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- 友成 義正
- 日本文理大学(旧大分工業大学)工学部
書誌事項
- タイトル別名
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- Aeroelastic Galloping of a Two-dimensional Flat Plate Set Normal to a Uniform Flow with a Wake Splitter Plate Attached to It
- コウリュウ スプリッタバン オ ユウシ イチヨウリュウ ニ スイチョク ナ 2
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説明
This paper reports the results of a wind tunnel experiment conducted to investigate the property of aeroelastic galloping and the pressure distribution of a two-dimensional flat plate set normal to a uniform flow with a wake splitter plate attached to it. Measurements show that (1) the instability of galloping starts and develops rapidly as the streamwise depth of the splitter plate exceeds a certain value, and (2) at around this singular depth, the pressure at the trailing edge of the splitter plate reaches a minimum. The correlation between the onset of galloping and the pressure variation, mentioned above, is similar to that observed for rectangular, or D-shaped cross-sectional cylinders.
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 30 (345), 581-588, 1982
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
- 1390282679483888768
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- NII論文ID
- 130003958511
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- NII書誌ID
- AN00189072
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- ISSN
- 24241369
- 00214663
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- NDL書誌ID
- 2467113
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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
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- CiNii Articles
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- 抄録ライセンスフラグ
- 使用不可