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. |
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Page 297
... ARALL has been flying in the lower wing of a Fokker - 50 prototype commercial transport aircraft [ 14 ] , and Fokker and other airframers are evaluating ... ARALL - 2 is intended 10 ARALL LAMINATES 297 Commercial ARALL Laminate Product Forms.
... ARALL has been flying in the lower wing of a Fokker - 50 prototype commercial transport aircraft [ 14 ] , and Fokker and other airframers are evaluating ... ARALL - 2 is intended 10 ARALL LAMINATES 297 Commercial ARALL Laminate Product Forms.
Page 303
... Laminate ( 3/2 lay - up , 0.053 inch thick ) , aramid - epoxy prepreg and 7075 - T6 sheet . properties ; however , the isotropic aluminum is advantageous when loading is multidirectional . ARALL Laminate yield ... ARALL LAMINATES 303.
... Laminate ( 3/2 lay - up , 0.053 inch thick ) , aramid - epoxy prepreg and 7075 - T6 sheet . properties ; however , the isotropic aluminum is advantageous when loading is multidirectional . ARALL Laminate yield ... ARALL LAMINATES 303.
Page 313
... ARALL - 1 and -3 panel toughness re- sponse is considerably less than that exhibited by the ARALL - 2 panel results [ 6,21 ] . Though more work needs to be done , ARALL Laminate Kc values can be estimated from the available center ...
... ARALL - 1 and -3 panel toughness re- sponse is considerably less than that exhibited by the ARALL - 2 panel results [ 6,21 ] . Though more work needs to be done , ARALL Laminate Kc values can be estimated from the available center ...
Contents
J T Staley 2 I AlMn Alloys | 4 |
AlCu Alloys | 6 |
AlMgSi Alloys | 12 |
Copyright | |
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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