摘要: Experiments were performed in the 14- by 22-Foot Subsonic Tunnel to assess natural transition on the symmetric-airfoil wings of the NASA Juncture-Flow Model. Infrared thermography was used to visualize the heating on the upper sur... 展开
作者 | Andrew N. Leidy Michael A. Kegerise Judith A. Hannon Meelan M. Choudhari Balaji Shankar Venkatachari Pedro Paredes | ||
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作者单位 | |||
文集名称 | Computational fluid dynamics | ||
出版年 | 2023 | ||
会议名称 | AIAA SciTech Forum and Exposition | ||
页码 | 144-170 | 开始页/总页数 | 00000144 / 27 |
会议地点 | Maryland(US) | 会议年 | 2023 |
馆藏号 | P2400086 |