書誌事項
- タイトル別名
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- Numerical Analysis of Circular Arc Airfoil at Low Reynolds Numbers
抄録
<p>Recently, with the advance of Micro Air Vehicle（MAV）and Mars exploratory airplane, there is a need to understand low Reynolds number flows. The objective of this study is to investigate the aerodynamic characteristics of a thin circular arc airfoil at low Reynolds numbers. Cartesian - mesh - based Computational Fluid Dynamics（CFD）was used to clarify the flow field of a thin circular arc airfoil with a camber of 3% chord at Reynolds numbers of 1.0 × 103 and 1.0 × 104. The results of this analysis were compared with the results of wind tunnel tests. As a result, qualitative agreement was obtained with the experimental results.</p>
収録刊行物
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- 計算力学講演会講演論文集
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計算力学講演会講演論文集 2021.34 (0), 118-, 2021
一般社団法人 日本機械学会
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キーワード
詳細情報 詳細情報について
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- CRID
- 1390010292760340480
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- ISSN
- 24242799
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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
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- 抄録ライセンスフラグ
- 使用不可