A CFD code is used to simulate flow over a twodimensional airfoil at an angle of attack

Chapter 15, Problem 15-16

(choose chapter or problem)

A CFD code is used to simulate flow over a twodimensional airfoil at an angle of attack. A portion of the computational domain near the airfoil is outlined in Fig. P1516 (the computational domain extends well beyond the region outlined by the dashed line). Sketch a coarse structured grid using four-sided cells and sketch a coarse unstructured grid using three-sided cells in the region shown. Be sure to cluster the cells where appropriate. Discuss the advantages and disadvantages of each grid type.

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