Metals exibit Elastic and Plastic deformation. Steels have a large elastic region, e.g. steel has a lower slope (Young's Modulus) of the elastic region in a stress versus strain curve (stress being force/cross-sectional area and strain being change in length/initial length). The elastic region is the region where a material can be stretched and it will shrink back to it's original size. The Plastic region is where there is permanenet deformation. Aluminum has a very small elastic region which means that every time it stretches it is essentially a permanent change in length (Young's Modulus starts to approach infinity). As forces are imparted on a piece of aluminum, it will continue to stretch until failure. This is why aluminum aircraft will suddenly loose a section of the fuselage after so many years of operation (cyclic use causes failure). Aluminum has a very strong strength to weight ratio but would need to be much thicker than steel to be able to withstand the same forces without fracturing due to load cycles (fatigue). You could make it the same thickness as steel but it would have a much shorter life cycle. This is a very basic background.
Here is a link with some tensile testing background:
http://www.instron.us/wa/applications/test...on/default.aspxThanks for the tips.I may try the steel diamond plate.I was planning on a parkerized finish anyhow so the shiny alum. type would have had no use.
SUBTOPIC: Why is it illegal to sell a kit gun?
One thing they don't add about the curves is that it seems the material will reach a maximum strength (Ultimate Tensile Strength - UTS) and then begin to loose strength. This is not the case. In reality the material has started to thin due to the ductile nature of metals and is essentially still increasing in stress versus strain. The stress is usually define as the force/cross-sectional area. As the cross-sectional area decreases the force can decrease and the strain can still go up. The stress in these curves isn't corrected for this thinning. It can be corrected by measuring the thickness of the sample following fracture and correcting the stress at the fracture point. If you graph this point on the stress versus strain curve you would actually see the stress continue to rise as the material is strained.
Also, temperature has a big impact on materials. Ductile materials at normal temps. will start to show brittle deformation at lower temps. The ductile transition temperature is dependant upon the material.