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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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Date Issued:2023
Community:高温气体动力学国家重点实验室
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Wall shear stress and wall heat flux in a supersonic turbulent boundary layer subjected to concave surface curvature
期刊论文
PHYSICAL REVIEW FLUIDS, 2023, 卷号: 8, 期号: 12, 页码: 29
Authors:
Tong FL(童福林)
;
Duan JY(段俊亦)
;
Ji XX(纪相鑫)
;
Dong, Siwei
;
Yuan, Xianxu
;
Li XL(李新亮)
Adobe PDF(7538Kb)
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View/Download:72/10
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Submit date:2024/01/22
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
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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View/Download:62/7
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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
基于 CO2 的飞行器降温减阻技术优化方法及特性
学位论文
硕士论文,北京: 中国科学院大学, 2023
Authors:
姚子康
Adobe PDF(7335Kb)
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View/Download:161/5
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Submit date:2023/07/10
飞行器热管理,仿生分形结构,优化,CO2 射流,降温减阻
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:431/82
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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