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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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State Key ... [2]
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岳连捷 [2]
张新宇 [2]
黄庭隆 [2]
张启帆 [1]
张旭 [1]
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2019 [2]
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Creator:岳连捷
First author
Creator:张新宇
Date Issued:2019
Language:英语
Funding Organization:National Natural Science Foundation of China
Funding Project:National Natural Science Foundation of China[11672309]
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Numerical investigation of mode transition and hysteresis in a cavity-based dual-mode scramjet combustor
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 94, 页码: 10
Authors:
Zhang X(张旭)
;
Yue LJ(岳连捷)
;
Huang TL(黄庭隆)
;
Zhang QF(张启帆)
;
Zhang XY(张新宇)
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Adobe PDF(3862Kb)
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View/Download:376/134
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Submit date:2020/03/21
Hysteresis
Dual-mode scramjet
Supersonic combustion
Mode transition
Flame stabilization
Combustion oscillation
Numerical study of a fully confined supersonic slot impinging jet from bleed system
期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2019, 卷号: 90, 页码: 12-22
Authors:
Huang TL(黄庭隆)
;
Yue LJ(岳连捷)
;
Chang XY(张新宇)
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Adobe PDF(3918Kb)
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View/Download:558/183
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Submit date:2019/09/09
Fully confined supersonic jet
Inclined impingement
Heat transfer
Boundary layer bleed
Numerical simulation