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Optimization Of Unmanned Aerial Vehicle Wing Structure

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Figure

TABLE 1 (b) MAIN CHARACTERISTICS OF THE WINGS
TABLE 2- RESULTS OF RECTANGULAR WING MATERIAL COMPOSITION MAX. VON
FIG 3 VON MISES STRESS FOR COMPOSITION 1 (5×4)
FIG 5 VON MISES STRESS FOR COMPOSITION 2 (5×4)
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