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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 [4]
胡宗民 [2]
韩桂来 [2]
俞鸿儒 [1]
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Indexed By:SCI
Funding Organization:National Natural Science Foundation of China
Funding Project:National Natural Science Foundation of China[11727901]
Author:姜宗林
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Analytic investigation on error of heat flux measurement and data processing for large curvature models in hypersonic shock tunnels
期刊论文
APPLIED MATHEMATICS LETTERS, 2022, 卷号: 134, 页码: 8
Authors:
Han GL(韩桂来)
;
Qi L(齐力)
;
Jiang ZL(姜宗林)
Adobe PDF(1715Kb)
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View/Download:293/49
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Submit date:2022/11/08
Heat flux
Measurement
Data processing
Error
Approximate solution
Simulation on Three-Dimensional Shock Interactions and Aerodynamic Heating Between Body and Wing
期刊论文
AIAA JOURNAL, 2021, 页码: 12
Authors:
Lin MY(林明月)
;
Wang C(王春)
;
Peng J(彭俊)
;
Jiang ZL(姜宗林)
Adobe PDF(4805Kb)
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View/Download:348/68
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Submit date:2022/01/12
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:357/178
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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)
Adobe PDF(1090Kb)
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View/Download:278/101
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Submit date:2020/11/30
hypervelocity
shock tunnel
detonation driver
flight condition
tailored condition
test facilities