Fluid-Structure Interaction of Cropped Delta Wing with Experimental Validation

Abstract

Fluid-structure interaction (FSI) is the commerce between a flexible structure and the surrounding fluid gives a variety of phenomenon. Application of this phenomenon in many areas like vibrational analysis of aircraft wings, machinery, bridges, etc. This computational analysis leads to many aerodynamic and structural dynamicproblems. In the present article, we review the structural analysis of cropped delta wing aircraft with fence and without the fence . One of the key aspects of developing a better design from the data collected by FCI. Several such techniques are reviewed in this paper. As a part of this work, the experimental model setup for analysis the cropped delta wing by using wind tunnel and validate with software analysis values. The model of a cropped delta wing with the fence at different Mach number and angle of attack are selected to high spot the futuristic of computational problems.