Improving Performance of Flying Wing Mini-UAV with Propeller Thrust Involved Trimming the Pitching Moment
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[1] Aydan Cavcar,et al. Optimum Range and Endurance of a Piston Propeller Aircraft with Cambered Wing , 2005 .
[2] G. Sachs. Flight Performance Issues of Electric Aircraft , 2012 .
[3] Kamran Mohseni,et al. Efficiency Analysis for Long -Duration Electric MAVs , 2005 .
[4] Lance W. Traub,et al. Range and Endurance Estimates for Battery-Powered Aircraft , 2011 .
[5] John A. Ekaterinaris,et al. Design Performance Evaluation and Optimization of a UAV , 2013 .
[6] Richard J. Foch,et al. Low Reynolds number, long endurance aircraft design , 1992 .
[7] Sergey V Shkarayev,et al. Aerodynamic Design of Micro Air Vehicles for Vertical Flight , 2008 .
[8] Pedro J. Boschetti,et al. Increasing the Lift-Drag Ratio of an Unmanned Aerial Vehicle Using Local Twist , 2008 .
[9] Falls Church,et al. Design of optimum propellers , 1994 .
[10] Lance W. Traub,et al. Experimental Investigation of a Morphable Biplane , 2012 .
[11] Timothy T. Takahashi,et al. Zero Lift Drag and Drag Divergence Prediction for Finite Wings in Aircraft Conceptual Design , 2010 .
[12] Ohad Gur,et al. Optimizing Electric Propulsion Systems for Unmanned Aerial Vehicles , 2009 .
[13] Götz Bramesfeld,et al. Small and Micro Aerial Vehicles: How Much Span is Too Much Span? , 2010 .
[14] Karl Nickel,et al. Tailless Aircraft in Theory and Practice , 1994 .