• Aysha Banu M
• Archana Sreedharan
• Alkka Jayadevan
• Amalenthu G
• Balaji R

Wings are the major structural member in the aircraft which decides the performance and aero dynamical characteristic of aircraft. Several methods and mechanisms were carried out for a decade to increase the performance of aircraft in order to achieve high lift to drag ratio. They achieved better lift to drag ratio with constant wing for entire flying, but not a single aircraft runs in a mechanism where the wing area will vary according to the flying condition. Nowadays researchers are looking for the mechanism which relates the adaptive technics for different flying condition. Based on the flight operational mode the wing cross section need to vary for better performance. The object of the study is to find the better mechanism for the variable camber technology. Extensive literature has been carried out to analyse the mechanism, and different operating condition flow behaviour has been discussed. In addition aerofoils flow behaviour with respect to operational condition has been shown.

wing interference, stream line, wing morphing, interference drag,aerofoil,variable camber,morphing angle

"Review on impact of lift generation over various chord for tapper wings", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.8, Issue 6, page no.a76-a78, June-2021, Available :http://www.jetir.org/papers/JETIR2106009.pdf

"Review on impact of lift generation over various chord for tapper wings", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.8, Issue 6, page no. ppa76-a78, June-2021, Available at : http://www.jetir.org/papers/JETIR2106009.pdf