Fluid-structure interaction methodology to analyse flutter effect on supersonic sheet metal wing design

Computational fluid dynamics and Static structural analysis were performed on the customized sheet metal design of an aircraft wing flying at an altitude of 1500m from the surface of the earth with Mach 2 in order to study the structural behaviour of wing especially to observe the flutter effect/self exciting oscillation under steady aerodynamic condition. The analysis performed here were of steady aerodynamic conditions.

This data provides a vivid picture on how the analysis has been performed from the scratch. The data enclosed in this files ensure precision in its results. The results obtained by flutter analyses under steady aerodynamic condition was similar to the ones tested under Unsteady aerodynamic conditions.