FAI Record ID No. 16052, Federation Aeronautique Internationale.
R. Laurenzo, "Soaring on a Solar Impulse," Aerospace America, Vol. 47, No. 5, 2009, pp. 32-36.
B. H. Lee, P. M. Park, K. B. Kim, and B. J. Cha, "A Study on Optimum Takeoff Time of the Hybrid Electric Powered Systems for a Middle Size UAV," Journal of The Korean Society Aeronautical and Space Sciences, Vol. 40, No. 11, 2012, pp. 940-947.
P. M. Park, K. B. Kim, and B. J. Cha, "Flight Test of Hybrid Propulsion System for Electrically Powered UAV," Journal of the Korean Society of Propulsion Engineers, Vol. 17, No. 4, 2013, pp. 49-55.
W. J. Jin, Y. G. Lee, C. W. Kim, S. M. Ahn, and D. S. Lee, "Computational Analysis of Aerodynamic Performance of a small-scale Electric Aerial Vehicle," Proceeding of the 2010 Korean Society for Aeronautical & Space Sciences (KSAS) Fall Conference, Vol. 1, 2010, pp. 473-476.
Y. G. Lee, W. J. Jin, S. M. Ahn, and D. S. Lee, "Numerical and In-Flight Drag Estimation of a Small Electric Aerial Vehicle," Proceeding of the 2011 Korean Society for Aeronautical & Space Sciences (KSAS) Spring Conference, Vol. 1, 2011, pp. 839-844.
M. Drela, and H. Youngren, XFOIL 6.94 User Guide, Massachusetts Institute of Technology, Cambridge, MA, URL: http://web.mit.edu/drela/Public/web/xfoil/, 2001.
M. S. Selig, J. J. Guglielmo, A. P. Broeren, and P. Giguere, Summary of Low-Speed Airfoil Data, Vol. 1, Soar Tech Publications, Virginia Beach, 1995.
C. A. Lyon, A. P. Broeren, P. Giguere, A. Gopalarathnam, and M. S. Selig, Summary of Low-Speed Airfoil Data, Vol. 3, Soar Tech Publications, Virginia Beach, 1998.
ANSYS FLUENT Ver. 12 Software Package, Ansys Fluent Inc., Canonsburg, PA, USA.
GAMBIT Software Package, Ver. 2.4.6, Ansys Fluent Inc., Canonsburg, PA, USA.
TGRID Ver. 3.5, Ansys Fluent Inc., Canonsburg, PA, USA.
G. W. Stickle, and J. L. Crigler, Propeller Analysis from Experimental Data, NACA Technical Report-712, 1941.
Advanced Aircraft Analysis Software Package, Ver. 3.2, DARCorporation, Lawrence, KS, USA.
W. J. Jin, and Y. G. Lee, "Computational Analysis of the Aerodynamic Performance of a Long-Endurance UAV," International Journal of Aeronautical and Space Sciences, Vol. 14, No. 4, 2014, pp. 374-382.
H. H. Heyson, G. D. Riebe, and C. L. Fulton, Theoretical Parametric Study of the Relative Advantages of Winglets and Wing-tip Extension, NASA Technical Paper, 1977.
R. Babigian, and S. Hayashibara, "Computational Study of the Vortex Wake Generated by a Three-Dimensional Wing with Dihedral, Taper, and Sweep," AIAA Paper 2009-4107, Jun. 2009.
"Drag and Pressure Recovery Characteristics of Auxiliary Inlets at Subsonic Speeds," ESDU International PLC, London, UK, 1986.
D. P. Raymer, Aircraft Design: A Conceptual Approach, the 4th edition, AIAA Education Series, AIAA Inc., Reston, 2006.
P. M. Park, O. S. Hwang, Y. M. Kim, C. T. Kim, and K. J. Kwon, "Wind Tunnel Test on Propellers for Middle Size Electric Propulsion UAV," Proceeding of the 2011 Korean Society of Propulsion Engineers (KSPE) Fall Conference, Vol. 1, 2011, pp. 784-788.