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State Key... [14]
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刘云峰 [14]
姜宗林 [14]
胡宗民 [5]
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Creator:刘云峰
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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 YF(刘云峰)
;
Wang C(王春)
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Submit date:2022/01/24
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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Submit date:2021/05/17
Concept demonstration
Hypersonic propulsion
Oblique detonation engine
Scramjet
Shock wave
Supersonic combustion
Wind tunnel test
Noise reduction for temperature-sensitive paint measurement contaminated by strong background radiation in a high enthalpy hypersonic tunnel
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 7
Authors:
Peng, Di
;
Liu, Xu
;
Jiao, Lingrui
;
Li, Ziyan
;
Wen, Xin
;
Yuan CK(苑朝凯)
;
Han GL(韩桂来)
;
Liu YF(刘云峰)
;
Liu, Yingzheng
;
Jiang ZL(姜宗林)
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Submit date:2021/03/30
Temperature-sensitive paint
Time-resolved measurement
Hypersonic flow
Background radiation
Formation of stabilized oblique detonation waves in a combustor
期刊论文
COMBUSTION AND FLAME, 2021, 卷号: 223, 页码: 423-436
Authors:
Zhang ZJ(张子健)
;
Wen, Chihyung
;
Zhang WS(张文硕)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(3599Kb)
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Submit date:2021/03/03
Oblique detonation wave
Combustor
Oblique detonation engine
Normal detonation wave
Boundary layer separation
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
Experimental Investigation of Hypervelocity Flow in an Expansion Tunnel
期刊论文
AIAA JOURNAL, 2020, 卷号: 58, 期号: 6, 页码: 2776-2783
Authors:
Yuan CK(苑朝凯)
;
Zhou K(周凯)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
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Submit date:2020/07/06
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)
Adobe PDF(4374Kb)
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Submit date:2019/09/09
Two-phase detonation
CE/SE
Eulerian-Lagrangian
MPI
Aluminum-air detonation
Starting Process in a Large-Scale Shock Tunnel
期刊论文
AIAA Journal, 2016, 卷号: 54, 期号: 5, 页码: 1240-1249
Authors:
Wang YP(汪运鹏)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(764Kb)
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Submit date:2017/09/19
Starting Process in a Large-Scale Shock Tunnel
会议论文
22nd AIAA Computational Fluid Dynamics Conference, Dallas, TX, JUN 22-26, 2015
Authors:
Wang YP
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
;
Wang, YP (reprint author), Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R China.
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Submit date:2016/06/28
Numerical investigation of the starting process in a long-test-duration hypersonic shock tunnel
会议论文
22nd AIAA Computational Fluid Dynamics Conference, 2015, Dallas, TX, United states, June 22, 2015 - June 26, 2015
Authors:
Wang YP(汪运鹏)
;
Hu ZM(胡宗民)
;
Liu YF(刘云峰)
;
Jiang ZL(姜宗林)
Adobe PDF(5104Kb)
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Submit date:2017/05/05
Inviscid Flows
Numerical Investigations
Outlet Diameters
Reflected Shock Waves
Simulated Results
Starting Process
Transmitted Shock
Unsteady Nozzle Flow