Numerical study of flowfield around a multislotted high-lift wing

Yuichi Kuya, Ryo Ito, Midori Maki, Keisuke Sawada

研究成果: ジャーナルへの寄稿学術論文査読

2 被引用数 (Scopus)

抄録

The objective of the present study is to understand the flowfield around the multislotted wing. Understand ing the flow characteristics around the multislotted wing is essential for further development of its concept. Two-dimensional and three-dimensional Reynolds-averaged Navier–Stokes (RANS) computations are conducted in this study. In the two-dimensional computation, the flowfield of the multislotted wing is compared with those of a three-element wing to examine the effects of the additional slots in the multislotted wing system. The three-dimensional computation is conducted to understand how the tip vortices induced around the multislotted wing affect the entire flowfield.

本文言語英語
ページ(範囲)383-389
ページ数7
ジャーナルJournal of Aircraft
58
2
DOI
出版ステータス出版済み - 2021

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