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Figure 9: Micro air vehicle model with flexible cambering wings [10]. Figure 8: Micro air vehicle model with flapping wings [9].

Figure 9 Micro air vehicle model with flexible cambering wings [10]. Figure 8: Micro air vehicle model with flapping wings [9].

Related Figures (9)

Figure 1: Dynamic stall development on a transiently pitching airfoil [3].
Figure 1: Dynamic stall development on a transiently pitching airfoil [3].
Figure 2: The Karman vortex street behind a stationary airfoil [6].
Figure 2: The Karman vortex street behind a stationary airfoil [6].
Figure 3: Development of a vortex street behind a harmonically plunging airfoil [6].
Figure 3: Development of a vortex street behind a harmonically plunging airfoil [6].
Figure 4: Time-averaged jet flow behind a harmonically plunging airfoil [9].
Figure 4: Time-averaged jet flow behind a harmonically plunging airfoil [9].
Figure 6: The wind tunnel arrangement of a flapping-wing model [9]. Figure 5: The flapping-wing wind tunnel test model [9].
Figure 6: The wind tunnel arrangement of a flapping-wing model [9]. Figure 5: The flapping-wing wind tunnel test model [9].
Figure 7: Thrust measurements for a flapping-wing model [9].
Figure 7: Thrust measurements for a flapping-wing model [9].
Figure 10: Static thrust measurements as a function of flapping frequency [10]. 704 FLOW PHENOMENA IN NATURE
Figure 10: Static thrust measurements as a function of flapping frequency [10]. 704 FLOW PHENOMENA IN NATURE
Related topics:
Aerospace EngineeringAerodynamicsWind TunnelAngle-of-attack
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