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姜宗林 [9]
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Force measurement using strain-gauge balance in shock tunnel based on deep learning
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2023, 卷号: 36, 期号: 8, 页码: 43-53
Authors:
Nie SJ(聂少军)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(2346Kb)
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View/Download:76/16
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Submit date:2024/02/26
Convolutional neural net-works
Deep learning
Frequency domain analysis
Force measurement
Time domain analysis
Recurrent neural networks
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:291/48
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Submit date:2022/11/08
Heat flux
Measurement
Data processing
Error
Approximate solution
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
Atomization of misaligned impinging liquid jets
期刊论文
PHYSICS OF FLUIDS, 2021, 卷号: 33, 期号: 9, 页码: 15
Authors:
Zhang, Chenwei
;
Zhang ZY(张振宇)
;
Wu K(吴坤)
;
Xia, Xi
;
Fan XJ(范学军)
Adobe PDF(15401Kb)
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Submit date:2022/01/12
AMP Exception
AMP Exception
Characterizing combustion of a hybrid rocket using laser absorption spectroscopy
期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2021, 卷号: 127, 页码: 9
Authors:
Fang SH(方思晗)
;
Wang ZZ(王泽众)
;
Lin X(林鑫)
;
Li F(李飞)
;
Li RJ(李仁杰)
;
Li, Jing
;
Zhang, Zhedian
;
Liu, Yan
;
Yu XL(余西龙)
Adobe PDF(4367Kb)
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Submit date:2021/08/03
Tunable diode laser absorption spectroscopy
Hybrid rocket motor
Temperature
Partial pressure
Combustion efficiency
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
Evolution of heat transfer at the stagnation point during the detached bow shock establishment
期刊论文
SHOCK WAVES, 2021, 页码: 8
Authors:
Wang Q(汪球)
;
Li JP(李进平)
;
Luo K(罗凯)
;
Li JW(栗继伟)
;
Zhao W(赵伟)
Adobe PDF(1158Kb)
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Submit date:2021/05/17
Hypersonic
Aerodynamic heating
Detached bow shock
Shock tube
expansion tube
Fast-response oxygen sensitive transparent coating for inner pressure ratiometric optical mapping
期刊论文
JOURNAL OF MATERIALS CHEMISTRY C, 2021, 卷号: 9, 期号: 11, 页码: 3919-3927
Authors:
Yang Di
;
Li JW(栗继伟)
;
Ren Junkai
;
Wang Qinglin
;
Zhou Shuyun
;
Wang Q(汪球)
;
Xie Zheng
;
Qu Xiaozhong
Adobe PDF(4555Kb)
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Submit date:2021/05/06
Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 12
Authors:
Yuan CK(苑朝凯)
;
Jiang ZL(姜宗林)
Adobe PDF(3790Kb)
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Submit date:2021/03/03
Hypersonics
Shock tunnels
Flow characteristics
Flow structure of pressure transmission tube and its influence on unsteady pressure measuring results in compressible flow
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2021, 卷号: 108, 页码: 22
Authors:
Tong XT(仝晓通)
;
Zhang QF(张启帆)
;
Yue LJ(岳连捷)
;
Zhang XY(张新宇)
Adobe PDF(8067Kb)
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Submit date:2021/03/03
Unsteady pressure measurement
Pressure sensor
Pressure transmission tube
Dynamic response
Compressible flow