2006
DOI: 10.4028/www.scientific.net/msf.519-521.1323
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Evaluation of AA 2050-T87 Al-Li Alloy Crack Turning Behaviour

Abstract: Crack turning or delamination behavior of AA 2050-T87 and AA 7050-T7451 ESE(T) and hourglass coupons under cyclic fatigue conditions is presented. Fatigue crack growth rate curves, fracture surface examinations, and the preferred manner of crack growth for each alloy are discussed in an effort to better understand fatigue crack growth behavior of aluminum-lithium alloys in structural components under service conditions.

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Cited by 11 publications
(3 citation statements)
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“…Compare to conventional Al alloys, they typically possess lower density, higher elastic modulus and improved fatigue crack growth resistance. 2050 alloy is one of the 3rd generation AleLi alloys targeting static and fatigue properties to be equal or better than 7050 alloy with 4% density reduction and 5% elastic modulus enhancement [1]. Heretofore, 2050 AleLi alloy has many applications in transport aircraft from wing spars and ribs to other internal structures in wings and fuselages [2].…”
Section: Introductionmentioning
confidence: 99%
“…Compare to conventional Al alloys, they typically possess lower density, higher elastic modulus and improved fatigue crack growth resistance. 2050 alloy is one of the 3rd generation AleLi alloys targeting static and fatigue properties to be equal or better than 7050 alloy with 4% density reduction and 5% elastic modulus enhancement [1]. Heretofore, 2050 AleLi alloy has many applications in transport aircraft from wing spars and ribs to other internal structures in wings and fuselages [2].…”
Section: Introductionmentioning
confidence: 99%
“…Así mismo, la presencia de Li disminuye el peso de la aleación en aproximadamente 3% en comparación con las otras aleaciones de aluminio (Crill et al, 2006;Warner, 2006;Li et al, 2008;Guérin et al, 2015). Dentro de este grupo de aleaciones, se destaca la aleación AA2050-T8 que, debido a su excelente combinación de resistencia, densidad, resistencia a la fatiga, estabilidad térmica y tenacidad, se ha convertido en candidata atractiva en aplicaciones aeronáuticas que requieren alta resistencia específica y excelente tolerancia al daño (Lequeu et al, 2010;Malard et al, 2015;Li et al, 2016).…”
Section: Introductionunclassified
“…One of the most complex examples of orthotropic behaviour is the macroscopically anomalous crack paths in high strength Al-Li based [3][4][5][6][7][8] and Al-Zn-Mg based alloys [9,10] under fatigue loading conditions, see Figure 1 (Al-Cu-Li alloy AA2297-T8) and Figure 2 (AA7050-T651 plate). The lack of a fully verified model for this behaviour hampers efficient design with these materials [11], leading to overly conservative designs, or avoidance of materials exhibiting the strongest orthotropic behaviour.…”
Section: Introductionmentioning
confidence: 99%