Experimental Study of a Ducted Contra-rotating Lift Fan for V/STOL UAV Application
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[1] Thomas Sylvester,et al. F-35B Lift Fan Inlet Development , 2011 .
[2] B. V. Oudheusden,et al. Wake structure visualization of a flapping-wing Micro-Air-Vehicle in forward flight , 2016 .
[3] Ivor Day,et al. Stall, Surge, and 75 Years of Research , 2016 .
[4] T. Mueller,et al. AERODYNAMICS OF SMALL VEHICLES , 2003 .
[5] Shuanghou Deng,et al. Experimental Investigation of Aerodynamics of Flapping-Wing Micro-Air-Vehicle by Force and Flow-Field Measurements , 2016 .
[6] R. D. Harrington,et al. Full-scale-tunnel Investigation of the Static-thrust Performance of a Coaxial Helicopter Rotor , 1951 .
[7] P. B. Sharma,et al. A Study of Some Factors Affecting the Performance of a Contra-Rotating Axial Compressor Stage , 1988 .