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机构地区:[1]College of Mathematics and Computational Science,Xiangtan University [2]Hunan Key Laboratory for Computation and Simulation in Science and Engineering,Xiangtan University
出 处:《Journal of Central South University》2008年第S1期181-186,共6页中南大学学报(英文版)
基 金:Projects(59375211,10771178,10676031) supported by the National Natural Science Foundation of China;Project(07A068) supported by the Key Project of Hunan Education Commission;Project(2005CB321702) supported by the National Key Basic Research Program of China
摘 要:The internal turbulent flow in conical diffuser is a very complicated adverse pressure gradient flow.DLR k-ε turbulence model was adopted to study it.The every terms of the Laplace operator in DLR k-ε turbulence model and pressure Poisson equation were discretized by upwind difference scheme.A new full implicit difference scheme of 5-point was constructed by using finite volume method and finite difference method.A large sparse matrix with five diagonals was formed and was stored by three arrays of one dimension in a compressed mode.General iterative methods do not work wel1 with large sparse matrix.With algebraic multigrid method(AMG),linear algebraic system of equations was solved and the precision was set at 10-6.The computation results were compared with the experimental results.The results show that the computation results have a good agreement with the experiment data.The precision of computational results and numerical simulation efficiency are greatly improved.The internal turbulent flow in conical diffuser is a very complicated adverse pressure gradient flow.DLR k-ε turbulence model was adopted to study it.The every terms of the Laplace operator in DLR k-ε turbulence model and pressure Poisson equation were discretized by upwind difference scheme.A new full implicit difference scheme of 5-point was constructed by using finite volume method and finite difference method.A large sparse matrix with five diagonals was formed and was stored by three arrays of one dimension in a compressed mode.General iterative methods do not work wel1 with large sparse matrix.With algebraic multigrid method(AMG),linear algebraic system of equations was solved and the precision was set at 10-6.The computation results were compared with the experimental results.The results show that the computation results have a good agreement with the experiment data.The precision of computational results and numerical simulation efficiency are greatly improved.
关 键 词:conical DIFFUSER turbulent flow DLR k-ε turbulence model 5-point scheme ALGEBRAIC MULTIGRID method(AMG)
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