation Diminishing
Adverse Pressure Gradient
Hypersonic Flows
Hypersonic Wind Tunnels
Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System
期刊论文
Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(9707Kb)
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Submit date:2022/11/14
Two-stage to orbit
Numerical simulation
Stage separation
Hypersonic flow
Aerodynamic interference
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel
期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(2434Kb)
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Submit date:2022/08/23
Aerodynamic Coefficients
Two Stage to Orbit
Aerodynamic Performance
Hypersonic Flight
Hypersonic Wind Tunnels
Solenoid Valves
Oblique Shock
Pneumatic Actuator
Hypersonic Flows
Computer Aided Engineering
Gas-surface interactions in a large-scale inductively coupled plasma wind tunnel investigated by emission/absorption spectroscopy
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 8, 页码: 14
Authors:
Fang SH(方思晗)
;
Lin X(林鑫)
;
Zeng, Hui
;
Zhu, Xingying
;
Zhou, Fa
;
Yang JN(杨俊娜)
;
Li F(李飞)
;
Ou, Dongbin
;
Yu XL(余西龙)
Adobe PDF(5914Kb)
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Submit date:2022/09/16
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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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
风洞模拟等离子体绕流场回波频谱调制特性实验研究
期刊论文
物理学报, 2022, 卷号: 71, 期号: 03, 页码: 221-227
Authors:
满良
;
邓浩川
;
吴洋
;
余西龙
;
肖志河
Adobe PDF(2239Kb)
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Submit date:2022/03/16
等离子体绕流场
频谱调制
一维距离像
风洞