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Study of A Flexible Blade for Optimized Proprotor

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Academic year: 2021

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Figure

Figure 1: Airfoil characteristics of NACA0012
Figure 4: BEMT validation for propeller
Figure 5: Twist effect to small proprotor Hover Forward flight Built-in twist (degree) 10 30 Collective pitch (degree) 31 54
Figure 6: Static validation of FBEAM
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