@inproceedings{fabe47143ff9474b859a5fd313113f65,
title = "Flow field on wing surface with control surface in propeller slipstream at low reynolds number",
abstract = "An experimental study is conducted on a NACA0012 airfoil with a control surface to investigate an influence of a propeller slipstream under low Reynolds number condition. To investigate the influence of the propeller slipstream on a wing surface, a flow field on the wing surface is visualized using the Temperature-Sensitive Paint at the chord-based Reynolds number of 3.0×104. Control surface performance improves in the propeller installed condition because laminar separation bubble is suppressed by the propeller slipstream. Finally, we suggest the propeller should be installed ahead of the control surface to use the effect of the propeller slipstream under low Reynolds number flight condition.",
author = "Tsubasa Ikami and Kensuke Kanou and Koichi Takahashi and Koji Fujita and Hiroki Nagai",
year = "2019",
month = jan,
day = "1",
doi = "10.2514/6.2019-2159",
language = "English",
isbn = "9781624105784",
series = "AIAA Scitech 2019 Forum",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "AIAA Scitech 2019 Forum",
note = "AIAA Scitech Forum, 2019 ; Conference date: 07-01-2019 Through 11-01-2019",
}