書誌事項
- タイトル別名
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- Analysis of the Large Deformation of Biconvex Airfoil Sections in an Air-Flow.
- キリュウ チュウ デ オオキク ヘンケイ スル レンズ ヨクガタ ノ ケイジョウ カイセキ
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説明
It is desirable that an airpiane couid exert its optimum aerodynamic performance by deforming the wing section to be suitable to the flight conditions. In this paper is presented an analytical calculation of the large deformation of a biconvex wing section and the experiment to confirm the calculated result. The experiment was carried out in a wind tunnel on the biconvex wing model being hollow and of which the outer surface is composed of two elastic curved thin plates. The wing surface is deformed through change of the difference between the outside pressure and the inside pressure of the wing in the air flow by adjusting the inside pressure. The good agreement is obtained between the analytical results and the experimental ones for the contours of the deformed wing sections.
収録刊行物
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- 日本航空宇宙学会論文集
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日本航空宇宙学会論文集 47 (549), 389-395, 1999
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
- 1390282679445536384
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- NII論文ID
- 10002723478
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- NII書誌ID
- AA11307372
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- ISSN
- 24323691
- 13446460
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- NDL書誌ID
- 4885229
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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