The aim of the work is to explore and justify an innovative concept in the niche of aerospace industry called as Wing
Morphing. To narrow down the study, specifically twist morphing is taken into consideration. Wings with twist and their flap
counterparts are compared in similar conditions and their aerodynamic efficiency is observed. The project implementation is
done with XFLR5, a VLM solver software. The results show that this concept brings about an improvement in the aerodynamic
efficiency without adding much to the drag penalty.