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Flow Patterns Induced by Vortices
https://jaxa.repo.nii.ac.jp/records/45191
https://jaxa.repo.nii.ac.jp/records/45191b92b9271-f35b-400a-b212-60ea6fce9935
名前 / ファイル | ライセンス | アクション |
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naltr00932.pdf (1.0 MB)
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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 | ||||||
言語 | en | |||||
タイトル | Flow Patterns Induced by Vortices | |||||
言語 | ||||||
言語 | eng | |||||
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 | ||||||
その他のタイトル | 渦のある翼間流れの数値シミュレーション | |||||
著者 |
西村, 英明
× 西村, 英明× NISHIMURA, Hideaki |
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著者所属 | ||||||
航空宇宙技術研究所原動機部 | ||||||
著者所属(英) | ||||||
en | ||||||
Aeroengine Division, National Aerospace Laboratory(NAL) | ||||||
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報告 en : Technical Report of National Aerospace Laboratory TR-932 巻 932, p. 13, 発行日 1987-05 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | When located in a confined region, vortices form a flow field in the region of mutual interference. The obtained flow field is very useful in the analysis of the secondary flow in a cascade. In this report three flow patterns are calculated by using the elliptic functions and hyperbolic functions. The flows are in; 1) a parallelogram bounded by four boundaries, 2) a channel restricted by upper and lower boundaries, 3) a half region confined by upper, lower and left boundaries. The method of vortex distribution in a calculation plane and the calculated results are also shown. A few comments on the characteristics of the elliptic functions are presented in the appendix. It is concluded that this method is effective in analysing the secondary flows with vortices in a cascade. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 0389-4010 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: NALTR0932000 | |||||
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 TR-932 |