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境界要素法による超音速非定常流の数値解析プログラム開発
https://jaxa.repo.nii.ac.jp/records/43506
https://jaxa.repo.nii.ac.jp/records/43506ed38eefa-827a-4ac9-a817-2dacc664cad1
名前 / ファイル | ライセンス | アクション |
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nalsp0016010.pdf (323.8 kB)
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Item type | テクニカルレポート / Technical Report(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 境界要素法による超音速非定常流の数値解析プログラム開発 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_18gh | |||||
資源タイプ | technical report | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Development of a Boundary Element Method Program for Numerical Analysis of Supersonic Unsteady Flow | |||||
著者 |
丸山, 祐一
× 丸山, 祐一× 澤田, 照夫× Maruyama, Yuichi× Sawada, Teruo |
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著者所属 | ||||||
岡山理科大学 | ||||||
著者所属 | ||||||
岡山理科大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Okayama University of Science | ||||||
著者所属(英) | ||||||
en | ||||||
Okayama University of Science | ||||||
出版者 | ||||||
出版者 | 航空宇宙技術研究所 | |||||
出版者(英) | ||||||
出版者 | National Aerospace Laboratory(NAL) | |||||
書誌情報 |
航空宇宙技術研究所特別資料 en : Special Publication of National Aerospace Laboratory SP-16 巻 16, p. 59-64, 発行日 1991-12 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A boundary element method program for supersonic unsteady flow around arbitrary configurations has been developed. The fundamental formulation is based on Morino's method. Linear distribution of doublet is adopted to ensure the continuity of the strength on panel edges, while constant distribution is used for source. The numerical results are given for the cases of flows around oscillating cones. The real parts of the solutions are compared with the results of steady flow calculations and they are shown to be consistent with each other. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0289-260X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10097345 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALSP0016010 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: NAL SP-16 |