2022
DOI: 10.1016/j.compstruct.2022.115444
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Development of a new flexible wing concept for Unmanned Aerial Vehicle using corrugated core made by 4D printing of composites

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Cited by 23 publications
(8 citation statements)
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“…The effects of environmental factors include fatigue, temperature and humidity, ultraviolet exposure [UV], biological attacks, and so forth. They are the most significant environmental degradation factors taken into consideration and can limit the utility of polymer composites by deteriorating mechanical properties during operation [82,83]. The two most significant factors that contribute to climatic deterioration are temperature and humidity.…”
Section: The Possibility Of Recycling Composite Materialsmentioning
confidence: 99%
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“…The effects of environmental factors include fatigue, temperature and humidity, ultraviolet exposure [UV], biological attacks, and so forth. They are the most significant environmental degradation factors taken into consideration and can limit the utility of polymer composites by deteriorating mechanical properties during operation [82,83]. The two most significant factors that contribute to climatic deterioration are temperature and humidity.…”
Section: The Possibility Of Recycling Composite Materialsmentioning
confidence: 99%
“…According to the review, their combination has more detrimental effects on the composite qualities than either one alone, and wetness molding allows for the adjustment of the failure mode at high temperatures. The matrix phase and potentially the interface are the primary environmental effects, whereas strands are often somewhat heartless in the molding process for polymer matrix composites [83,84].…”
Section: The Possibility Of Recycling Composite Materialsmentioning
confidence: 99%
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“…The corrugated core was made using 4D technique. The wing prototype has been tested and it has been shown that the wing can support the load for a medium-sized UAV (Hoa et al, 2022) Fuselage parts of Quadcopter unmanned aerial vehicle (Galatas et al, 2018) Continuous carbon fiber and two matrix materials -thermoset resulting in a unidirectional composite layer-bylayer CFRC 3D printing frame structure of small UAV, the mass of the frame is 75 g (Azarov et al, 2019) Low temperature pre-preg -combined with careful processing methods and carbon fibre-reinforced CNC direct mould tools 9m x 5m composite curing oven manufacture of all primary composite structures for a solar-powered UAV (wing, frame, etc.) (Richardson, 2018) *PLA -polylactic acid; PP -polypropylene; PET -polyethylene terephthalate; PA -polyamide; CFRP -High-quality carbonfiber-reinforced polymer…”
Section: Composite Materials Used In the Structure Of Uavsmentioning
confidence: 99%
“…The corrugated core was made using 4D technique. The wing prototype has been tested and it has been shown that the wing can support the load for a medium-sized UAV (Hoa et al, 2022) Continuous carbon fiber and two matrix materials -thermoset resulting in a unidirectional composite layer-bylayer CFRC 3D printing frame structure of small UAV, the mass of the frame is 75 g (Azarov et al, 2019) Low temperature pre-preg -combined with careful processing methods and carbon fibre-reinforced CNC direct mould tools 9m x 5m composite curing oven manufacture of all primary composite structures for a solar-powered UAV (wing, frame, etc.) (Richardson, 2018) *PLA -polylactic acid; PP -polypropylene; PET -polyethylene terephthalate; PA -polyamide; CFRP -High-quality carbonfiber-reinforced polymer…”
Section: Composite Materials Used In the Structure Of Uavsmentioning
confidence: 99%