Study of aerodynamic interference between main wing and tail wing using 2D Building-Cube Method
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- KITA Ryuho
- Kanazawa Institute of Technology
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- SASAKI Daisuke
- Kanazawa Institute of Technology
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- SHIKADA Yusuke
- Graduate School of Engineering Kanazawa Institute of Technology
Bibliographic Information
- Other Title
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- 2次元BCMを用いた主翼―尾翼間の空力干渉の研究
Abstract
<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>
Journal
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- The Proceedings of Conference of Hokuriku-Shinetsu Branch
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The Proceedings of Conference of Hokuriku-Shinetsu Branch 2021.58 (0), E013-, 2021
The Japan Society of Mechanical Engineers
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Details 詳細情報について
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- CRID
- 1390852482512630912
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- NII Article ID
- 130008092485
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- ISSN
- 24242772
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- Text Lang
- ja
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- Data Source
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- JaLC
- Crossref
- CiNii Articles
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- Abstract License Flag
- Disallowed