書誌事項
- タイトル別名
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- Numerical Analysis of Detached Shock Wave by Cartesian Mesh
抄録
Recently spaceplane has been researched and developed all over the world because they have some advantage for world environment and economy. But they have many aerodynamics problems in development. One of them is shock-shock interaction. These problems may cause serious incidents because the shock wave is known to affect aerodynamics heating and flight performance. Shock wave occur during supersonic flight. Thus, in this research, a cylinder model in used to, analyze detachment shock wave by Cartesian grid.Computationalresult is compared with the experimental data about standoff distance. Through the computations, the accuracy of Cartesian-mesh CFD for supersonic was validated. As a result, it was confirmed that the computational result almost coincided with the experimental data.
収録刊行物
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- 北陸信越支部総会・講演会 講演論文集
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北陸信越支部総会・講演会 講演論文集 2020.57 (0), N012-, 2020
一般社団法人 日本機械学会
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詳細情報 詳細情報について
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- CRID
- 1390004951544655616
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- NII論文ID
- 130007943070
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- ISSN
- 24242772
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- 本文言語コード
- ja
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- データソース種別
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- JaLC
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可