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- W4387169946 abstract "Polymer matrix-fiber reinforcement composites are known for their high strength-to-weight ratio, so it is a great option to increase the efficiency of the wing structure especially for solar-powered unmanned aerial vehicles (UAVs). This research aims to examine the mechanical properties of composite materials manufactured by hand lay-up and vacuum bagging technique at room temperature, which will be the same as the in-house low-cost UAV wing production process in the coming future. Mechanical properties’ result from the coupon test based on ASTM standard is used to create a multiple web wing design with the highest load factor and a manufactured wing spar prototype in one cure cycle for sandbag testing. Spar web structure is made of polyurethane foam core and plain weave carbon fiber sandwich structure. Unidirectional carbon fiber was added to the top of the web to improve compressive strength of the wing spar. The sandbag test result of wing spar is good agreement with the calculation, the wing can withstand 1.3 safety factor and 2.5 load factor as expected." @default.
- W4387169946 created "2023-09-30" @default.
- W4387169946 creator A5037848986 @default.
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- W4387169946 date "2023-01-01" @default.
- W4387169946 modified "2023-09-30" @default.
- W4387169946 title "Design and Testing of Multiple Web Composite Wing Spar for Solar-Powered UAV" @default.
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- W4387169946 doi "https://doi.org/10.1007/978-3-031-37943-7_22" @default.
- W4387169946 hasPublicationYear "2023" @default.
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