A Full Multigrid Method Applied to Turbulent Flow using the SIMPLEC Algorithm Together with a Collocated Arrangement

1994 ◽  
pp. 245-256 ◽  
Author(s):  
Peter Johansson ◽  
Lars Davidson
2006 ◽  
Vol 13 (2-3) ◽  
pp. 275-291 ◽  
Author(s):  
M. Mehl ◽  
T. Weinzierl ◽  
Chr. Zenger

1994 ◽  
Vol 116 (3) ◽  
pp. 435-445 ◽  
Author(s):  
A. Arnone

A three-dimensional code for rotating blade-row flow analysis has been developed. The space discretization uses a cell-centered scheme with eigenvalue scaling for the artificial dissipation. The computational efficiency of a four-stage Runge–Kutta scheme is enhanced by using variable coefficients, implicit residual smoothing, and a full-multigrid method. An application is presented for the NASA rotor 67 transonic fan. Due to the blade stagger and twist, a zonal, nonperiodic H-type grid is used to minimize the mesh skewness. The calculation is validated by comparing it with experiments in the range from the maximum flow rate to a near-stall condition. A detailed study of the flow structure near peak efficiency and near stall is presented by means of pressure distribution and particle traces inside boundary layers.


2016 ◽  
Vol 59 (10) ◽  
pp. 2037-2048 ◽  
Author(s):  
ShangHui Jia ◽  
HeHu Xie ◽  
ManTing Xie ◽  
Fei Xu

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