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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2019
/
Article
/
Tab 6
/
Research Article
Aerodynamic Optimization of a UAV Wing subject to Weight, Geometric, Root Bending Moment, and Performance Constraints
Table 6
,
,
and
of Case 1, Case 2, and Case 3.
Case 1
Case 2
Case 3
13
18
12
32
26
38
8520
10505
23896