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Development of Turbulent Boundary Layers Along the Curved Walls of an Annular Diffusing Passage
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| 内容注記 |
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Turbulent boundary layer development along the curved walls of an axisymmetric diffusing annulus was determined experimentally and compared with results calculated using a form of the von Karman momentum integral boundary layer equation and several sets of simple auxiliary equations.Based on the comparisons made,one iterative solution method for predicting curved wall annular diffuser boundary layer growth that yields fair results is proposed.
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資料番号: NALTR0278T000
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レポート番号: NAL TR-278T
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航空宇宙技術研究所
National Aerospace Laboratory(NAL)
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| 日付 |
Created2020-01-29
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Issued1972-02
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| 言語 |
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| 資源タイプ |
technical report |
| 出版タイプ |
NA |
| 資源識別子 |
URI
http://id.nii.ac.jp/1696/00044515/
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| 収録誌情報 |
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Technical Report of National Aerospace Laboratory TR-278T
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巻278T
開始ページ13
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| ファイル |
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| コンテンツ更新日時 |
2023-03-20 |