Loads were calculated based on Microsoft Excel. An example of calculation of loads that acts on top chord:
Nodal load = 1.0 * ((2.114/2)+(2.360/2))*8.0
= 17.896kN
= 17.896kN
Loads were assigned to Main Truss A.
The first analysis was conducted and it yields a deflection of 76.59mm. Moreover, numerous members failed for lateral torsional buckling and plane flexural buckling. Problem was rectified, it was found that top chord was too thick, hence the next analysis was conducted it is fine.
Today, loads were assigned to the 2 dimension model of Main Truss A, Main Truss B and Main Truss C. Loads were calculated with the help of Microsoft Excel. Then checks for axial stress, lateral torsional buckling and plane flexural buckling was conducted and section assigned was adequate. After that, loads for Main Truss A, Main Truss B and Main Truss C was assigned to the 3 dimension model. Lastly loads were assigned to rafter.
Loads were assigned to the 2 dimension model of Box Truss 1, Box Truss 2, Box Truss 3, Box Truss 4 and Box Truss 5. Loads were calculated with the help of Microsoft Excel. After that, loads for Box Truss 1, Box Truss 2, Box Truss 3, Box Truss 4 and Box Truss 5 was assigned to the 3 dimension model. Supports were assigned to the 3 dimension model. Checks for axial stress, lateral torsional buckling and plane flexural buckling was conducted and section assigned was adequate.
Loads were assigned to the 3 dimension model of Main Truss A
Loads assigned to the 3 dimension model of UTAR Grand Hall
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