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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2016
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Article
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Tab 4
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Research Article
Aerodynamic Optimization Based on Continuous Adjoint Method for a Flexible Wing
Table 4
Optimization results of ONERA M6.
Parameter
Before optimization
After optimization
Δ%
0.2903
0.29
0.01417
0.01059
20.49
27.38
33.63%