A Safety Design Of Aerospace Vehicle Using Numerical Analysis

Shawaluddin, Shah Fathi (2011) A Safety Design Of Aerospace Vehicle Using Numerical Analysis. Project Report. UTeM, Melaka. (Submitted)

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Abstract

This paper presents the study and a design development on force effect for aerospace vehicle during lift and drag behaviour. The main objective of this study is to design and analysis the suitable model of aerospace vehicle using numerical method. In every design of an aircraft, the analysis on the wing joints, tail and propellers of an aerospace vehicle will be very critical since these are the parts which play the major role during takeoff and landing process. All parameter of the aircraft design structure have to be considered and studied to make sure that the aircraft does not fails during airborne. Moreover, analysis on the aerodynamics of the wings and tail considering the drag and lift has to be made to the aircraft's wing design to ensure that it manage to carry the aircraft body and load airborne. In addition, designing and proposing the best designs for the wing and tail part of the aircraft have to be done to increase the safety of the aircraft during airborne generally and during takeoff and landing specifically. The first step in this study is to select an aircraft model to be analyzed theoretically on the lift and drag force acting on the aircraft during takeoff and landing followed by designing the actual and propose models of the wing and tail part using the software SolidWorks. SolidWorks is a 3D mechanical CAD (computer-aided design) program that runs on Microsoft Windows. Then the wing and tail part model that have been designed are transferred to the ABAQUS software to determine its structure tenacity when a stress is applied to get the most suitable design of wing and tail for the aircraft.

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