Three dimensional computational analysis of fluid structure interaction over a finite wing

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.

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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

Item Type: Conference or Workshop Item (Paper)
Uncontrolled Keywords: Fluid Structure Interaction, CFD, Structural Analysis, 3Dimensional Flows, Finite Wing.
Subjects: Engineering > MIT Manipal > Aeronautical and Automobile
Depositing User: MIT Library
Date Deposited: 16 Dec 2015 14:42
Last Modified: 16 Dec 2015 14:43
URI: http://eprints.manipal.edu/id/eprint/144832

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