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Source Publication:ACTA MECHANICA SINICA
Language:英语
Community:高温气体动力学国家重点实验室
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Reconstructing shock front of unstable detonations based on multi-layer perceptron
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
Authors:
Zhou, Lin
;
Teng, Honghui
;
Ng, Hoi Dick
;
Yang PF(杨鹏飞)
;
Jiang ZL(姜宗林)
Adobe PDF(6382Kb)
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View/Download:238/36
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Submit date:2021/11/01
Cellular detonation
Lead shock evolution
Multi-layer perceptron
Numerical simulations
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)
Adobe PDF(3477Kb)
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View/Download:275/55
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Submit date:2021/03/30
Temperature-sensitive paint
Time-resolved measurement
Hypersonic flow
Background radiation
Experimental investigation of hypersonic flight-duplicated shock tunnel characteristics
期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 12
Authors:
Yuan CK(苑朝凯)
;
Jiang ZL(姜宗林)
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Submit date:2021/03/03
Hypersonics
Shock tunnels
Flow characteristics
Kerosene-fueled supersonic combustion modeling based on skeletal mechanisms
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 6, 页码: 1155-1177
Authors:
Yao W(姚卫)
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View/Download:664/298
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Submit date:2019/12/17
Kerosene
Supersonic combustion
Large eddy simulation
Skeletal mechanism
Scramjet
Numerical study of convective heat transfer of a supersonic combustor with varied inlet flow conditions
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 5, 页码: 943-953
Authors:
Fan WH(范文慧)
;
Zhong FQ(仲峰泉)
;
Ma SG(马素刚)
;
Zhang XY(张新宇)
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View/Download:314/93
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Submit date:2020/03/11
Wall heat flux
Numerical simulation
Ethylene
Supersonic combustor
An efficient unstructured WENO method for supersonic reactive flows
期刊论文
ACTA MECHANICA SINICA, 2018, 卷号: 34, 期号: 4, 页码: 623-631
Authors:
Zhao WG
;
Zheng HW(郑洪伟)
;
Liu FJ
;
Shi XT
;
Gao J
;
Hu N
;
Lv M
;
Chen SC
;
Zhao HD
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View/Download:422/99
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Submit date:2018/10/30
Supersonic reactive flows
Adaptive splitting scheme
Unstructured grids
WENO reconstruction
Engine performance analysis and optimization of a dual-mode scramjet with varied inlet conditions
期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 1, 页码: 75-82
Authors:
Tian L
;
Chen LH(陈立红)
;
Chen Q(陈强)
;
Zhong FQ(仲峰泉)
;
Zhang XY(张新宇)
;
Chen, LH (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:355/91
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Submit date:2016/09/14
Dual-mode Scramjet
Engine Performance
Thrust
Optimization
Heat Release Distribution
Simulated Annealing Algorithm
Development of efficient and accurate skeletal mechanisms for hydrocarbon fuels and kerosene surrogate
期刊论文
ACTA MECHANICA SINICA, 2015, 卷号: 31, 期号: 5, 页码: 732-740
Authors:
Zhong FQ(仲峰泉)
;
Ma SG
;
Zhang XY(张新宇)
;
Sung CJ
;
Niemeyer KE
;
Zhong, FQ (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:2016/01/08
Reduced Chemistry
Hydrocarbons
Directed Relation Graph
Ignition Delay Time
Characteristics of compressible flow of supercritical kerosene
期刊论文
ACTA MECHANICA SINICA, 2012, 卷号: 28, 期号: 1, 页码: 8-13
Authors:
Zhong FQ(仲峰泉)
;
Fan XJ(范学军)
;
Wang J(王晶)
;
Yu G(俞刚)
;
Li JG(李建国)
;
Fan, XJ
;
Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Submit date:2013/01/18
Supercritical Kerosene
Compressible Flow
Laval Nozzle
Isentropic Process
Aviation Kerosene
Combustion
Propulsion