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Experimental and numerical investigation on the unsteady interaction in longitudinal stage separation for parallel-staged two-body configuration
期刊论文
Physics of Fluids, 2024, 卷号: 36, 页码: 016116
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(7258Kb)
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View/Download:96/19
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Submit date:2024/01/15
Two-stage-to-orbit
Wind tunnel test
Numerical simulation
Stage separation
Hypersonic
Shock waves
High-fidelity state-to-state modeling of hypersonic flow over a double cone
期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 11, 页码: 10
Authors:
Wang XY(王小永)
;
Guo, Jinghui
;
Hong QZ(洪启臻)
;
Li, Sijia
Adobe PDF(3376Kb)
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Submit date:2023/12/18
Characteristics of cellular structure of detonation waves propagating in annular channels
期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 10, 页码: 13
Authors:
Yao KP(姚克鹏)
;
Yang PF(杨鹏飞)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
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Submit date:2024/02/19
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
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
Numerical study on wave configuration of wedge-induced oblique detonation wave: Reactive boundary layer effect
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 11, 页码: 11
Authors:
Yang L(杨理)
;
Yue LJ(岳连捷)
;
Yu, Dehai
;
Chen, Zheng
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Submit date:2022/12/29
A theoretical method for solving shock relations coupled with chemical equilibrium and its applications
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 6, 页码: 47-62
Authors:
Zhang, Zijian
;
Wen, Chihyung
;
Zhang WS(张文硕)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
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Submit date:2022/07/18
Chemical equilibrium
Detonation
Dissociated air
Shock relation
Theoretical solution
高马赫数燃烧强化的激波风洞试验研究
期刊论文
力学学报, 2022, 卷号: 54, 期号: 05, 页码: 1403-1413
Authors:
张旭
;
张启帆
;
岳连捷
;
孟东东
;
罗苇航
;
于江鹏
;
张晓源
;
李进平
;
陈宏
;
李飞
Adobe PDF(3069Kb)
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Submit date:2022/08/11
高马赫数
超声速燃烧
燃烧强化
小支板
JF-24激波风洞
Mechanisms of the destabilized Mach reflection of inviscid oblique detonation waves before an expansion corner
期刊论文
JOURNAL OF FLUID MECHANICS, 2022, 卷号: 940, 页码: 39
Authors:
Zhang, Zijian
;
Liu YF(刘云峰)
;
Wen, Chihyung
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Submit date:2022/05/17
detonation waves
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:560/104
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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