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Experimental Study of Owl Like Airfoil Aerodynamics at Low Reynolds Numbers

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Figure

Figure 1. Airfoil section of owl-like wing (Black dash line: Test model geometry, Red dash line: Measured owl wing geometry)
Figure 2. Test model of owl wing.
Table 1. Corresponding Reynolds number and flow velocity.
Figure 4. Reynolds number dependency on aerodynamic performance. (a) Lift coeffi-cients; (b) Drag coefficients
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