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- 明石 光一郎
- 熊本工大
書誌事項
- タイトル別名
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- Partial Flow Visualization around an Airfoil by the Smoke Wind Tunnel
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抄録
In teaching fluid mechanics, we have been making researches of high lift devices of an airplane, flap and slat by using a smoke wind tunnel. In this experimental study, we used NACA4412 wing section, and searched the optimum shape of a slot between the main wing and the flap. By the partial flow visualization technique, we confirmed the slot shape that a smoke streak-line passing through the slot was attached to the upper surface of the flap and by the force measurement technique, we also confirmed that the slot shape mentioned above had brought maximum lift coefficient. In this paper, we refer to the partial flow visualization of slotted flap of 40% chord length.
収録刊行物
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- 可視化情報学会誌
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可視化情報学会誌 15 (Supplement2), 101-104, 1995
社団法人 可視化情報学会
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詳細情報
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- CRID
- 1390282679595421696
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- NII論文ID
- 10002673762
- 130003648473
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- NII書誌ID
- AN10374478
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- ISSN
- 1884037X
- 09164731
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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
- Crossref
- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可