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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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岳连捷 [1]
张启帆 [1]
张新宇 [1]
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黄庭隆 [1]
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Creator：黄庭隆
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Date Issued：2019
Funding Project：National Natural Science Foundation of China[11472279]
Document Type：期刊论文
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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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Submit date：2020/03/21
Hysteresis
Dual-mode scramjet
Supersonic combustion
Mode transition
Flame stabilization
Combustion oscillation
