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会议论文 [11]
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2017 [11]
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发表日期:2017
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IAEA's coordinated research project on EBR-II Shutdown heat removal tests
会议论文
作者:
Batra, Chirayu
;
Kriventsev, Vladimir
;
Monti, Stefano
;
Briggs, L.
;
Su, G.
收藏
  |  
浏览/下载:4/0
  |  
提交时间:2019/11/26
Argonne National Laboratory
Coordinated research projects
EBR-II
Heat removal
Initial and boundary conditions
International atomic energy agency
Passive safety
Reactor thermal hydraulics
Nonlinear dynamics of sloshing in tank based on Hamilton Principle
会议论文
Tingting Zhang
;
Jianying Yang
收藏
  |  
浏览/下载:5/0
  |  
提交时间:2017/12/03
Sloshing
Hamilton Principle
Jourdain variation
FEM
Sloshing
Hamilton Principle
Jourdain variation
FEM
Development of zone flamelet model for scramjet combustor modeling
会议论文
Xiamen, China, 6-9 March 2017
作者:
Yao W(姚卫)
;
Fan XJ(范学军)
收藏
  |  
浏览/下载:16/0
  |  
提交时间:2018/01/16
Combustion
Cost Benefit Analysis
Costs
Mixtures
Spacecraft
Supersonic Aircraft
Development of zone flamelet modelfor scramjet combustor modeling
会议论文
Xiamen, China, March 6, 2017 - March 9, 2017
作者:
Yao W(姚卫)
;
Fan XJ(范学军)
收藏
  |  
浏览/下载:30/0
  |  
提交时间:2018/11/08
Combustion
Cost benefit analysis
Costs
Mixtures
Ramjet engines
Supersonic aircraft
Computational costs
Equivalence ratios
Local flow conditions
Scramjet combustors
Statistics approaches
Supersonic combustion
Supersonic combustors
Turbulent combustion
Preliminary study on determination of reasonable ratio of spacing to diameter of double tunnels under earthquake
会议论文
Zhuhai, PEOPLES R CHINA, MAR 11-12, 2017
作者:
Zhou Yongqiang
;
Sheng Qian
;
Leng Xianlun
;
Fu Xiaodong
;
Li Nana
收藏
  |  
浏览/下载:19/0
  |  
提交时间:2018/06/05
earthquake
reasonable ratio of spacing to diameter
double tunnels
relative displacement
plastic zone
Application of Free Interface Modal Synthesis Method on Modal Test Boundary Transformation of One Missile Wing
会议论文
Phuket, THAILAND, 2017-08-06
作者:
Feng, Song
;
He, Yun
;
Wen, Yan
;
Feng, S (reprint author), XiAn Inst Opt & Precis Mech, Xian, Shaanxi, Peoples R China.
收藏
  |  
浏览/下载:16/0
  |  
提交时间:2018/04/03
Test Boundary Transformation
Modal Synthesis
Missile Wing
Modal Parameters
Direct numerical simulation of supersonic turbulent boundary layer subjected to a curved compression ramp
会议论文
Llanwddyn, WALES, 2017
作者:
Tong FL(童福林)
;
Li XL(李新亮)
;
Duan, Yanhui
;
Yu ZP(于长平)
;
Yu, CP (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
收藏
  |  
浏览/下载:20/0
  |  
提交时间:2018/01/16
Concave Surface Curvature
Adverse Pressure-gradient
Large-eddy Simulation
Reynolds-number
Near-wall
Flows
Separation
Vortices
Models
Influencing factors and scaling law of bubble detachment at a submerged orifice
会议论文
Phoenix, AZ, NOV 11-17, 2016
作者:
Wang YW(王一伟)
;
Huang CG(黄晨光)
;
Wu XC(吴小翠)
;
Wang, YW (reprint author), Chinese Acad Sci, Key Lab Mech Fluid Solid Coupling Syst, Inst Mech, Beijing, Peoples R China.
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  |  
浏览/下载:12/0
  |  
提交时间:2018/01/16
Constant-flow Conditions
Layer Drag Reduction
Simulation
Liquid
Recent channel adjustments in the Jingjiang Reach controlled by various boundary conditions
会议论文
作者:
Xia, J.Q.
;
Zhou, M.R.
;
Deng, S.S.
;
Lu, J.Y.
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  |  
浏览/下载:2/0
  |  
提交时间:2019/12/05
Spectral and pseudospectral schemes for the distributed order time fractional reaction-diffusion equation with Neumann boundary conditions
会议论文
2017 29TH CHINESE CONTROL AND DECISION CONFERENCE (CCDC), 2017-01-01
作者:
Liu, Haiyu
;
Lu, Shujuan
;
Chen, Wenping
收藏
  |  
浏览/下载:2/0
  |  
提交时间:2019/12/30
distributed order diffusion equation
Neumann boundary conditions
GLLB pseudospectral method
stability and convergence
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