MEGAFLOW - Numerical Flow Simulation for Aircraft Design: Results of the second
210,66 €
Grid Generation. - Structured Solver FLOWer. - Turbulence Models in FLOWer. - Hybrid Solver TAU. - Overview of the Hybrid RANS Code TAU. - Hybrid Grid Adaptation in TAU. - Shape Optimization. - The Continuous Adjoint Approach in Aerodynamic Shape Optimization.
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