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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2016
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Article
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Tab 6
/
Research Article
Aerodynamic Optimization Based on Continuous Adjoint Method for a Flexible Wing
Table 6
Optimization results of flexible wing.
Parameter
Before design
After design
Δ%
0.5815
0.5807
0.02237
0.02186
26.0
26.6
2.3%