Development of a structured overset Navier–Stokes solver with a moving grid and full multigrid method

2018 ◽  
Vol 24 (3) ◽  
pp. 884-901 ◽  
Author(s):  
Kunihide Ohashi ◽  
Takanori Hino ◽  
Hiroshi Kobayashi ◽  
Naoyuki Onodera ◽  
Nobuaki Sakamoto
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.


2017 ◽  
Author(s):  
Bruno Benato Rutyna ◽  
Marcio Augusto Villela Pinto ◽  
Réverton Luís Antunes Neundorf ◽  
Márcio Alexandro Maciel de Anunciação ◽  
Márcio André Martins

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