Numerical Simulation of the Aerodynamics of High-Lift Configurations by Omar Darío López Mejia & Jaime A. Escobar Gomez

Author:Omar Darío López Mejia & Jaime A. Escobar Gomez
Language: eng
Format: epub
Publisher: Springer International Publishing, Cham

4 Results

To exclude the uncertainty introduced by the lack of computational convergence, all the computations are run until the norm of the global residual decreases by more than three orders of magnitude, and the final oscillations of aerodynamic force and moment are less than 1%. Examples of the convergence of density residual and force/moment coefficient are presented in Fig. 3.

Fig. 3Convergence of density residual and force and moment coefficient

4.1 The Performance of Massively Parallel Computing

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