Depending on which source you consult, the expected value is betwen 120 and 130 Gpa. On the net it is possible to find the answer in psi (pounds per square inch) but I assume you require a value in SI units. We have just done a classroom experiment which returned a value of about 80 GPa. The stress strain graph looked like a typical ductile material graph, straght line followed by a curve as defopration became plastic. Our value was obtained using the eleastic straight line section. I suspect our low value was due to some 'give' in the anchorage of the specimen wire.
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That depends on the temper ( heat treat). For anneled condition (T0) it is 8000 psi and for T6 condition, which is usual specification, it is 35,000 psi. It is in between those values for other tempers between T1 and T5
10.5 million psi at 21 deg C, goes down with temperature. See: http://www.engineeringtoolbox.com/young-modulus-d_773.html
the young's modulus of aluminium is 0.675 * 105
this can also be called as the modulus of elasticity
It depends on the heat treat and type but in general modulus is the same as most all aluminum - around 10.2 million psi or 70.3 GPa
7075 is stronger than 6061 aluminum.
6061 T6 is a specific temper designation for aluminum alloy 6061, indicating that it has been solution heat-treated and artificially aged to achieve a certain level of strength. On the other hand, AMS4027 is a specification set by the Society of Automotive Engineers (SAE) that outlines the requirements for aluminum alloy 6061 in the form of sheet and plate. In summary, 6061 T6 refers to the specific treatment of the alloy, while AMS4027 refers to the industry standard specification for the material in a particular form.
That will depend on how it is heat treated and the material type. For example 6061 T6 has an ultimate of 42,000 psi but 6061 annealed is only 18,000 psi. Aluminum 7075 is 80,000 psi heat treated to T6 temper and 33,000 psi annealed.