Mesh Adaption Strategies for Vortex-dominated Flows

Mesh Adaption Strategies for Vortex-dominated Flows

Author: Sean Javad Kamkar

Publisher: Stanford University

Published: 2011

Total Pages: 218

ISBN-13:

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A new adaptive mesh refinement strategy that is based on a coupled feature-detection and error-estimation approach is developed. The overall goal is to apply the proper degree of refinement to key vortical features in aircraft and rotorcraft wakes. The refinement paradigm is based on a two-stage process wherein the vortical regions are initially identified for refinement using feature-detection, and then the appropriate resolution is determined by the local solution error. The feature-detection scheme uses a local normalization procedure that allows it to automatically identify regions for refinement with threshold values that are not dependent upon the convective scales of the problem. An error estimator, based on the Richardson Extrapolation method, then supplies the identified features with appropriate levels of refinement. The estimator is shown to be well-behaved for steady-state and time-accurate aerodynamic flows. The above strategy is implemented within the Helios code, which features a dual-mesh paradigm of unstructured grids in the near-body domain, and adaptive Cartesian grids in the off-body domain. A main objective of this work is to control the adaption process so that high fidelity wake resolution is obtained in the off-body domain. The approach is tested on several theoretical and practical vortex-dominated flow-fields in an attempt to resolve wingtip vortices and rotor wakes. Accuracy improvements to rotorcraft performance metrics and increased wake resolution are simultaneously documented.


Mesh Adaption Strategies for Vortex-dominated Flows

Mesh Adaption Strategies for Vortex-dominated Flows

Author: Sean Javad Kamkar

Publisher:

Published: 2011

Total Pages:

ISBN-13:

DOWNLOAD EBOOK

A new adaptive mesh refinement strategy that is based on a coupled feature-detection and error-estimation approach is developed. The overall goal is to apply the proper degree of refinement to key vortical features in aircraft and rotorcraft wakes. The refinement paradigm is based on a two-stage process wherein the vortical regions are initially identified for refinement using feature-detection, and then the appropriate resolution is determined by the local solution error. The feature-detection scheme uses a local normalization procedure that allows it to automatically identify regions for refinement with threshold values that are not dependent upon the convective scales of the problem. An error estimator, based on the Richardson Extrapolation method, then supplies the identified features with appropriate levels of refinement. The estimator is shown to be well-behaved for steady-state and time-accurate aerodynamic flows. The above strategy is implemented within the Helios code, which features a dual-mesh paradigm of unstructured grids in the near-body domain, and adaptive Cartesian grids in the off-body domain. A main objective of this work is to control the adaption process so that high fidelity wake resolution is obtained in the off-body domain. The approach is tested on several theoretical and practical vortex-dominated flow-fields in an attempt to resolve wingtip vortices and rotor wakes. Accuracy improvements to rotorcraft performance metrics and increased wake resolution are simultaneously documented.


Process Intensification

Process Intensification

Author: Mirko Skiborowski

Publisher: Walter de Gruyter GmbH & Co KG

Published: 2022-10-03

Total Pages: 324

ISBN-13: 3110724995

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Process intensification aims for increasing efficiency and sustainability of (bio-)chemical production processes. This book presents strategies for improving fluid separation such as reactive distillation, reactive absorption and membrane assisted separations. The authors discuss computer simulation, model development, methodological approaches for synthesis and the design and scale-up of final industrial processes.


Computational Grids

Computational Grids

Author: Graham F. Carey

Publisher: CRC Press

Published: 1997-05-01

Total Pages: 518

ISBN-13: 9781560326359

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In this comprehensive volume a treatment of grid generation, adaptive refinement, and redistribution techniques is developed together with supporting mathematical, algorithmic, and software concepts. Efficient solution strategies that exploit grid hierarchies are also described and analyzed. Emphasis is on the fundamental ideas, but the presentation includes practical guidelines for designing and implementing grid strategies.


Numerical Solutions of the Euler Equations for Steady Flow Problems

Numerical Solutions of the Euler Equations for Steady Flow Problems

Author: Albrecht Eberle

Publisher: Vieweg+Teubner Verlag

Published: 2013-04-17

Total Pages: 456

ISBN-13: 3663068315

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The last decade has seen a dramatic increase of our abilities to solve numerically the governing equations of fluid mechanics. In design aerodynamics the classical potential-flow methods have been complemented by higher modelling-level methods. Euler solvers, and for special purposes, already Navier-Stokes solvers are in use. The authors of this book have been working on the solution of the Euler equations for quite some time. While the first two of us have worked mainly on algorithmic problems, the third has been concerned off and on with modelling and application problems of Euler methods. When we started to write this book we decided to put our own work at the center of it. This was done because we thought, and we leave this to the reader to decide, that our work has attained over the years enough substance in order to justify a book. The problem which we soon faced, was that the field still is moving at a fast pace, for instance because hyper sonic computation problems became more and more important.


Simulation of Vortex Interactions with a Solid Wall Using Adaptive Mesh Refinement

Simulation of Vortex Interactions with a Solid Wall Using Adaptive Mesh Refinement

Author: Kristopher Rowe

Publisher:

Published: 2016

Total Pages: 152

ISBN-13:

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One feature that is common to many fluid flows is that phenomena of interest often occur at disparate length scales, whether it be vortices interacting with a boundary layer, or shear instabilities on an internal gravity wave. It has been demonstrated in many studies that when performing computer simulations of fluid flows, one must ensure that sufficient resolution is used to capture the smallest scale features of the flow. If the smallest scale features of the flow occur in a small subset of the problem domain, however, much of the computational resources used for a simulation will be wasted where they are not needed. In order to address these kinds of problems, a class of algorithms known as adaptive mesh refinement (AMR) seek to use grid resolution only where it is needed. Upon a coarse base grid, areas of a fluid flow where small scale features occur are identified, and a hierarchy of successively finer grids is build until sufficient resolution is obtained. We give a thorough review of the adaptive mesh refinement algorithm for the incompressible Navier-Stokes equations presented in Martin, Colella, and Graves (2008) and connect their techniques to the literature for finite volume methods. The performance and scalability of their algorithm on a commodity computer cluster is studied in order to systematically choose optimal grid parameters. This algorithm is then used to perform a number of simulations of vortices interacting with a viscous boundary layer. Following Clercx and Bruneau (2006), the interaction of a vortex dipole with a solid wall is modelled: a problem which has been suggested as a difficult physical benchmark for incompressible Navier-Stokes solvers due to the resolution needed to obtain the correct behaviour for the flow. The interaction of a vortex ring with a solid wall is also simulated for a variety of Reynolds numbers. The results of these simulations are shown agree well with those seen in laboratory experiments. A loop-structured secondary vortex ring is formed which undergoes a topologically complex interaction with the initial vortex ring, ultimately leading to the breakdown and dissipation of both vortex rings. Emphasis is placed on the performance of AMR when compared to a traditional single grid model, and subsequently, the ability of AMR methods to model fluid flows using direct numerical simulation at higher Reynolds numbers than were previously possible.