Design and Analysis of an Aircraft Wing Structure
Structural design plays a major role in the design of any aircraft or spacecraft. The wing analysis is important in aircraft design as wings undergo various loads and stresses. The objective of present work is to determine wing structural loading for a conventional aircraft and perform its structural analysis. Schrenk’s curve has been plotted and load distribution over the wingspan has been calculated and tabulated. Bending moment, shear force and torque calculations for the conventional aircraft wing has been performed at different wing stations and the detailed results are presented.