Numerical simulation of the aerodynamics of high-lift configurations /
General Material Designation
[Book]
First Statement of Responsibility
Omar Darío López Mejia, Jaime A. Escobar Gomez, editors.
.PUBLICATION, DISTRIBUTION, ETC
Place of Publication, Distribution, etc.
Cham, Switzerland :
Name of Publisher, Distributor, etc.
Springer,
Date of Publication, Distribution, etc.
2018.
PHYSICAL DESCRIPTION
Specific Material Designation and Extent of Item
1 online resource
INTERNAL BIBLIOGRAPHIES/INDEXES NOTE
Text of Note
Includes bibliographical references.
CONTENTS NOTE
Text of Note
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
Text of Note
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
Text of Note
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
Text of Note
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
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SUMMARY OR ABSTRACT
Text of Note
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 aerodynamics of high-lift configurations has become an active field not only in academic but also in industrial environments. The scope of the book includes applications and topics of interest related to the simulation of high-lift configurations such as: lift and drag prediction, unsteady aerodynamics, low Reynolds effects, high performance computing, turbulence modelling, flow feature visualization, among others. This book gives a description of the state-of-the-art of computational models for simulation of high-lift configurations. It also shows and discusses 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.
ACQUISITION INFORMATION NOTE
Source for Acquisition/Subscription Address
Springer Nature
Stock Number
com.springer.onix.9783319621364
OTHER EDITION IN ANOTHER MEDIUM
Title
Numerical simulation of the aerodynamics of high-lift configurations.