Geometry optimization of sound-propagating flows in complex-shaped spaces based on a higher-order scheme
| Project/Area Number |
15K04759
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| Research Category |
Grant-in-Aid for Scientific Research (C)
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| Allocation Type | Multi-year Fund |
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| Section | 一般 |
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| Research Field |
Computational science
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| Research Institution | Ehime University |
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Principal Investigator |
Matsuura Kazuo 愛媛大学, 理工学研究科(工学系), 准教授 (20423577)
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| Project Period (FY) |
2015-04-01 – 2018-03-31
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| Project Status |
Completed (Fiscal Year 2017)
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| Budget Amount *help |
¥4,940,000 (Direct Cost: ¥3,800,000、Indirect Cost: ¥1,140,000)
Fiscal Year 2017: ¥1,300,000 (Direct Cost: ¥1,000,000、Indirect Cost: ¥300,000)
Fiscal Year 2016: ¥1,300,000 (Direct Cost: ¥1,000,000、Indirect Cost: ¥300,000)
Fiscal Year 2015: ¥2,340,000 (Direct Cost: ¥1,800,000、Indirect Cost: ¥540,000)
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| Keywords | 数値シミュレーション / 流体 / 高次精度スキーム / 最適化 / 流体解析 / 境界層 / 層流ー乱流遷移 / 水素安全 / センシング / 流体力学 / 空力音響学 / 数値流体力学 / 格子インターフェース |
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| Outline of Final Research Achievements |
A new optimization method for compressive flows with sound propagation in complex space is developed. A higher-order accurate IB method and an interface condition based on characteristic lines are derived. In the development of the interface condition, it is extended for non-conforming cases where mesh points do not coincide on the interface.The developed method was incorporated into a fluid analysis software of compressible Navier-Stokes equation based on higher-order accuracy scheme, which is parallelized by MPI. This method was also successfully applied to the problem of introducing longitudinal vortices by wedge rows to a boundary layer formed under hypersonic flows of Mach 6.
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Report
(4 results)
Research Products
(5 results)
