Aluminum Alloys--contemporary Research and ApplicationsAsuri K. Vasudevan, Roger Davidge Doherty This book discusses the structure and properties of the current and potential aluminum alloys in terms of their structure (and structural transformations by new processing methods) and the relationship between structure and mechanical and other properties. The alternative materials that challenge aluminum are considered as well, since the challenge of new competitive materials is a strong influence on innovation. The book bridges the gap between current scientific understanding and engineering practice. It is an up-to-date reference that will be of use to researchers and advanced students in metallurgy and materials engineering. |
From inside the book
Results 1-3 of 63
Page 58
... temper , and most 7XXX alloys are used in either the T6 or T7 tempers . Peak strength is normally obtained by aging for various times , usually up to 24 hours , at temperatures ranging from 388 to 403K . The T73 and T76 overaged tempers ...
... temper , and most 7XXX alloys are used in either the T6 or T7 tempers . Peak strength is normally obtained by aging for various times , usually up to 24 hours , at temperatures ranging from 388 to 403K . The T73 and T76 overaged tempers ...
Page 90
... temper ( 2 hrs @ 343 ° C ) " O " Grain Size Mg Mn Yield Tensile ΕΙ Yield Tensile ΕΙ ( wt % ) ( wt % ) ( MPa ) ( MPa ) ... temper sheet dropped below the initial yield strength of the H16 temper . Tensile strength ( MPa ) Yield strength ...
... temper ( 2 hrs @ 343 ° C ) " O " Grain Size Mg Mn Yield Tensile ΕΙ Yield Tensile ΕΙ ( wt % ) ( wt % ) ( MPa ) ( MPa ) ... temper sheet dropped below the initial yield strength of the H16 temper . Tensile strength ( MPa ) Yield strength ...
Page 91
... Temper O - H16 Temper A - H14 Temper A - H18 Temper 500 -H18 -H16 450 400 -M14 -M12 350 300 450 -H18 400 -H16 350 -H12 300 Elongation ( % ) 250 200 150 20 10 .1 1 yr . 17 yr . 10 100 1000 10,000 Time at room temperature , days FIG . 20 ...
... Temper O - H16 Temper A - H14 Temper A - H18 Temper 500 -H18 -H16 450 400 -M14 -M12 350 300 450 -H18 400 -H16 350 -H12 300 Elongation ( % ) 250 200 150 20 10 .1 1 yr . 17 yr . 10 100 1000 10,000 Time at room temperature , days FIG . 20 ...
Contents
J T Staley 2 I AlMn Alloys | 4 |
AlCu Alloys | 6 |
AlMgSi Alloys | 12 |
Copyright | |
69 other sections not shown
Other editions - View all
Common terms and phrases
2XXX 5XXX 7XXX Acta addition aging aircraft Al-Li alloys Al-Mg Alcoa alloys containing aluminum alloys Aluminum-Lithium Alloys annealing applications ARALL Laminate ARALL-1 atomization behavior coarsening commercial Composite Materials constituent crack growth deformation density dislocation dispersoid ductility E.A. Starke effect elongation extrusion fatigue crack fibers formability fracture toughness grain boundaries grain growth heat heat-treatable high-strength hydrogen increase ingot interface intermetallic lithium magnesium matrix mechanical properties metal Metallurgy microstructure modulus mold nucleation occurs oxide particles phase PM alloys powder powder-metallurgy precipitates precipitation-hardening produced quenching rapid solidification Rapidly Solidified recrystallized grain reduced reinforced resistance rolling shear sheet shown in Fig shows solid solution strain rate strain-hardening strengthening stress corrosion structure subgrain superplastic superplastic forming surface T.H. Sanders T₁ temperature tensile strength texture thermal thermomechanical tion TMS-AIME Trans V₁ volume fraction Warrendale welding whisker yield strength zones