Practical aspects of p-multigrid discontinuous Galerkin solver for steady and unsteady RANS simulations

2015 ◽  
Vol 78 (11) ◽  
pp. 670-690 ◽  
Author(s):  
Zhenhua Jiang ◽  
Chao Yan ◽  
Jian Yu ◽  
Wu Yuan
2020 ◽  
Vol 170 ◽  
pp. 103345
Author(s):  
G. Guiza ◽  
A. Larcher ◽  
A. Goetz ◽  
L. Billon ◽  
P. Meliga ◽  
...  

2016 ◽  
Vol 123 ◽  
pp. 131-145 ◽  
Author(s):  
Tahsin Tezdogan ◽  
Atilla Incecik ◽  
Osman Turan

Author(s):  
Christoph Gmelin ◽  
Mathias Steger ◽  
Erik Wassen ◽  
Frank Thiele ◽  
Andre Huppertz ◽  
...  

2013 ◽  
Vol 58 ◽  
pp. 208-216 ◽  
Author(s):  
Xinliang Tian ◽  
Muk Chen Ong ◽  
Jianmin Yang ◽  
Dag Myrhaug

2010 ◽  
Vol 98 (12) ◽  
pp. 742-753 ◽  
Author(s):  
Claudio Mannini ◽  
Ante Šoda ◽  
Ralph Voß ◽  
Günter Schewe

Author(s):  
Axel Holewa ◽  
Sébastien Guérin ◽  
Christian Weckmüller ◽  
Lars Enghardt

Struts and bifurcations installed in the bypass duct of aeroengines can deteriorate the aerodynamic and acoustic performances of the fan and therefore should be accounted for in the design process. This paper compares two 3-D unsteady RANS simulations of a fan model obtained respectively for an isolated and an installed configuration. In the installed case the strut–bifurcation system creates a strong disturbance of the steady flowfield. This involves a deformation of the rotor wakes during their convection, so that their impingement on the stator generates pressure fluctuations acting as sound sources with strong scattered azimuthal mode orders. The scattering is found by analyzing the acoustic field upstream and downstream of the fan stage. The present results are obtained while the rotor is supersonic (Mtip,rel ≈ 1.24). Since all the blades are identical, no frequency scattering (buzz-saw) does happen in the simulations.


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