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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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姜宗林 [6]
汪运鹏 [3]
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Indexed By:SCI
Date Issued:2022
Community:高温气体动力学国家重点实验室
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Effect of interaction strength on recovery downstream of incident shock interactions
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 12, 页码: 27
Authors:
Tong FL(童福林)
;
Lai, Jiang
;
Duan JY(段俊亦)
;
Dong, Siwei
;
Yuan, Xianxu
;
Li XL(李新亮)
Adobe PDF(9700Kb)
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View/Download:171/35
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Submit date:2023/02/07
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:334/97
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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:332/90
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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
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)
Adobe PDF(3178Kb)
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Submit date:2022/07/18
Chemical equilibrium
Detonation
Dissociated air
Shock relation
Theoretical solution
Wall heat flux in a supersonic shock wave/turbulent boundary layer interaction
期刊论文
PHYSICS OF FLUIDS, 2022, 卷号: 34, 期号: 6, 页码: 16
Authors:
Tong FL(童福林)
;
Yuan, Xianxu
;
Lai, Jiang
;
Duan JY(段俊亦)
;
Sun, Dong
;
Dong, Siwei
Adobe PDF(6246Kb)
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Submit date:2022/07/18
Three-dimensional flow structures and heat transfer characteristics of compressible flow over a cylindrical cavity
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 122, 页码: 12
Authors:
Wang JT(王江涛)
;
Ma T(马特)
;
Wang Z(王哲)
;
Wang RX(王睿星)
;
Song HW(宋宏伟)
;
Yuan W(袁武)
;
Zheng HW(郑洪伟)
Adobe PDF(4247Kb)
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Submit date:2022/06/10
Cylindrical cavity
Heat transfer
Compressible flow
3D flow behaviors
A numerical study of oblique detonation re-stabilization by expansion waves
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2022, 卷号: 122, 页码: 8
Authors:
Yao KP(姚克鹏)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
Adobe PDF(1789Kb)
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Submit date:2022/06/10
Oblique detonation
Stationary
Thermal choking
Expansion waves
An experimental study of formation of stabilized oblique detonation waves in a combustor
期刊论文
COMBUSTION AND FLAME, 2022, 卷号: 237, 页码: 5
Authors:
Zhang ZJ(张子健)
;
Wen, Chihyung
;
Yuan CK(苑朝凯)
;
Liu YF(刘云峰)
;
Han GL(韩桂来)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
Adobe PDF(865Kb)
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Submit date:2022/02/17
Theories and methods for designing hypersonic high-enthalpy flow nozzles
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 1, 页码: 318-339
Authors:
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
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Submit date:2022/06/10
Boundary layer correction
High-enthalpy flow
Hypersonic wind tunnel
Nozzle design
Real-gas effects