Automatic mesh adaptation using the continuous adjoint approach and the spectral difference method
Abstract/Contents
- Abstract
- In this thesis, mesh adaptation using continuous adjoint is tested on two-dimensional Euler equations. Both the flow solver and the adjoint solver are implemented with the high order spectral difference (SD) method. Both h and p adaptation are studied. The test cases include a half-cylinder in subsonic flow and a NACA 0012 airfoil in subsonic and transonic flows. It is found that h-refinement is more suitable for flow discontinuities while p-refinement offers a better performance in smooth flows. Both adaptation methods lead to a faster functional convergence than uniformly h or p refined meshes. In addition, the adapted meshes show similar patterns as those arrived at using the discrete adjoint method. Comparisons between different adjoint target output functionals are also made.
Description
Type of resource | text |
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Form | electronic; electronic resource; remote |
Extent | 1 online resource. |
Publication date | 2013 |
Issuance | monographic |
Language | English |
Creators/Contributors
Associated with | Li, Yi |
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Associated with | Stanford University, Department of Aeronautics and Astronautics. |
Primary advisor | Jameson, Antony, 1934- |
Thesis advisor | Jameson, Antony, 1934- |
Thesis advisor | MacCormack, R. W. (Robert William), 1940- |
Thesis advisor | Pinsky, P |
Advisor | MacCormack, R. W. (Robert William), 1940- |
Advisor | Pinsky, P |
Subjects
Genre | Theses |
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Bibliographic information
Statement of responsibility | Yi Li. |
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Note | Submitted to the Department of Aeronautics and Astronautics. |
Thesis | Thesis (Ph.D.)--Stanford University, 2013. |
Location | electronic resource |
Access conditions
- Copyright
- © 2013 by Yi Li
- License
- This work is licensed under a Creative Commons Attribution Non Commercial 3.0 Unported license (CC BY-NC).
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