Hybrid Immersed Boundary Method for Airfoils with a Trailing-Edge Flap

标题
Hybrid Immersed Boundary Method for Airfoils with a Trailing-Edge Flap
作者
关键词
-
出版物
AIAA JOURNAL
Volume 51, Issue 1, Pages 30-41
出版商
American Institute of Aeronautics and Astronautics (AIAA)
发表日期
2012-11-23
DOI
10.2514/1.j051446

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