Design & Analysis of Fuselage Structure using Solidworks & ANSYS

This paper describes a conceptual design and analysis of fuselage structure for A320 NEO (New Engine Option) aircraft by using Solidworks and ANSYS software as a design tool. Specific size, configuration arrangements, weight and performance and some commanality of features with existing A320 aircrafts are need to be considered in the design process. This conceptual design develops the first general size and configuration for a new A320 NEO aircraft fuselage structure. The model of the fuselage structure is then undergoing model analysis, linear buckling and fatigue life. In this paper structural and model analysis of A320 fuselage structure, we aim to learn the process to solve many engineering problems with the help of a solver commonly known as SPARSE directs solver which is the default solver in ANSYS without preparing the prototype model and caring the actual experiments.