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The dual information preserving method for stiff reacting flows 期刊论文
COMPUTERS & FLUIDS, 2017, 卷号: 157, 页码: 253-275
Authors:  Liu, Li;  Shen YQ(申义庆);  Liu, Shengping;  Yu, Ming;  Shen, YQ (reprint author), Chinese Acad Sci, Inst Mech, LHD, Beijing 100190, Peoples R China.
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Stiff Reacting Flow  Dual Information Preserving Method  Numerical Perturbation Method  Shock-capturing Scheme  
High-Pressure Capturing Wing Configurations 期刊论文
AIAA JOURNAL, 2017, 卷号: 55, 期号: 6, 页码: 1909-1919
Authors:  Cui K(崔凯);  Li GL;  Xiao Y(肖尧);  Xu YZ;  Cui,K(reprint author), Chinese Acad Sci, Inst Mech
View  |  Adobe PDF(671Kb)  |  Favorite  |  View/Download：648/183  |  Submit date：2017/07/24
A novel weighting switch function for uniformly high-order hybrid shock-capturing schemes 期刊论文
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2017, 卷号: 83, 期号: 9, 页码: 681-703
Authors:  Peng J(彭峻);  Shen YQ(申义庆);  Shen, YQ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Comparison of drag prediction using RANS models and DDES for the DLR-F6 configuration using high order schemes 会议论文
54th AIAA Aerospace Sciences Meeting, 2016, San Diego, CA, United states, January 4, 2016 - January 8, 2016
Authors:  Gan JY;  Shen YQ(申义庆);  Zha GC
View  |  Adobe PDF(555Kb)  |  Favorite  |  View/Download：298/96  |  Submit date：2017/05/05
Central Differencing  Drag Prediction  Finite Difference Scheme  High  Order Scheme  Line Relaxation  Mesh Refinement  Trailing Edges  Turbulent Models  
An improved unstructured WENO method for compressible multi-fluids flow 期刊论文
INTERNATIONAL JOURNAL FOR NUMERICAL METHODS IN FLUIDS, 2016, 卷号: 82, 期号: 3, 页码: 113-129
Authors:  Zheng HW(郑洪伟);  Zhao WG(赵文赓);  Zheng, HW (reprint author), Chinese Acad Sci, Inst Mech, 15 Beisihuanxi Rd, Beijing 100190, Peoples R China.
View  |  Adobe PDF(10441Kb)  |  Favorite  |  View/Download：370/104  |  Submit date：2016/12/08
Compressible Multi-fluid Flows  Weno  Finite Volume Method  High-order Accuracy  Unstructured Grids  
Development of a symplectic and phase error reducing perturbation finite-difference advection scheme 期刊论文
NUMERICAL HEAT TRANSFER PART B-FUNDAMENTALS, 2016, 卷号: 70, 期号: 2, 页码: 136-151
Authors:  Yu CH;  Gao Z(高智);  Sheu TWH;  Sheu, TWH (reprint author), Natl Taiwan Univ, Dept Engn Sci & Ocean Engn, 1,Sec 4,Roosevelt Rd, Taipei 106, Taiwan.
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Resolution-optimised nonlinear scheme for secondary derivatives 期刊论文
INTERNATIONAL JOURNAL OF COMPUTATIONAL FLUID DYNAMICS, 2016, 卷号: 30, 期号: 2, 页码: 107-119
Authors:  Li L(李理);  Yu ZP(于长平);  Chen Z(陈哲);  Li XL(李新亮);  Li, XL (reprint author), Chinese Acad Sci, Inst Mech, Beijing, Peoples R China.
View  |  Adobe PDF(1358Kb)  |  Favorite  |  View/Download：425/87  |  Submit date：2016/11/08
Spectral-like Schemes  Secondary Derivatives  Viscous Terms  Nonlinear Optimisation  Nonlinear Weight  
Improvement of weighted compact scheme with multi-step strategy for supersonic compressible flow 期刊论文
COMPUTERS & FLUIDS, 2015, 卷号: 115, 页码: 2841-2849
Authors:  Peng J(彭峻);  Shen YQ(申义庆);  Shen, YQ (reprint author), Chinese Acad Sci, Inst Mech, State Key Lab High Temp Gas Dynam, Beijing 100190, Peoples R China.
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Numerical Method  Supersonic Compressible Flow  Weighted Compact Scheme  Multi-step Strategy  
Coupling Analysis for the Thermo-Acoustic-Vibration Response of a Thin-Walled Box 会议论文
10th International Conference on Vibration Engineering and Technology of Machinery, Manchester ENGLAND, SEP 09-11 2014
Authors:  Yang Y(杨焱);  Wu CW(吴臣武);  yangyan@imech.ac.cn
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Thermal  Vibration  Acoustic  Multi-physics Environment  
A conceptual design of next generation hypersonic air-breathing airplanes with dual waveriders forebody 会议论文
20th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2015, Glasgow, United kingdom, July 6, 2015 - July 9, 2015
Authors:  Cui K(崔凯);  Hu SC(胡守超);  Li GL;  Xiao Y(肖尧);  Situ M
View  |  Adobe PDF(872Kb)  |  Favorite  |  View/Download：371/160  |  Submit date：2017/05/05
Aero  Dynamic Performance  Aerodynamic Performance Predictions  Design Methodology  Flight Altitudes  Numerical Results  Propulsion System  Turbulent Models  Wing Body Aircraft