2018年
Postlimiters and simple dirty-cell detection for three-dimensional unstructured (unlimited) aerodynamic simulations
AIAA Journal
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- 巻
- 56
- 号
- 8
- 開始ページ
- 3192
- 終了ページ
- 3204
- 記述言語
- 英語
- 掲載種別
- 研究論文(学術雑誌)
- DOI
- 10.2514/1.J056683
- 出版者・発行元
- American Institute of Aeronautics and Astronautics (AIAA)
Copyright © 2018 by the American Institute of Aeronautics and Astronautics, Inc. All rights reserved. The postlimiter (simple a posteriori slope limiter) is an anti-slope-limiting mechanism to preserve nominal second order in space as much as possible. This technique has been demonstrated to increase resolutions of two-dimensional simulations up to four times in each dimension [Kitamura, K., and Hashimoto, A., "Simple a posteriori Slope Limiter (Post Limiter) for High Resolution and Efficient Flow Computations," Journal of Computational Physics, Vol. 341, July 2017, pp. 313-340]. This paper extends the postlimiter to three dimensions with an emphasis on "dirty" (meaning ill-shaped) cells, which arise in practical three-dimensional (3-D) unstructured grids over complex geometries. Gradient accuracy is known to significantly deteriorate on dirty cells, and a slope limiter needs to be applied. However, the original postlimiter does not recognize dirty cells and deactivates a slope limiter. To address this issue, a simple dirty-cell detection method is proposed and incorporated into the postlimiter. The 3-D version of postlimiter (referred to as "postlimiter 3") is successfully incorporated into fast aerodynamic routine (FaSTAR), a 3-D unstructured grid flow solver is developed at the Japan Aerospace Exploration Agency. Postlimiter 3 can handle general 3-D unstructured grids. Numerical examples support its efficiency, accuracy, robustness, and applicability to a wide spectrum of aerodynamic problems of high engineering importance.
- リンク情報
- ID情報
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- DOI : 10.2514/1.J056683
- ISSN : 0001-1452
- eISSN : 1533-385X
- SCOPUS ID : 85051024117