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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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Method of applying temperature-sensitive paint in hypersonic test with strong combustion radiation
期刊论文
ACTA MECHANICA SINICA, 2023, 卷号: 39, 期号: 8, 页码: 322474./通讯作者:Peng, D (corresponding author), Shanghai Jiao Tong Univ, Gas Turbine Res Inst, Sch Mech Engn, Shanghai 200240, Peoples R China.
Authors:
Yuan CK(苑朝凯)
;
Meng FZ(孟凡钊)
;
Liu, Xu
;
Liu YF(刘云峰)
;
Lian H(连欢)
;
Liu, Yingzheng
;
Peng, Di
Adobe PDF(3477Kb)
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Submit date:2023/07/17
Temperature-sensitive paint
Heat flux
Conjugate gradient method
Air-breathing hypersonic vehicle
Inverse heat conduction problem
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./通讯作者:Wang YP(汪运鹏)(1,2)
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:754/148
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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
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./通讯作者:HU, Zongmin
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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Submit date:2021/03/30
High-enthalpy flow
Hypersonic wind tunnel
Aerospace vehicle
Aerodynamic balance
Heat flux sensor
Optical measurement technique
Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108./通讯作者:Wang, Xiaojun
Authors:
Zhu JJ
;
Wang XJ
;
Zhang HG
;
Li YW
;
Wang RX(王睿星)
;
Qiu ZP
View
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Adobe PDF(2082Kb)
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View/Download:571/240
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Submit date:2020/03/21
Hypersonic vehicle
Six sigma robust optimization
Successive response surface
Thermal protection system
Uncertainty
基于实验设计方法的高超声速飞机前缘型线优化分析
期刊论文
力学学报, 2016, 卷号: 48, 期号: 2, 页码: 290-299
Authors:
胡守超
;
崔凯
;
李广利
;
肖尧
;
司徒明
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View/Download:655/218
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Submit date:2016/12/16
Hypersonic Airplane
Air-breathing Vehicle
Shape Optimization
Parameterization
Uniform Design
Aerothermal optimization of hypersonic vehicle leading edge based on genetic algorithm
会议论文
23rd International Congress of Theoretical and Applied Mechanics, 中国北京/Beijing, China, 2012-08-19
Authors:
Cui K(崔凯)
;
Hu SC(胡守超)
;
Gao TY(高太元)
;
Wang XP(王秀平)
;
Yang GW(杨国伟)
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View/Download:723/194
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Submit date:2014/04/02
Vehicle
Leading
0algorithm
Genetic
Hypersonic
Optimization
Aerothermal
Based
Method
Design
Attack
Novel
Around
Angle
Evaluated
Greatly
About
Fluid
Result
Differ
Experimental Demonstration Of A New Concept Of Drag Reduction And Thermal Protection For Hypersonic Vehicles
期刊论文
Acta Mechanica Sinica, 2009, 卷号: 25, 期号: 3, 页码: 417-419
Authors:
Jiang ZL(姜宗林)
;
Liu YF(刘云峰)
;
Han GL(韩桂来)
;
Zhao W(赵威)
;
Jiang ZL
Adobe PDF(226Kb)
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View/Download:984/243
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Submit date:2009/08/03
Hypersonic Vehicle
Shock-reconstruction
Drag Reduction
Thermal Protection
Spike And Lateral Jets
Research Progress On Thermal Protection Materials And Structures Of Hypersonic Vehicles
期刊论文
Applied Mathematics and Mechanics (English Edition), 2008, 页码: 51-60
Authors:
Yang YZ(杨亚政)
;
Yang JL
;
Fang DN
;
Yang, YZ (reprint author), Beijing Univ Aeronaut & Astronaut, Sch Aeronaut Sci & Technol, Beijing 100083, Peoples R China.
Adobe PDF(601Kb)
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View/Download:1027/414
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Submit date:2009/08/03
Hypersonic Vehicle
High-temperature
Thermal Protection
High-temperature Ceramics
Carbon/carbon Composites
Oxidation Behavior
Creep-behavior
Carbon
Microstructure
Diboride
Kinetics