Wings Aeroelastic Experimental Analysis Using Piezoelectric Materials

The study of aeroelasticity is very important for any spacecraft vehicles such as aircrafts, missiles, and helicopter rotary plates which are moved in the air, there are two phenomena discussed as follows “Divergence” and “Flutter”.  In the present work, we concentrate on the analytical and experimental analysis of wing flutter using wind tunnel testing in addition to flutter suppression using piezoelectric materials.