Moreto et al., 2018 - Google Patents
Effect of localized corrosion on fatigue–crack growth in 2524-T3 and 2198-T851 aluminum alloys used as aircraft materialsMoreto et al., 2018
- Document ID
- 1350213569811240300
- Author
- Moreto J
- Broday E
- Rossino L
- Fernandes J
- Bose Filho W
- Publication year
- Publication venue
- Journal of Materials Engineering and Performance
External Links
Snippet
Corrosion and fatigue of aluminum alloys are major issues for the in-service life assessment of aircraft structures and for the management of aging air fleets. The aim of this work was to evaluate the effect of localized corrosion on fatigue crack growth (FCG) resistance of the …
- 229910000838 Al alloy 0 title abstract description 51
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N2203/0058—Kind of property studied
- G01N2203/006—Crack, flaws, fracture or rupture
- G01N2203/0062—Crack or flaws
-
- C—CHEMISTRY; METALLURGY
- C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
- C22F—CHANGING THE PHYSICAL STRUCTURE OF NON-FERROUS METALS AND NON-FERROUS ALLOYS
- C22F1/00—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working
- C22F1/04—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon
- C22F1/053—Changing the physical structure of non-ferrous metals or alloys by heat treatment or by hot or cold working of aluminium or alloys based thereon of alloys with zinc as the next major constituent
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N2203/02—Details not specific for a particular testing method
- G01N2203/0202—Control of the test
- G01N2203/0212—Theories, calculations
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N2203/02—Details not specific for a particular testing method
- G01N2203/025—Geometry of the test
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N2203/0014—Type of force applied
- G01N2203/0016—Tensile or compressive
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01N—INVESTIGATING OR ANALYSING MATERIALS BY DETERMINING THEIR CHEMICAL OR PHYSICAL PROPERTIES
- G01N2203/00—Investigating strength properties of solid materials by application of mechanical stress
- G01N2203/0058—Kind of property studied
- G01N2203/0069—Fatigue, creep, strain-stress relations or elastic constants
Similar Documents
Publication | Publication Date | Title |
---|---|---|
Moreto et al. | Effect of localized corrosion on fatigue–crack growth in 2524-T3 and 2198-T851 aluminum alloys used as aircraft materials | |
Gao et al. | Fatigue life of 7075-T651 aluminium alloy treated with vibratory stress relief | |
El May et al. | Modelling of corrosion fatigue crack initiation on martensitic stainless steel in high cycle fatigue regime | |
Cavalcante et al. | Fatigue crack propagation of aeronautic AA7050-T7451 and AA2050-T84 aluminum alloys in air and saline environments | |
Puchi-Cabrera et al. | Flow stress and ductility of AA7075-T6 aluminum alloy at low deformation temperatures | |
Shuey et al. | Experimental and analytical investigations on plane strain toughness for 7085 aluminum alloy | |
Frodal et al. | Influence of pre-compression on the ductility of AA6xxx aluminium alloys | |
Khan et al. | Experimental and numerical lifetime assessment of Al 2024 sheet | |
Moazam et al. | Ring-core integral method to measurement residual stress distribution of Al-7075 alloy processed by cyclic close die forging | |
Rader et al. | Plastic deformation and ductility of AA7075 and AA6013 at warm temperatures suitable to retrogression forming | |
Ali et al. | Computational model of mechano-electrochemical effect of aluminum alloys corrosion | |
Tuchscheerer et al. | Hydrogen-induced embrittlement of fine-grained twin-roll cast AZ31 in distilled water and NaCl solutions | |
Imantalab et al. | Strengthening mechanisms and electrochemical behavior of ultrafine-grained commercial pure copper fabricated by accumulative roll bonding | |
Lin et al. | Effects of severe cold rolling on exfoliation corrosion behavior of Al-Zn-Mg-Cu-Cr alloy | |
Harzheim et al. | Corrosion phenomena and fatigue behavior of clinched joints: Numerical and experimental investigations | |
Jafarlou et al. | Evaluation of the mechanical properties of AA 6063 processed by severe plastic deformation | |
Tomczyk et al. | Experimental investigations and damage growth modeling of EN‐AW 2024 aluminum alloy under LCF loading accounting creep pre‐deformation | |
Siddiqui et al. | Yield locus and texture evolution of AA7475-T761 aluminum alloy under planar biaxial loading: An experimental and analytical study | |
Ghosh et al. | Effect of temper condition on the corrosion and fatigue performance of AA2219 aluminum alloy | |
Huang et al. | Effect of ultrasonic impact treatment on corrosion fatigue performance of friction stir welded 2024-T4 aluminum alloy | |
Kumar et al. | Investigation of mechanical properties and fracture simulation of solution-treated AA 5754 | |
Agius et al. | Cyclic elastoplastic performance of aluminum 7075-T6 under strain-and stress-controlled loading | |
Ao et al. | Unexpected stress corrosion cracking improvement achieved by recrystallized layer in Al-Zn-Mg alloy | |
Sunar et al. | A research on the effect of retrogression and re-aging heat treatment on hot tensile properties of AA7075 aluminum alloys | |
Asquith et al. | Evaluation of residual stress development at the interface of plasma electrolytically oxidized and cold-worked aluminum |