Test stands are designed and built to test the performance of the structures against the targets set in the design specification. This study reports on the finite element analysis of a 20 structural frame of a wing box test stand. In this study, two types of structural analyses of the test stand are conducted which are static analysis and buckling analysis. The static analysis is conducted to determine displacements, stresses; and deflection . under static loading, whereas the buckling analysis is done to determine buckling loads and the buckling mode shape. The finite element analysis is accomplished using ANSYS/ED and ANSYS 11.0. Results from the finite element analysis were then compared with the results obtained by formulation. The mate...
The bachelor´s thesis is intent on the computation of a plane frame which is used for test the resis...
The topic of this final project is “The Analysis of SME MD3-160 Aircraft Wing Structure”. This analy...
This project aims to develop a standard design procedure to simulate the buckling and post-buckling ...
Wing box test rig is designed to hold the wing in place and keep them cantilevered so that the lift ...
The design of airplane, when plane is in the flight mode it is because of wings on both sides. While...
This project aims to develop a standard design procedure to simulate the bending behavior of thin-wa...
This project aims to develop a standard design procedure to simulate the bending behavior of thin-wa...
In this paper, deformation, Von-Mises stress, and failure analysis were carried out on a base stand ...
A lightweight box with dimension of 1200mm x 400mm x 120mm consisting of 4 ribs, 8 stringers and 2 s...
Airplanes are designed to stay aloft with the help of wings on both sides. In operation at cruising ...
In this research, a factory portal frame has been analysed by using ANSYS software. This research is...
Generally, this project is about designing a 3D Wing Box Test rig for static test using solid modell...
Construction of structures using steel as the construction material has become one of the major alte...
In this research, 3D steel frame was analyzed by manual calculation and also ANSYS program with the ...
Finite element analysis (FEA) has become an increasingly important tool in evaluating structural per...
The bachelor´s thesis is intent on the computation of a plane frame which is used for test the resis...
The topic of this final project is “The Analysis of SME MD3-160 Aircraft Wing Structure”. This analy...
This project aims to develop a standard design procedure to simulate the buckling and post-buckling ...
Wing box test rig is designed to hold the wing in place and keep them cantilevered so that the lift ...
The design of airplane, when plane is in the flight mode it is because of wings on both sides. While...
This project aims to develop a standard design procedure to simulate the bending behavior of thin-wa...
This project aims to develop a standard design procedure to simulate the bending behavior of thin-wa...
In this paper, deformation, Von-Mises stress, and failure analysis were carried out on a base stand ...
A lightweight box with dimension of 1200mm x 400mm x 120mm consisting of 4 ribs, 8 stringers and 2 s...
Airplanes are designed to stay aloft with the help of wings on both sides. In operation at cruising ...
In this research, a factory portal frame has been analysed by using ANSYS software. This research is...
Generally, this project is about designing a 3D Wing Box Test rig for static test using solid modell...
Construction of structures using steel as the construction material has become one of the major alte...
In this research, 3D steel frame was analyzed by manual calculation and also ANSYS program with the ...
Finite element analysis (FEA) has become an increasingly important tool in evaluating structural per...
The bachelor´s thesis is intent on the computation of a plane frame which is used for test the resis...
The topic of this final project is “The Analysis of SME MD3-160 Aircraft Wing Structure”. This analy...
This project aims to develop a standard design procedure to simulate the buckling and post-buckling ...