On the Wing Sections with High Maximum Lift Coefficient
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- YAMANA Late Masao
- 明治大学工学部
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- ITO Akira
- 明治大学工学部
Bibliographic Information
- Other Title
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- 最大揚力係数の大きな翼型
- 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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Abstract
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.
Journal
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- Aeronautical and Space Sciences Japan
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Aeronautical and Space Sciences Japan 25 (279), 201-207, 1977
THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES
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Details 詳細情報について
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- CRID
- 1390001204507126528
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- NII Article ID
- 130003958187
- 10004069179
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- NII Book ID
- AN00189072
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- ISSN
- 24241369
- 00214663
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- NDL BIB ID
- 1823047
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- Text Lang
- ja
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- Data Source
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- JaLC
- NDL
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed