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The main objective of this paper is to carry out the buffeting analysis on aircraft wing. The analyses were done for various frequency values and the deformations were captured for the corresponding frequencies. Rectangular tapered wing was selected as the object of our study. This vibrational study helps us to understand about the sizing and designing of wing on structural basis. The analyses were carried out with iterations by providing a set of previously defined frequency values. From the analysis, we can analyze that the particular design could able to provide the needed strength and stability. The model was designed using CATIA V5 designing tool and the simulations were carried out by ANSYS package.