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- ANDO Shigenori
- 名古屋大学工学部航空学教室
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- AZUMA Toshihiko
- 名古屋大学工学部大学院(航空工学専攻)
Bibliographic Information
- Other Title
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- 狭いすき間をもつ二次元薄翼の空力特性
- 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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Description
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.
Journal
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- Aeronautical and Space Sciences Japan
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Aeronautical and Space Sciences Japan 25 (276), 33-40, 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
- 1390001204506457216
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- NII Article ID
- 130003958166
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- NII Book ID
- AN00189072
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- ISSN
- 24241369
- 00214663
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- NDL BIB ID
- 1806808
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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