An Investigation Of The Effect Of Retrogression And Reaging (RRA) Treatment On Stress Corrosion Cracking (SCC) Of Aluminum Alloy 7075
The focus of this report is on the mechanical end corrosion properties of high-strength aluminum alloys. Aluminum alloy 7075, a common material in the aerospace industry, is susceptible to stress-corrosion cracking (SCC) in the T6, or peak-aged temper. The susceptibility of this temper to SCC is...
Internet
http://library.utem.edu.my:8000/elmu/index.jsp?module=webopac-d&action=graphicFullDisplayRetriever.jsp&szMaterialNo=0000063434http://library.utem.edu.my:8000/elmu/index.jsp?module=webopac-d&action=graphicFullDisplayRetriever.jsp&szMaterialNo=0000063434
http://eprints.utem.edu.my/3396/1/An_Investigation_Of_The_Effect_Of_Retrogression_And_Reaging_%28RRA%29_Treatment_On_Stress_Corrosion_Cracking_%28SCC%29_Of_Aluminum_Alloy_7075_-_24_pages_-_Copy.pdf
http://eprints.utem.edu.my/3396/2/An_Investigation_Of_The_Effect_Of_Retrogression_And_Reaging_%28RRA%29_Treatment_On_Stress_Corrosion_Cracking_%28SCC%29_Of_Aluminum_Alloy_7075_-_Full_Text.pdf