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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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Direct numerical simulation of impinging shock wave and turbulent boundary layer interaction over a wavy-wall
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 5, 页码: 350-363
Authors:
Tong FL(童福林)
;
Sun D(孙栋)
;
Li XL(李新亮)
Adobe PDF(4402Kb)
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Submit date:2021/06/07
Direct numerical simulation
Low-frequency unsteadiness
Shock waves
Turbulent boundary layer
Wavy-wall
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:351/177
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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
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)
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Submit date:2020/11/30
hypervelocity
shock tunnel
detonation driver
flight condition
tailored condition
test facilities
PIMOL: A New Semi-analytical Method Based on the Finite Difference Method of Lines and the Precise Integration Method
期刊论文
ACTA MECHANICA SOLIDA SINICA, 2020, 卷号: 33, 期号: 3, 页码: 381-391
Authors:
Xu YJ(徐永君)
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View/Download:253/61
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Submit date:2020/03/21
PIMOL
ODE
FDMOL
PIM
Poisson's equation
Semi-analytical
Semi-discrete
Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475
Authors:
Wang Q(汪球)
;
Luo K(罗凯)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
Adobe PDF(2057Kb)
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Submit date:2020/08/26
Shock tunnel
Detonation driver
Diaphragm
Dual ignition
High-enthalpy flow
PIMOL: The Finite Difference Method of Lines Based on the Precise Integration Method for an Arbitrary Irregular Domain
期刊论文
ACTA MECHANICA SOLIDA SINICA, 2020, 页码: 13
Authors:
Xu YJ(徐永君)
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View/Download:220/48
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Submit date:2020/05/18
PIMOL
ODEs
FDMOL
PIM
Poisson's equation problems
Semi-analytical (discrete)
Irregular domain
Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177
Authors:
Yao W(姚卫)
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View/Download:663/297
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Submit date:2019/12/17
Kerosene
Supersonic combustion
Large eddy simulation
Skeletal mechanism
Scramjet
Dynamic deformation behavior of a face-centered cubic FeCoNiCrMn high-entropy alloy
期刊论文
Science Bulletin, 2018, 卷号: 63, 期号: 6, 页码: 362-368
Authors:
He JY
;
Wang Q
;
Zhang HS(张虎生)
;
Dai LH(戴兰宏)
;
Mukai T
;
Wu Y
;
Liu XJ
;
Wang H
;
Nieh TG
;
Lu ZP
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Adobe PDF(3368Kb)
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Submit date:2018/10/24
High-entropy Alloys
Dynamic Deformation
Deformation Twinning
Work-hardening
Plastic Stability
Numerical studies of static aeroelastic effects on grid fin aerodynamic performances
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2017, 卷号: 30, 期号: 4, 页码: 1300-1314
Authors:
Huang CD(黄程德)
;
Liu W(刘文)
;
Yang GW(杨国伟)
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Adobe PDF(4021Kb)
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View/Download:342/100
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Submit date:2017/11/29
Aeroelasticity
Fluid-structure Interpolation
Grid Fin
Mesh Deformation
Radial Basis Function
Shock relations in gases of heterogeneous thermodynamic properties
期刊论文
SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2017, 卷号: 60, 期号: 7, 页码: 1050-1057
Authors:
Hu ZM(胡宗民)
;
Zhou K(周凯)
;
Peng J(彭俊)
;
Li JP(李进平)
;
Jiang ZL(姜宗林)
;
Li, JP (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Submit date:2017/10/25
Shock Wave
Imperfect Gas
Heterogeneous
Theoretical Solution