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- W2392763863 abstract "In this paper,structure of Zephyr7 UAV wing will be analyzed with software of ABAQUS.Especially,the effects of the diameter of beam and the pretension of wing skin on the resistance to flexural capacity and resistance to torsional capacity of the wing.The results of analysis show that the resistance of flexural capacity and resistance to torsional capacity of the main beam exponential growth when the diameter increase,the resistance to flexural capacity of the wing growth linearly when the pretension of wing skin increase." @default.
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- W2392763863 date "2012-01-01" @default.
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- W2392763863 title "Mechanical performance analysis on wing's of Zephyr7 UAV" @default.
- W2392763863 hasPublicationYear "2012" @default.
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