A passively bend-twist-coupled composite flapping wing is simulated to produce about five times more lift and 77% more thrust than a bending-only wing.
Aerodynamic performance and flow mechanism of 3D flapping wing using discrete vo rtex method,
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Lift augmentation by incorporating bend twist coupled composites in flapping wing
A passively bend-twist-coupled composite flapping wing is simulated to produce about five times more lift and 77% more thrust than a bending-only wing.