書誌事項
- タイトル別名
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- On the Relation between Subsonic Part of Supersonic Cascade and Directions of Outlet Flow
- チョウオンソクヨクレツ ノ アオンソクブ ト リュウシュツ ホウコウ ノ カンケイ ニ ツイテ
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This paper deals with the analitical method to obtain the directions of outlet flow of the subsonic flow down-stream a normal shock in the neighbouring blades of the two-dimensional supersonic cascade of which subsonic part consists of straight surfaces. This method first solves the problem for the corresponding invisid flow, and then applied its solution to the compressible flow by Karman-Tsien's method. According to the analysed results, the relation α-∞≥α+∞≥(1/2)α-∞ exists between the outlet flow direction α+∞ and the divergence angle of the subsonic part α-∞, and the outlet flow direction coincides with the tangential detection to the pressure side, when a normal shock occurs at the trailing edge of a blade. The more upstream a normal shock occurs in the subsonic region, the nearer the outlet flow direction turns to the suction side of the blade first rapidly and then slowly.
収録刊行物
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- 日本機械学會論文集
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日本機械学會論文集 28 (195), 1504-1511, 1962
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
- 1390001205159643392
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- NII論文ID
- 110002351718
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- NII書誌ID
- AN00187419
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- ISSN
- 21859485
- 00290270
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- NDL書誌ID
- 9151061
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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
- NDL
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可