Towards industry-ready high-order flow solvers : increasing robustness and usability

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Abstract/Contents

Abstract
High-order methods are truer to the flow physics and more accurate per degree of freedom than low-order methods. Their high computational intensity relative to their communication requirements makes them prime candidates for implementation in the latest hyper-parallel computing architectures like Graphical Processing Units (GPUs). Why are they not more prevalent in the toolset of design teams? One of the main barriers to wide adoption of high-order numerical methods in industrial applications is the schemes' low robustness relative to low-order methods. Their stability is highly dependent on the quality of the grid, even when the solution is relatively smooth. Aliasing, underresolution, and non-smoothness are the main causes of instabilities. This dissertation proposes solutions from two fronts: the creation of a set of families of numerical schemes with guaranteed linear stability and tunable dispersion- dissipation properties, and the formulation of filters with spectral effectiveness and element-local stencil. To ease the adoption, or increase usability, of high-order methods in industry and academia, a well-documented, validated, verified, and constantly improved source code is needed. This dissertation walks the reader through the efforts by the Aerospace Computing Laboratory (ACL) to provide such code: High-Fidelity Large Eddy Simulation (LES) Open Source Code (HiFiLES) (hifiles.stanford.edu).

Description

Type of resource text
Form electronic; electronic resource; remote
Extent 1 online resource.
Publication date 2016
Issuance monographic
Language English

Creators/Contributors

Associated with Lopez Morales, Manuel Rodrigo
Associated with Stanford University, Department of Aeronautics and Astronautics.
Primary advisor Jameson, Antony, 1934-
Thesis advisor Jameson, Antony, 1934-
Thesis advisor Alonso, Juan José, 1968-
Thesis advisor Farhat, Charbel
Advisor Alonso, Juan José, 1968-
Advisor Farhat, Charbel

Subjects

Genre Theses

Bibliographic information

Statement of responsibility Manuel Rodrigo López Morales.
Note Submitted to the Department of Aeronautics and Astronautics.
Thesis Thesis (Ph.D.)--Stanford University, 2016.
Location electronic resource

Access conditions

Copyright
© 2016 by Manuel Rodrigo Lopez Morales
License
This work is licensed under a Creative Commons Attribution Non Commercial 3.0 Unported license (CC BY-NC).

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