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Knowledge Management System of Institue of Mechanics, CAS
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Source Publication:ACTA MECHANICA SINICA
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:229/34
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Submit date:2021/11/01
Cellular detonation
Lead shock evolution
Multi-layer perceptron
Numerical simulations
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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View/Download:398/63
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Submit date:2021/03/03
Hypersonics
Shock tunnels
Flow characteristics
Subgrid-scale model based on the vorticity gradient tensor for rotating turbulent flows
期刊论文
ACTA MECHANICA SINICA, 2020, 页码: 9
Authors:
Qi H(齐涵)
;
Li XL(李新亮)
;
Yu ZP(于长平)
Adobe PDF(2084Kb)
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View/Download:354/81
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Submit date:2020/07/06
Large-eddy simulation
Subgrid-scale model
Rotating turbulent channel flow
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:656/295
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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:306/90
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Submit date:2020/03/11
Wall heat flux
Numerical simulation
Ethylene
Supersonic combustor
Spectral measurements of hypervelocity flow in an expansion tunnel
期刊论文
ACTA MECHANICA SINICA, 2019, 卷号: 35, 期号: 1, 页码: 24-31
Authors:
Yuan CK(苑朝凯)
;
Zhou K(周凯)
;
Liu YF(刘云峰)
;
Hu ZM(胡宗民)
;
Jiang ZL(姜宗林)
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View/Download:346/102
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Submit date:2019/04/11
Spectral measurement
Hypervelocity flow
Radiation
Expansion tunnel
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:413/98
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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:339/86
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Submit date:2016/09/14
Dual-mode Scramjet
Engine Performance
Thrust
Optimization
Heat Release Distribution
Simulated Annealing Algorithm
Influences of affiliated components and train length on the train wind
期刊论文
ACTA MECHANICA SINICA, 2016, 卷号: 32, 期号: 2, 页码: 191-205
Authors:
Guo DL(郭迪龙)
;
Shang KM
;
Zhang Y
;
Yang GW(杨国伟)
;
Sun ZX(孙振旭)
;
Guo, DL
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View/Download:294/121
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Submit date:2017/09/04
Measurements of non-equilibrium and equilibrium temperature behind a strong shock wave in simulated martian atmosphere
期刊论文
ACTA MECHANICA SINICA, 2012, 卷号: 28, 期号: 5, 页码: 1296-1302
Authors:
Lin X
;
Yu XL(余西龙)
;
Li F(李飞)
;
Zhang SH(张少华)
;
Xin JG
;
Zhang XY(张新宇)
;
Yu, XL
;
Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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View/Download:809/246
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Submit date:2013/01/18
Radiation Measurements
Shock Wave
Mars Re-entry
Rotational Temperature
Vibrational Temperature
Radiation Measurements
Cn
Entry
Tube
Mixtures
Model