@inproceedings{80440cf2f1b74e3da20a8e2b5faddaae,
title = "Numerical and experimental wind tunnel and flight testing of active flow control for modified NACA 643-618 airfoil",
abstract = "The previously developed modified NACA 64a-618 wing glove airfoil implemented on a one-fifth scaled Aeromot 200S Super Ximango motor glider was further investigated towards development of closed-loop active flow control. 2D numerical studies were completed at Re = 300,000 with α = 15° and Re = 64,200 with α = 8.64° with open-loop parameter studies and two closed-loop control schemes for further comparison with experimental results. Before flight-testing the wing glove with the tapered wing section and active flow control system was tested in a closed-return low-speed wind tunnel. Flight experiments were completed with a modified autopilot system to measure angle of attack while wall-pressure and active flow control state were recorded. Analysis and comparison of numerical and experimental results of open-and closed-loop active flow control with zero net mass flux and pulsed blowing actuators are presented.",
author = "Dianics, {James V.} and Ohno, {Duncan M.} and Fuggmann, {Stefan D.} and Jonas Lay and Daniel Heim and Fasel, {Hermann F.}",
note = "Funding Information: This work was funded by the Air Force Office of Scientific Research (AFOSR) under grant number FA9550-09-1-0214 with Dr. Douglas Smith serving as program manager. The authors would like to thank Josh Alexander for his help in the free flight experiments. Publisher Copyright: {\textcopyright} 2015 by James V Dianics, Duncan M. Ohno, Stefan D. Fuggmann, Jonas Lay, Daniel Heim, Hermann F. Fasel.; 53rd AIAA Aerospace Sciences Meeting, 2015 ; Conference date: 05-01-2015 Through 09-01-2015",
year = "2015",
doi = "10.2514/6.2015-1705",
language = "English (US)",
isbn = "9781624103438",
series = "53rd AIAA Aerospace Sciences Meeting",
publisher = "American Institute of Aeronautics and Astronautics Inc, AIAA",
booktitle = "53rd AIAA Aerospace Sciences Meeting",
}