2009
DOI: 10.1016/j.compfluid.2009.04.007
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Hybrid grid generation for two-dimensional high-Reynolds flows

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Cited by 35 publications
(14 citation statements)
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“…Therefore, it is not only necessary to capture these detailed flow features, but also to verify that the flow field solution is independent of the constructed grids. An incorrect evaluation of the flow field solution can be incurred if the local size of the grids is not considered in greater extent and variations in the smaller portion of the domain, the sampler inlet grid, can affect the whole flow field solution (Dussin, Fossati, Guardone & Vigevano, 2009). The aforementioned drawbacks are particularly encountered when manual scaling of grids is used, since several attempts may be needed to generate a grid that can reach a converged solution from which subsequent scaling will be performed and that can achieve the least computational effort.…”
Section: Methods and Modelsmentioning
confidence: 99%
“…Therefore, it is not only necessary to capture these detailed flow features, but also to verify that the flow field solution is independent of the constructed grids. An incorrect evaluation of the flow field solution can be incurred if the local size of the grids is not considered in greater extent and variations in the smaller portion of the domain, the sampler inlet grid, can affect the whole flow field solution (Dussin, Fossati, Guardone & Vigevano, 2009). The aforementioned drawbacks are particularly encountered when manual scaling of grids is used, since several attempts may be needed to generate a grid that can reach a converged solution from which subsequent scaling will be performed and that can achieve the least computational effort.…”
Section: Methods and Modelsmentioning
confidence: 99%
“…Also, the number of design variables times 100 is taken for the number of blackbox evaluations needed for each optimization problem. A hybrid grid (Dussin et al 2009) is used around the NACA 0012 airfoil and a structured one inside the leading edge's composite shell (Fig. 10).…”
Section: Numerical Test Casesmentioning
confidence: 99%
“…The results have been compared with wind tunnel experimental data . The initial grid has been generated by means of a hybrid grid generation technique proposed by the authors . The grid is made of 19,370 nodes and 24,579 elements and comprises a structured layer for the boundary layer around the main airfoil element and around the flap, together with three structured regions located approximately in correspondence of the wakes at the trailing edge of both the main element and the flap and in correspondence of the lower corner of the flap cove.…”
Section: Numerical Experimentsmentioning
confidence: 99%