書誌事項
- タイトル別名
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- On the Wing Sections with High Maximum Lift Coefficient
- サイダイ ヨウリョク ケイスウ ノ オオキナ ヨクガタ
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説明
Experimental studies for determining the profiles of the wing sections with high maximum lift coefficient is described. Observation of flow around the wing sections and measurement of section lift coefficient are carried out in a twodimensional smoke wind-tunnel. Transition in the boundary layer along the wing surfaces is also observed by using evaporated-gas-oil smoke. Additionally, the wing sections with extended trailing-edge are investigated. Maximum lift coefficient up to 2.28 is obtained at Reynolds number of 5.34×105.
収録刊行物
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- 日本航空宇宙学会誌
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日本航空宇宙学会誌 25 (279), 201-207, 1977
一般社団法人 日本航空宇宙学会
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詳細情報 詳細情報について
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- CRID
- 1390001204507126528
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- NII論文ID
- 130003958187
- 10004069179
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- NII書誌ID
- AN00189072
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- ISSN
- 24241369
- 00214663
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- NDL書誌ID
- 1823047
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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