Design and Analysis of General Aviation Aircraft Wings Using Different Materials
Anuj Shankar Rai, Ashish Gupta , Manu Kumar
An aircraft produces lift using its wings, while gliding through air. Through the geometry, wings have efficient cross-sections that are subjected to lift and drag forces and it act as an airfoil. In this thesis work, it is investigated how modelling and simulating softwares can be used in the early stages of an aircraft design process, especially for the design of an aircraft wing and its structural entities like wing spars and wing ribs. The domain of this research has been restricted to the engineering design of the wing and its analysis, as it plays a vital role in the generation of lift required by an aircraft. The main purpose of this project is to determine the material most suitable for wings structure. The wing is designed in CAD and the analysis is done ANSYS. Static structural analysis of the wing is done to find deformation, stress and FOS.
Article Details
Unique Paper ID: 159812

Publication Volume & Issue: Volume 9, Issue 12

Page(s): 797 - 808
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