Titlebook: Numerical Simulation of the Aerodynamics of High-Lift Configurations; Omar Darío López Mejia,Jaime A. Escobar Gomez Book 2018 Springer Int

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Omar Darío López Mejia,Jaime A. Escobar GomezDescribes state-of-the-art computational and theoretical models for simulation of high-lift configurations.Includes numerical results and validations of computational models applied to of high-lift co

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978-3-030-09671-7Springer International Publishing AG, part of Springer Nature 2018

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Grid Generation About High-Lift Wing Configurations,about the NASA High Lift Common Research Model and the Japanese Aerospace Exploration Agency Standard Model with and without nacelles and pylons. Several modifications to the guidelines that enhance grid quality are presented. Additionally, the user-defined parameters within Pointwise that govern the mesh generation process are reviewed in detail.

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Book 2018voted to the Computational Fluids Dynamics (CFD) method using full Navier-Stokes solvers typically used in the simulation of high-lift configuration. With the increase of computational resources in the aeronautical industry, the computation of complex flows such as the aerodynamics of high-lift conf

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Incompressible Solutions About High-Lift Wing Configurations,e incompressible solutions about the Japanese Aerospace Exploration Agency Standard Model configuration with and without nacelles and pylons are compared with experiment at multiple angles of attack to demonstrate the effectiveness of this approach.

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lidations of computational models applied to of high-lift co.This book deals with numerical simulations and computations of the turbulent flow around high-lift configurations commonly used in aircraft. It is devoted to the Computational Fluids Dynamics (CFD) method using full Navier-Stokes solvers t

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numerical results and validation of these computational models. Finally, this book is a good reference for graduate students and researchers interested in the field of simulation of high-lift configurations..978-3-030-09671-7978-3-319-62136-4

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