I don't need to give any information, I just need to know the best way to calculate E from a range of values for load and displacement given the length and diameter. I've calculate it for a few values and the value appears to decrease so I'm not sure where to take the value for E from.
Mild steel will have a region where there is a linear stress-strain relationship, while there is no such region for aluminum.
Aluminum does have a linear stress-strain relationship for small strains, but unlike mild steel it doesn't have an obvious "yield point" where the linear relationship ends.
For some structural applications the maximum allowable stress for aluminum is in the nonlinear region. If the material is loaded up to that stress level, its behavior is not elastic and it does not return to its original length when unloaded. But for other applications aluminum is assumed to be a linear elastic material, with a lower stress limit.