書誌事項
- タイトル別名
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- Study of aerodynamic interference between main wing and tail wing using 2D Building-Cube Method
抄録
<p>In this study, a two-dimensional compressible block-structured Cartesian mesh CFD solver was used to perform a numerical analysis of the cross-sectional shapes of the NASA-CRM main and tail wings. The purpose is to investigate the influence of aerodynamic interference between the main wing and the tail. As a result, it was revealed that the lift coefficient and the pitching moment coefficient tend to increase by employing finer mesh. In addition, the flowfields slightly differ with/without the refinement between the main wing and the tail when the wake from the main wing affects the tail.</p>
収録刊行物
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- 北陸信越支部総会・講演会 講演論文集
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北陸信越支部総会・講演会 講演論文集 2021.58 (0), E013-, 2021
一般社団法人 日本機械学会
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詳細情報 詳細情報について
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- CRID
- 1390852482512630912
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- NII論文ID
- 130008092485
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- ISSN
- 24242772
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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