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Design, development and testing of shape shifting wing model

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Figure

Figure 1.Figure 1. (a) The finished 3D printed conventional wing aerofoil model; ( (a) The finished 3D printed conventional wing aerofoil model; (b) The finished 3D printed b) The finished 3D printedoptimized morphing aerofoil model.
Figure 11. The flow domains geometry. Figure 11. The flow domains geometry.
Figure 15.a( Images showing the vortex size for the conventional wing (es showing the vortex size for the conventional wing () at 0 degrees’ angle of attack a) at 0 degrees’ angle of attackb) at 5 degrees’ angle of attack.
Figure 16 shows the coefficient of lift data generated by Ansys, a significant increase in coefficientof lift when comparing the initial morphing wing and conventional wing.
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