Numerical simulation of the aerodynamics of high-lift configurations /
نام عام مواد
[Book]
نام نخستين پديدآور
Omar Darío López Mejia, Jaime A. Escobar Gomez, editors.
وضعیت نشر و پخش و غیره
محل نشرو پخش و غیره
Cham, Switzerland :
نام ناشر، پخش کننده و غيره
Springer,
تاریخ نشرو بخش و غیره
2018.
مشخصات ظاهری
نام خاص و کميت اثر
1 online resource
یادداشتهای مربوط به کتابنامه ، واژه نامه و نمایه های داخل اثر
متن يادداشت
Includes bibliographical references.
یادداشتهای مربوط به مندرجات
متن يادداشت
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
متن يادداشت
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
متن يادداشت
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
متن يادداشت
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
بدون عنوان
0
بدون عنوان
8
بدون عنوان
8
بدون عنوان
8
یادداشتهای مربوط به خلاصه یا چکیده
متن يادداشت
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.
یادداشتهای مربوط به سفارشات
منبع سفارش / آدرس اشتراک
Springer Nature
شماره انبار
com.springer.onix.9783319621364
ویراست دیگر از اثر در قالب دیگر رسانه
عنوان
Numerical simulation of the aerodynamics of high-lift configurations.