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Knowledge Management System of Institue of Mechanics, CAS
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姜宗林 [6]
岳连捷 [4]
刘云峰 [3]
李进平 [3]
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Funding Organization:National Natural Science Foundation of China
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Computational study of lateral jet interaction in hypersonic thermochemical non-equilibrium flows using nonlinear coupled constitutive relations
期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 11, 页码: 14
Authors:
Zeng, Shuhua
;
Yang, Junyuan
;
Zhao, Wenwen
;
Huang YF(黄依峰)
;
Jiang, Zhongzheng
;
Chen, Weifang
Adobe PDF(3990Kb)
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View/Download:101/13
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Submit date:2024/01/22
Parameters for evaluating the efficiency of inlet compression
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 12, 页码: 51-56
Authors:
Chen KT(陈科挺)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(511Kb)
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Submit date:2022/01/12
Airbreathing engine
Compression efficiency
Compression quality
Inlet
Self-consistency
Vibrational Energy Transfer in CO+N-2 Collisions: A Database for V-V and V-T/R Quantum-Classical Rate Coefficients
期刊论文
MOLECULES, 2021, 卷号: 26, 期号: 23, 页码: 27
Authors:
Hong QZ(洪启臻)
;
Bartolomei, Massimiliano
;
Coletti, Cecilia
;
Lombardi, Andrea
;
Sun QH(孙泉华)
;
Pirani, Fernando
Adobe PDF(735Kb)
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Submit date:2022/03/05
vibrational energy transfer
inelastic scattering
potential energy surface
rate coefficients database
quantum-classical nuclear dynamics
quasi-classical trajectories
Hysteresis of Shock Train Movement in the Isolator with a Ramp
期刊论文
AIAA JOURNAL, 2021, 卷号: 59, 期号: 10, 页码: 3873-3882
Authors:
Huang TL(黄庭隆)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang P
;
Zhao QJ
Adobe PDF(2961Kb)
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Submit date:2022/02/17
Optical diagnostics in a detonation-driven direct-connected circular combustor fueled with hydrogen for mach 10 scramjet
期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2021, 卷号: 46, 期号: 54, 页码: 27801-27815
Authors:
Zhou GX(周功喜)
;
Zhang X(张旭)
;
Li JP(李进平)
;
Zhang XY(张晓源)
;
Zhang SZ(张仕忠)
;
Lin X(林鑫)
;
Li F(李飞)
;
Chen H(陈宏)
;
Yue LJ(岳连捷)
;
Yu XL(余西龙)
Adobe PDF(4108Kb)
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Submit date:2021/09/07
High mach number scramjet
Circular cross-section
TDLAS
Multi-view simultaneous imaging
POD
Fluid-structure interaction-based aerodynamic modeling for flight dynamics simulation of parafoil system
期刊论文
NONLINEAR DYNAMICS, 2021, 页码: 22
Authors:
Zhu, Hong
;
Sun, Qinglin
;
Liu, Xuefeng
;
Liu, Jinglei
;
Sun, Hao
;
Wu WN(邬婉楠)
;
Tan, Panlong
;
Chen, Zengqiang
Adobe PDF(4213Kb)
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Submit date:2021/08/03
Fluid-structure interaction
Parafoil system
Flexible deformation
Trailing edge deflection
Aerodynamic performance
Dynamic model
Criteria for hypersonic airbreathing propulsion and its experimental verification
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:
Jiang ZL(姜宗林)
;
Zhang ZJ(张子健)
;
Liu YF(刘云峰)
;
Wang C(王春)
;
Luo ZT(罗长童)
Adobe PDF(1806Kb)
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Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
Authors:
Jiang ZL(姜宗林)
;
Hu ZM(胡宗民)
;
Wang YP(汪运鹏)
;
Han GL(韩桂来)
Adobe PDF(1129Kb)
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View/Download:354/177
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Submit date:2021/03/30
High-enthalpy flow
Hypersonic wind tunnel
Aerospace vehicle
Aerodynamic balance
Heat flux sensor
Optical measurement technique
Impulse force-measurement system
期刊论文
SHOCK WAVES, 2020, 页码: 11
Authors:
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(1551Kb)
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Submit date:2020/11/30
Shock tunnel
High enthalpy
Aerodynamic force measurement
Strain gauge balance
On theory and methods for advanced detonation-driven hypervelocity shock tunnels
期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors:
Jiang ZL(姜宗林)
;
Li JP(李进平)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Yu HR(俞鸿儒)
Adobe PDF(1090Kb)
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View/Download:276/101
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Submit date:2020/11/30
hypervelocity
shock tunnel
detonation driver
flight condition
tailored condition
test facilities