I have got myself all confused over some calculations
(not hard)
I have done some tensile tests on some Carbon Epoxy laminates. The purpose is to predict the max load the samples will take and compare with the actual samples performance.
The predicted values are calculated by using the Reuss & Voigt expressions.
The problem has arissen that my predicted values are way off the actual values ie over 50% more. I expected a certain difference ie 20%. I just want to check my calculations are right. So here goes:
Sample 1:
CSA of sample 1.88E-5 M2
Tensile Strength = 1570 Mpa
Tensile Modulus = 162 GPa
Ultimate Strain = 0.326
How do I calculate the max load in kN/mm2 from this info???
I have done it by multiplying Tensile strength by area = 29.516 kN
Is this right or am I missing something really obvious???