For solving partial differential equations (or distributed dynamic systems), the method of lines (MOL) and the space-time conservation element and solution element (CE/SE) method are compared in terms of computational efficiency, solution accuracy and stability. Several representative examples including convection-diffusion-reaction PDEs are numerically solved using the two methods on the same spatial grid. Even though the CE/SE method uses a simple stencil structure and is developed on a simple mathematical basis (i.e., Gauss' divergence theorem), accurate and computationally-efficient solutions are obtained in a stable manner in most cases. However, a remedy is still needed for PDEs with a stiff source term. It seems to be out of date to use the MOL for solving PDEs containing steep moving fronts because of the dissipation error caused by spatial discretization and time consuming computations. It is concluded that the CE/SE method is adequate to capturing shocks in PDEs but for diffusion-dominated stiff PDEs, the MOL with an ODE time integrator is complementary to the CE/SE method.
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Hong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R ChinaHong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China
Shen, Hua
Wen, Chih-Yung
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Hong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R ChinaHong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China
Wen, Chih-Yung
Zhang, De-Liang
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Chinese Acad Sci, Inst Mech, LHD, Beijing 100080, Peoples R ChinaHong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China
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Hong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R ChinaHong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China
Jiang, Yazhong
Wen, Chih-Yung
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Hong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China
Hong Kong Polytech Univ, Interdisciplinary Div Aeronaut & Aviat Engn, Kowloon, Hong Kong, Peoples R ChinaHong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China
Wen, Chih-Yung
Zhang, Deliang
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Chinese Acad Sci, State Key Lab High Temp Gas Dynam, Inst Mech, Beijing 100190, Peoples R ChinaHong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China
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NASA, John H Glenn Res Ctr Lewis Field, Turbomachinery & Prop Syst Div, Cleveland, OH 44135 USANASA, John H Glenn Res Ctr Lewis Field, Turbomachinery & Prop Syst Div, Cleveland, OH 44135 USA
Loh, CY
Hultgren, LS
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NASA, John H Glenn Res Ctr Lewis Field, Turbomachinery & Prop Syst Div, Cleveland, OH 44135 USANASA, John H Glenn Res Ctr Lewis Field, Turbomachinery & Prop Syst Div, Cleveland, OH 44135 USA
Hultgren, LS
Chang, SC
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NASA, John H Glenn Res Ctr Lewis Field, Turbomachinery & Prop Syst Div, Cleveland, OH 44135 USANASA, John H Glenn Res Ctr Lewis Field, Turbomachinery & Prop Syst Div, Cleveland, OH 44135 USA
机构:
Hong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R ChinaHong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China
Shen, Hua
Wen, Chih-Yung
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Hong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R ChinaHong Kong Polytech Univ, Dept Mech Engn, Kowloon, Hong Kong, Peoples R China