タイトル(掲載誌)航空宇宙技術研究所報告 = Technical Report of National Aerospace Laboratory TR-932
一般注記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.
資料番号: NALTR0932000
レポート番号: NAL TR-932
一次資料へのリンクURLhttps://jaxa.repo.nii.ac.jp/?action=repository_action_common_download&item_id=45191&item_no=1&attribute_id=31&file_no=1
連携機関・データベース国立情報学研究所 : 学術機関リポジトリデータベース(IRDB)(機関リポジトリ)
提供元機関・データベース宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ