Kinematic and aerodynamic modeling of flexible wings with wing root adjustment for flapping wing micro aerial vehicles.

Sci Rep · 2026 · PMC13018484 · PMID 41714697

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a decreasing trendno p-value reported

According to the variation law of the lift and drag coefficient 57 , when the attack angle exceeds the critical value of , the lift coefficient shows a decreasing trend while the drag coefficient continues to increase.

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