Short Title: Int. J. Mech. Eng. Robot. Res.
Frequency: Bimonthly
Professor of School of Engineering, Design and Built Environment, Western Sydney University, Australia. His research interests cover Industry 4.0, Additive Manufacturing, Advanced Engineering Materials and Structures (Metals and Composites), Multi-scale Modelling of Materials and Structures, Metal Forming and Metal Surface Treatment.
2024-10-25
2024-09-24
Abstract—The A300 is currently the largest aircraft in commercial operation and one of the most advance planes in the world. Designs of airplanes depend on their wings for flight. The wing of a airplane is one of the most important and complicated elements of a design airplane. A wing is a type of fin with a surface that produces aerodynamic force for flight through the atmosphere. When a force acts on a body, the latter will of these forces are generated by the relative movement of the air compared to the plane. The first one is the lift. This force is directed upwards and is acting perpendicular to the displacement of the wing and second one is drag. It is exerted in the direction opposed to the displacement of the plane. In this conventional type of wing is used with two material, they are AL alloy and AL alloy 7068. Because of its versatility in many flight roles and situations. It is generally not limited to certain flying levels or airspeeds and is extremely useful. The main purpose of this project is to find out which material (AL alloy and Al alloy 7068) is best suited for making wing of flight. In this the CAD model of A300 wing with spares and ribs using the modelling software CATIA V5 R20 and later we made modelling and structural analysis on wing Skelton structure by using ANSYS WORKBENCH. Index Terms—A300 flight, Conventional type wing, Aluminum alloy, Aluminum alloy 7068, Model and static structural analysis
Cite: Kakumani Sureka and Satya Meher, "Modeling and Structural Analysis on A300 Flight Wing by Using ANSYS ," International Journal of Mechanical Engineering and Robotics Research, Vol.4, No. 2, pp. 123-130, April 2015.