I need to calculate the stresses in a composite slab made from glass, concrete and steel and I transformed the glass and concrete into the equivalent area of steel using modular ratios.
Using excel, I calculated the position of the neutral axis and then applied the parallel axis theorem to obtain the transformed inertia.
To check my answer, I drew the transformed section in AutoCAD and checked the properties using the Mass Properties Enquiry Tool. The position of the Neutral Axis was ok and so was the transformed Area but I cannot confirm the Transformed Inertia. Using Excel I obtain 5.492E7mm4 and the AutoCAD check gave 3.432E6mm4.
I attach three PDFs showing my results.
Would anyone be able to point out my error, please?
Using excel, I calculated the position of the neutral axis and then applied the parallel axis theorem to obtain the transformed inertia.
To check my answer, I drew the transformed section in AutoCAD and checked the properties using the Mass Properties Enquiry Tool. The position of the Neutral Axis was ok and so was the transformed Area but I cannot confirm the Transformed Inertia. Using Excel I obtain 5.492E7mm4 and the AutoCAD check gave 3.432E6mm4.
I attach three PDFs showing my results.
Would anyone be able to point out my error, please?