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Mechanical behavior of aerospace materials (200865)
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The T4 treatment for alluminum alloys corresponds to : solution + natural aging
The series 5xxx of aluminum alloys corresponds to Zn as the principal alloying element
7000 alloys are therefore used in aircraft structures required to carry higher stresses than 2000 alloys
When the aging is given at elevated temperature, is called artificial ageing
Age-hardenable alloys are characterised by their ability to be strengthened by precipitation hardening when heat treated
Types of impurities and second phase
The number of vacancies
Pores and cracks are crystalline defects