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Aeroelastic study of bistable composite airfoils
S. Daynes
,
P. M. Weaver
, K. D. Potter
University of Bristol
Research output
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peer-review
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Engineering
Bistables
100%
Airfoil
100%
Aerodynamic Load
66%
Flaps
50%
Rotor Blade
16%
Actuator System
16%
Trailing Edge
16%
Equilibrium Point
16%
Test Machine
16%
Foam Tape
16%
Actuator
16%