Optimum design of uav wing skin structure with a high aspect ratio using variable laminate stiffness

HIGHLIGHTS

  • who: Jun-Hwan Jang and Sang-Ho Ahn from the Department of Mechanical Design, Yuhan University, Bucheon, Korea have published the Article: Optimum Design of UAV Wing Skin Structure with a High Aspect Ratio Using Variable Laminate Stiffness, in the Journal: (JOURNAL)
  • what: The authors show the stacking of a single fly, which may contain at least the thickest panel, according to consideration, and the mixing of Figure 3a can be effectively explained using guidance. In this paper, only the constraints for the first failure mode and the buckling failure length (Skin), L 250 mode . . .

     

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