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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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Investigation of Burst Pressure of Flat-Scored Metal Diaphragms in Hypersonic Impulse Facilities
期刊论文
AIAA JOURNAL, 2024, 页码: 8
Authors:
Wang WT(王文韬)
;
Wang Q(汪球)
;
Li JP(李进平)
;
Zhao W(赵伟)
;
Gao, Liangjie
;
Liu, Zhongchen
;
Qian, Zhansen
Favorite
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View/Download:63/0
  |  
Submit date:2024/02/26
Finite Element Method
Hypersonic
Shock Tube/Tunnel
Diaphragm
Burst Pressure
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:93/19
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Submit date:2024/01/15
Two-stage-to-orbit
Wind tunnel test
Numerical simulation
Stage separation
Hypersonic
Shock waves
Experimental demonstration of forced initiation of kerosene oblique detonation by an on-wedge trip in an ODE model
期刊论文
COMBUSTION AND FLAME, 2023, 卷号: 258, 页码: 6
Authors:
Han X(韩信)
;
Liu YF(刘云峰)
;
Zhang, Zijian
;
Zhang WS(张文硕)
;
Yuan CK(苑朝凯)
;
Han GL(韩桂来)
;
Jiang ZL(姜宗林)
Adobe PDF(1092Kb)
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View/Download:86/8
  |  
Submit date:2023/11/28
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:388/39
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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
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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View/Download:403/77
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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
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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View/Download:599/88
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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
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
Adobe PDF(1844Kb)
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View/Download:166/41
  |  
Submit date:2023/02/09
高超声速进气道
不起动
再起动
主动射流
流动控制
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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View/Download:323/94
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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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View/Download:326/87
  |  
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
Experimental study on the effects of the cone nose-tip bluntness
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 10, 页码: 7
Authors:
Liu MK(刘美宽)
;
Han GL(韩桂来)
;
Li, Zongxian
;
Jiang ZL(姜宗林)
Adobe PDF(2020Kb)
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View/Download:188/55
  |  
Submit date:2022/12/29