• Sumit Mori
• Y. D. Vora
• Umang Jani

Aircraft has two major components, which are fuselage and wing . An aircraft wing is a most crucial part of any aircraft that produces lift, while moving through air. As such, wings have efficient cross-sections that are subject to aerodynamic forces and act as an airfoils. The aim of this project is to study the deformation caused in the wing of a 2- seater ultra-light aircraft having NACA - 23015 airfoil profile having stringers and without having stringers and to check how much role the stringers can play in reducing the deformation of the wing. The design is done corresponding to the calculated values with the help of designing software Creo 4.0 and the analysis is done to show the structural deformations for the applied loading conditions with the help of ANSYS 19.3, also CFD is done with the help of ANSYS FLUENT (a flow analysis software) to fins the optimum AOA (Angle of Attack)

Ultra-light Aircraft, Wing Design Analysis, CAD, CFD, Creo 4.0 Ansys, Lift, Aerodynamics forces, NACA airfoil, Aircraft wing, Design optimization, Finite Element Analysis (FEA)

"Improving the design of a wing of an ultra-light aircraft and its analysis with & without stringers using CAD/CAE technologies", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.7, Issue 6, page no.919-938, June-2020, Available :http://www.jetir.org/papers/JETIR2006469.pdf

"Improving the design of a wing of an ultra-light aircraft and its analysis with & without stringers using CAD/CAE technologies", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.7, Issue 6, page no. pp919-938, June-2020, Available at : http://www.jetir.org/papers/JETIR2006469.pdf