@inproceedings{e64dec8b23f44266aea6a714c9c626c4,
title = "Global pressure measurement of transonic convex corner model with vortex generators",
abstract = "This study aims to present the application of Pressure Sensitive Paint (PSP) technique to investigate a convex corner model with different heights of counter-vane vortex generators in a transonic wind tunnel. From the experimental results, the height of vortex generators that is 0.2 of boundary layer thickness can effectively postpone the occurrence of separation. By contrast, the height of which equals 1.0 boundary layer thickness can induce parasitic drag.",
author = "Chen, \{Chao Yu\} and Chen, \{Wei Chieh\} and Huang, \{Chih Yung\} and Chung, \{Kung Ming\}",
note = "Publisher Copyright: {\textcopyright} 2022, American Institute of Aeronautics and Astronautics Inc. All rights reserved.; AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022 ; Conference date: 03-01-2022 Through 07-01-2022",
year = "2022",
doi = "10.2514/6.2022-1941",
language = "English",
isbn = "9781624106316",
series = "AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA SciTech Forum 2022",
}