The main purpose is to develop an efficient yet accurate tightly coupling method integrating Euler and potential flow solvers. In order to improve the efficiency while maintaining a good accuracy of the method, artificial boundary condition is introduced to reduce the domain size required for the far-field boundary condition. The coupled solver is validated in various flow cases around two-dimensional airfoil and three-dimensional wing. The validation result showed that the tightly coupled solver is valid in the various flow cases.
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