Structural Analysis of a Composite Target-drone |
Park, Yong-Bin
(Research Center for Aircraft Parts Technology, Department of Aerospace Engineering, Gyeongsang National University)
Nguyen, Khanh-Hung (Research Center for Aircraft Parts Technology, Department of Aerospace Engineering, Gyeongsang National University) Kweon, Jin-Hwe (Research Center for Aircraft Parts Technology, Department of Aerospace Engineering, Gyeongsang National University) Choi, Jin-Ho (Research Center for Aircraft Parts Technology, Department of Aerospace Engineering, Gyeongsang National University) Han, Jong-Su (Micro Enginering) |
1 | Frulla, G. and Cestino, E. (2008). Design, manufacturing and testing of a HALE-UAV structural demonstrator. Composite Structures, 83, 143-153. DOI ScienceOn |
2 | Gadomski, J., Hernik, B., and Goraj, Z. (2006). Analysis and optimisation of a MALE UAV loaded structure. Aircraft Engineering and Aerospace Technology, 78, 120-131. DOI ScienceOn |
3 | Romeo, G. (1998). Manufacturing and testing of graphiteepoxy wing box and fuselage structures for a solar powered UAV-HAVE. Proceeding of the 21st International Council of the Aeronautical Sciences Congress, Melbourne, Australia. pp. 98-31591. |
4 | Romeo, G. (1999). Numeical analysis, manufacturing and testing of advanced composite structures for a solar powered airplane. Proceeding of the 15th AIDAA Congress (Italian Association of Areonautics and Astronautics), Torino, Italy. pp. 1001-1012. |
5 | Romeo, G. and Frulla, G. (1995). Analysis of an advanced composite wing structure for a solar powered airplane. Proceeding of the 13th AIDAA Congress (Italian Association of Areonautics and Astronautics), Roma, Italy. pp. 965-976. |
6 | Romeo, G., Frulla, G., Cestino, E., and Corisino, G. (2003). HELIPLAT: manufacturing and structural design of UAV scaled prototype. Proceeding of the 17th AIDAA Congress (Italian Association of Areonautics and Astronautics), Rome, Italy. pp. 569-578. |
7 | US Forest Products Laboratory. (1964). Bending Strength and Stiffness of Plywood. Madison, WI: US Department of Agriculture Forest Service Forest Products Laboratory. |
8 | US Forest Products Laboratory, Doyle, D. V., Drow, J. T., and McBurney, R. S. (1962). Elastic Properties of Wood: the Young’s Moduli, Moduli of Rigidity, and Poisson’s Ratios of Balsa and Quipo [Report no. 1528]. Madison, WI: US Department of Agriculture, Forest Service, Forest Products Laboratory. |
9 | Young, D. W. (1986). Aircraft landing gears-the past present, and future. Proceedings of the Institution of Mechanical Engineers Part D, Transport engineering, 200, 75-92. DOI |
10 | ASTM International (2003). ASTM D3039/D3039M-08 Standard Test Method for Tensile Properties of Polymer Matrix Composite Materials. West Conshohocken, PA: ASTM International. DOI: 10.1520/D3039_D3039M-07. DOI |
11 | ASTM International (2003). ASTM D5379/D5379M-05 Standard Test Method for Shear Properties of Composite Materials by the V-Notched Beam Method. West Conshohocken, PA: ASTM International. DOI: 10.1520/D5379_D5379M-05. DOI |
12 | Cestino, E. (2006). Design of solar high altitude long endurance aircraft for multi payload & operations. Aerospace Science and Technology, 10, 541-550. DOI ScienceOn |
13 | Federal Aviation Administration (FAA). FAR Part 23--Airworthiness standards: normal, utility, and acrobatics, and commuter category airplanes. http://www.flightsimaviation.com/data/FARS/part_23.html. |