UAV flight test of plasma slats and ailerons with microsecond dielectric barrier discharge<xref rid="cpb_27_10_105205fn1" ref-type="fn">*</xref><fn id="cpb_27_10_105205fn1"><label>*</label><p>Project supported by the National Natural Science Foundation of China (Grant Nos. 51336011 and 51607188), the China Postdoctoral Science Foundation (Grant No. 2014M562446), and the PhD Research Startup Foundation of Xi’an University of Technology (Grant No. 256081802).</p></fn>

UAV flight test of plasma slats and ailerons with microsecond dielectric barrier discharge**

Project supported by the National Natural Science Foundation of China (Grant Nos. 51336011 and 51607188), the China Postdoctoral Science Foundation (Grant No. 2014M562446), and the PhD Research Startup Foundation of Xi’an University of Technology (Grant No. 256081802).

Su Zhi¹, Li Jun¹, Liang Hua^{1, †}, Zheng Bo-Rui^{2, ‡}, Wei Biao¹, Chen Jie¹, Xie Li-Ke¹

(color online) Comparison between flow control effects with NS-DBD and μs-DBD, showing (a) lift coefficient curves and (b) pressure distribution curves at α = 13°.