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State Key ... [3]
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刘云峰 [3]
姜宗林 [3]
张子健 [2]
Wen CY [1]
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Creator:liuyunfeng分刘云峰
Creator:刘云峰
First author
Funding Organization:National Natural Science Foundation of China
Funding Project:National Natural Science Foundation of China[11532014]
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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:316/70
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Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
On theory and methods for advanced detonation-driven hypervelocity shock tunnels
期刊论文
NATIONAL SCIENCE REVIEW, 2020, 卷号: 7, 期号: 7, 页码: 1198-1207
Authors:
Jiang ZL(姜宗林)
;
Li JP(李进平)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Yu HR(俞鸿儒)
Adobe PDF(1090Kb)
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Submit date:2020/11/30
hypervelocity
shock tunnel
detonation driver
flight condition
tailored condition
test facilities
Application of CE/SE method to gas-particle two-phase detonations under an Eulerian-Lagrangian framework
期刊论文
JOURNAL OF COMPUTATIONAL PHYSICS, 2019, 卷号: 394, 页码: 18-40
Authors:
Zhang ZJ(张子健)
;
Wen CY
;
Liu YF(刘云峰)
;
Zhang DL(张德良)
;
Jiang ZL(姜宗林)
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View/Download:444/154
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Submit date:2019/09/09
Two-phase detonation
CE/SE
Eulerian-Lagrangian
MPI
Aluminum-air detonation