The design of an aircraft or an aircraft part (in this case, we will be referring to the wing) is a prolonged process that has mainly three phases; The first is the conceptual design phase, and it is the phase that we have employed here, this phase deals with the layout of the aircraft/aircraft part and what major characteristics it must have in order to achieve its design goals, if the conceptual design is to be a success no major changes should be implemented on it in future phases. Hence, the conceptual design engulfs the major characteristic of the aircraft while delivering a layout of its major components. The second and third phases of the design process are the preliminary and detail design phases; these phases deal with the analysis of the aircraft components in all major aspects of aerospace such as structures, dynamics, control and others. In this project modelling and structural analysis on wing is performed in ANSYS WORKBENCH. Structural analysis of the wing is carried out to compute the stresses due to pressure and various loads.