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Source Publication：CHINESE JOURNAL OF AERONAUTICS
Language：英语
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Investigation of dual ignition for a detonation-driven shock tunnel in forward driving mode
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 5, 页码: 1468-1475
Authors:
Wang Q(汪球)
;
Luo K(罗凯)
;
Li JW(栗继伟)
;
Li JP(李进平)
;
Zhao W(赵伟)
Adobe PDF(2057Kb)
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View/Download：266/83
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Submit date：2020/08/26
Shock tunnel
Detonation driver
Diaphragm
Dual ignition
High-enthalpy flow
Six sigma robust design optimization for thermal protection system of hypersonic vehicles based on successive response surface method
期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2019, 卷号: 32, 期号: 9, 页码: 2095-2108
Authors:
Zhu JJ
;
Wang XJ
;
Zhang HG
;
Li YW
;
Wang RX(王睿星)
;
Qiu ZP
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Adobe PDF(2082Kb)
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View/Download：439/192
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Submit date：2020/03/21
Hypersonic vehicle
Six sigma robust optimization
Successive response surface
Thermal protection system
Uncertainty
