書誌事項
- タイトル別名
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- Aerodynamic Characteristics of thin Aerofoil Sections having Narrow Gaps
- セマイ ゲキカン オ モツ 2ジゲン ウスヨク ノ クウリキ トクセイ
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説明
Aerodynamic characteristics of two-dimensional thin aerofoils having narrow gaps are investigated, being based on the limit matching principle. The flow is assumed to be inviscid, incompressible and steady. Both the camber line and the gap location are assumed to be arbitrary. Lift, pitching moment, and center-of-pressure location are given in closed expressions. It is found that blend of the three concepts-limit matching principle, reciprocal theorem, and membrane-makes calculations drastically simple. Applications are presented for flat and circulararc airfoils. The case of deflected fap is also discussed for the arbitrary hinge location at which the gap exists.
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 (276), 33-40, 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
- 1390001204506457216
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- NII論文ID
- 130003958166
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- NII書誌ID
- AN00189072
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- ISSN
- 24241369
- 00214663
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- NDL書誌ID
- 1806808
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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