Shivaprasad, U and Reddy, Sree Vaibhav KM (2015) Three dimensional computational analysis of fluid structure interaction over a finite wing. In: Proceedings of International Conference on Mechanical and Aeronautical Engineering, July 15-16, 2015.

PDF Display7Pdf.pdf - Published Version Restricted to Registered users only Download (993kB) | Request a copy

Abstract

The present study emphasizes on interaction between the lifting structure and the fluid flow i.e. submerged flow a wing results in various dynamic phenomenal changes. The traditional analysis of a flow field around a finite wing assumes that the lifting body is rigid and doesn’t experience any deformation. This study utilizes fluid structure interaction principles to compute and define the structural stability of the modern aircraft wings namely Cessna 172, Boeing 737 and Glaser-dirks dg-808 glider. The above aircrafts have been considered due to their unique wing design and diversified characteristics. The study has been conducted using the commercial software ANSYS Inc. and the results will be presented based on Fluid Structure Interaction in the context of aerodynamic behaviour of the wing

Actions (login required)

View Item