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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 [92]
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Indexed By:SCI
Author:姜宗林
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Experimental demonstration of forced initiation of kerosene oblique detonation by an on-wedge trip in an ODE model
期刊论文
COMBUSTION AND FLAME, 2023, 卷号: 258, 页码: 6
Authors:
Han X(韩信)
;
Liu YF(刘云峰)
;
Zhang, Zijian
;
Zhang WS(张文硕)
;
Yuan CK(苑朝凯)
;
Han GL(韩桂来)
;
Jiang ZL(姜宗林)
Adobe PDF(1092Kb)
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View/Download:88/8
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Submit date:2023/11/28
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:64/13
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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
Characteristics of reattached oblique detonation induced by a double wedge
期刊论文
PHYSICS OF FLUIDS, 2023, 卷号: 35, 期号: 3, 页码: 36112
Authors:
Yao KP(姚克鹏)
;
Yang PF(杨鹏飞)
;
Li HY(李昊洋)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
Adobe PDF(2986Kb)
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View/Download:121/10
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Submit date:2023/04/20
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:411/78
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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
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:282/45
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Submit date:2022/11/08
Heat flux
Measurement
Data processing
Error
Approximate solution
Numerical Investigation of Aerodynamic Separation Schemes for Two-Stage-to-Orbit-like Two-body System
期刊论文
Aerospace Science and Technology, 2022, 卷号: 131, 期号: Part A, 页码: 107995
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(9707Kb)
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View/Download:326/95
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Submit date:2022/11/14
Two-stage to orbit
Numerical simulation
Stage separation
Hypersonic flow
Aerodynamic interference
Experimental Study of Longitudinal Stage Separation of Two-Body Configuration in Shock Tunnel
期刊论文
AIAA Journal, 2022, 卷号: 60, 期号: 12, 页码: 6940-6946
Authors:
Wang Y(王粤)
;
Wang YP(汪运鹏)
;
Jiang ZL(姜宗林)
Adobe PDF(2434Kb)
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View/Download:330/88
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Submit date:2022/08/23
Aerodynamic Coefficients
Two Stage to Orbit
Aerodynamic Performance
Hypersonic Flight
Hypersonic Wind Tunnels
Solenoid Valves
Oblique Shock
Pneumatic Actuator
Hypersonic Flows
Computer Aided Engineering
Divide and Conquer: A Quick Scheme for Symbolic Regression
期刊论文
INTERNATIONAL JOURNAL OF COMPUTATIONAL METHODS, 2022, 卷号: 19, 期号: 08, 页码: 25
Authors:
Luo ZT(罗长童)
;
Chen C(陈辰)
;
Jiang ZL(姜宗林)
Adobe PDF(204Kb)
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View/Download:176/39
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Submit date:2023/02/07
Symbolic regression
machine learning
divide and conquer
bi-correlation test
mathematical modeling
genetic programming
A theoretical method for solving shock relations coupled with chemical equilibrium and its applications
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 6, 页码: 47-62
Authors:
Zhang, Zijian
;
Wen, Chihyung
;
Zhang WS(张文硕)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(3178Kb)
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View/Download:247/58
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Submit date:2022/07/18
Chemical equilibrium
Detonation
Dissociated air
Shock relation
Theoretical solution
Oblique detonation wave triggered by a double wedge in hypersonic flow
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2022, 卷号: 35, 期号: 4, 页码: 176-184
Authors:
Teng, Honghui
;
Zhang, Yuhang
;
Yang PF(杨鹏飞)
;
Jiang ZL(姜宗林)
Adobe PDF(1747Kb)
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View/Download:193/39
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Submit date:2022/07/18
Double wedge
Hypersonic flow
Initiation structures
Oblique detonation
Shock interactions