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Numerical simulation of the aerodynamics of high-lift configurations

Author: Omar Darío López Mejia; Jaime A Escobar Gomez
Publisher: Cham, Switzerland : Springer, 2018.
Edition/Format:   eBook : Document : EnglishView all editions and formats
Summary:
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 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  Read more...
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Genre/Form: Electronic books
Additional Physical Format: Print version:
Numerical simulation of the aerodynamics of high-lift configurations.
Cham, Switzerland : Springer, 2018
(OCoLC)989966288
Material Type: Document, Internet resource
Document Type: Internet Resource, Computer File
All Authors / Contributors: Omar Darío López Mejia; Jaime A Escobar Gomez
ISBN: 9783319621364 331962136X
OCLC Number: 1031214409
Description: 1 online resource
Contents: Intro; Preface; Contents; Review on High-Lift Systems for Aerodynamic Applications; 1 Introduction; 2 Trailing Edge Devices; 3 Leading Edge Devices; 4 Physics of High-Lift Systems and Numerical Simulations; References; Grid Generation About High-Lift Wing Configurations; 1 Introduction; 2 CAD Model; 3 Mesh Generation Guidelines; 4 Surface Mesh Generation; 4.1 Farfield and Symmetry Plane; 4.2 Grid Quality; 4.3 Deviation from HiLiftPW3 Meshing Guidelines; 5 Volume Grid Generation; 6 Final Remarks; References; Incompressible Solutions About High-Lift Wing Configurations; 1 Introduction 2 Numerical Approach3 Grid Generation; 4 Solution Process; 5 Results and Discussion; 5.1 Force and Moment Comparisons; 5.2 Pressure Comparisons; 6 Conclusions and Future Work; References; Numerical Investigations of the Jaxa High-Lift Configuration Standard Model with MFlow Solver; 1 Introduction; 2 Geometry and Computational Grids; 3 Numerical Methods; 4 Results; 4.1 The Performance of Massively Parallel Computing; 4.2 The Effects of Nacelle and Pylon Assembled; 5 Conclusions; References; Time-Resolved Adaptive Direct FEM Simulation of High-Lift Aircraft Configurations; 1 Introduction 2 Simulation Methodology2.1 The cG(1)cG(1) Method; 2.2 The Adaptive Algorithm; 2.3 A Posteriori Error Estimate for cG(1)cG(1); 2.4 The Do-Nothing Error Estimate and Indicator; 2.5 Turbulent Boundary Layers; 2.6 Numerical Tripping; 2.7 The FEniCS-HPC Finite Element Computational Framework; 3 Results; 3.1 Aerodynamic Forces; 3.2 Pressure Coefficients; 3.3 Flow and Adaptive Mesh Refinement Visualization; 4 Conclusions; References; RANS Simulations of the High Lift Common Research Model with Open-Source Code SU2; 1 Introduction; 2 NASA's Common Research Model; 3 Numerical Methods 3.1 Stanford University Unstructured (SU2)3.2 Turbulence Modelling; 3.3 Computational Resources; 3.4 Geometry Description and Grids; 3.5 Geometry; 4 Results and Discussion; 5 Conclusions; References
Responsibility: Omar Darío López Mejia, Jaime A. Escobar Gomez, editors.

Abstract:

This book deals with numerical simulations and computations of the turbulent flow around high-lift configurations commonly used in aircraft.  Read more...

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