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Ebrahimi Pour, Neda: Efficient high-order simulation of aeroacoustics from rigid body motion on massively parallel systems. 2021
Inhalt
Title Page
Acknowledgement
Abstract
Zusammenfassung
Contents
Nomenclature
Notation
Introduction
Motivation
Related work
Embedded method
Partitioned coupling
Aim of this work
Outline
Fluid dynamic equations
Compressible viscid Navier-Stokes equations
Boundary conditions
Compressible inviscid Euler equations
Boundary conditions
Linearized Euler equations
Boundary conditions
Discretization in space and time
Spatial discretization - Discontinuous Galerkin method
Compressible inviscid Euler equations
Compressible viscous Navier-Stokes equations
Explicit time discretization - Runge-Kutta method
Numerical oscillations - Gibbs oscillation
Numerical Framework
APES simulation framework
High-order Discontinuous Galerkin solver - Ateles
Integrated coupling approach - APESmate
External coupling approach - preCICE
Embedded boundary method
State of the art - Geometry representation
Volume penalization method - Brinkman penalization
Representation of the masking function in high-order Discontinuous Galerkin
Evaluation of the masking function in the numerical scheme
Over-integration - Cost estimation
Specification of the masking function
Implicit-mixed-explicit Runge-Kutta method
Validation of the moving geometry
Convergence study - Acoustic pulse
Shock capturing - Shock-wall interaction
Interaction of a shock wave with a non-moving wall
Interaction of a shock wave with a moving wall
Shock formation - Moving piston
Curved boundary - Moving cylinder
Sharp boundary - Supersonic moving wedge
Reduced computation inside the geometry
Scalability and computational cost of the embedded method
Scalability of the embedded method
Computational cost of the embedded method
Multi-scale problems - An efficient strategy
State of the art - Coupled problems
Partitioned coupling
Quality of the solution - Data mapping
Interpolation
Data mapping by evaluation
Error investigation
Load balancing - Coupled multi-scale problems
Intra-subdomain
SPartA algorithm
Inter-subdomain
Optimization of the gradient computation
Load balancing for a 3-field coupled simulation
Application examples - Complex moving geometries
Numerical results - Moving geometry
Supersonic flow - Moving cylinder
Rotating airfoil
Collision of two moving spheres
Collision of three moving Spheres
Rotating fan
Performance results - Moving geometry
Rotating fan
Collision of three moving Spheres
Numerical results - Coupled 3-field simulation
Innermost subdomain: Compressible Navier-Stokes
Innermost and middle subdomain: Compressible Navier-Stokes and Euler
Innermost, middle and outermost subdomain: Navier-Stokes, Euler and Linearized Euler
Coupling interfaces of the 3-field coupled simulation
Performance
Conclusion
Appendix
Multi-scale simulations - Partitioned coupling with preCICE
Reduced computation inside the geometry - Code
Sharp boundary - Supersonic moving wedge
Sponge - Reduced boundary reflections
Bibliography
List of Figures
List of Tables