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Indexed By:EI
Funding Organization:National Natural Science Foundation of China
Funding Project:National Natural Science Foundation of China[11532014]
Document Type:期刊论文
Community:高温气体动力学国家重点实验室
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Standing oblique detonation for hypersonic propulsion: A review
期刊论文
PROGRESS IN AEROSPACE SCIENCES, 2023, 卷号: 143, 页码: 17
Authors:
Jiang ZL(姜宗林)
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View/Download:55/7
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Submit date:2024/02/26
Standing oblique detonation
Scramjet engine
Oblique detonation engine
Shock wave
Supersonic combustion
Hypersonic ramjet propulsion
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:170/37
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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:244/57
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Submit date:2022/07/18
Chemical equilibrium
Detonation
Dissociated air
Shock relation
Theoretical solution
Numerical investigations of the lateral heat transfer in coaxial thermocouples
期刊论文
NUMERICAL HEAT TRANSFER PART A-APPLICATIONS, 2022, 页码: 19
Authors:
Qi L(齐力)
;
Han GL(韩桂来)
;
Hu ZM(胡宗民)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
Adobe PDF(3726Kb)
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View/Download:272/54
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Submit date:2022/07/18
Coaxial thermocouples
lateral heat transfer
maximum temperature point
numerical simulation
surface heat flux
Mechanisms of the destabilized Mach reflection of inviscid oblique detonation waves before an expansion corner
期刊论文
JOURNAL OF FLUID MECHANICS, 2022, 卷号: 940, 页码: 39
Authors:
Zhang, Zijian
;
Liu YF(刘云峰)
;
Wen, Chihyung
Adobe PDF(1777Kb)
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View/Download:162/39
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Submit date:2022/05/17
detonation waves
Numerical investigation on the generation mechanism of aero-heating of rudder shaft from three-dimensional flow separation and vortices
期刊论文
AIP ADVANCES, 2022, 卷号: 12, 期号: 4, 页码: 13
Authors:
Lin MY(林明月)
;
Yang F(杨帆)
;
Wang C(王春)
Adobe PDF(16512Kb)
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View/Download:180/27
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Submit date:2022/07/18
An experimental study of formation of stabilized oblique detonation waves in a combustor
期刊论文
COMBUSTION AND FLAME, 2022, 卷号: 237, 页码: 5
Authors:
Zhang ZJ(张子健)
;
Wen, Chihyung
;
Yuan CK(苑朝凯)
;
Liu YF(刘云峰)
;
Han GL(韩桂来)
;
Wang C(王春)
;
Jiang ZL(姜宗林)
Adobe PDF(865Kb)
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View/Download:329/47
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Submit date:2022/02/17
Numerical investigation of free oblique detonation wave induced by non-intrusive energy deposition
期刊论文
AIP ADVANCES, 2021, 卷号: 11, 期号: 12, 页码: 17
Authors:
Zhang WS(张文硕)
;
Zhang, Zijian
;
Jiang ZL(姜宗林)
;
Han X(韩信)
;
Liu, Yunfeng
;
Wang, Chun
Adobe PDF(15045Kb)
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View/Download:257/28
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Submit date:2022/01/24
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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Submit date:2022/01/12
Criteria for hypersonic airbreathing propulsion and its experimental verification
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2021, 卷号: 34, 期号: 3, 页码: 94-104
Authors:
Jiang ZL(姜宗林)
;
Zhang ZJ(张子健)
;
Liu YF(刘云峰)
;
Wang C(王春)
;
Luo ZT(罗长童)
Adobe PDF(1806Kb)
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View/Download:289/60
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Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test