Characterization of phases, tensile properties, and fracture toughness in aircraft-grade aluminum alloys

[1] Fridlyander I.N., Aluminum alloys in aircraft in the periods of, Met Sci Heat Treat, 43, 1, pp. 5-9, (2001)

[2] Wanhill R.J.H., Fatigue crack initiation in aerospace aluminium alloys, components and structures, Natl Aerosp Lab NLR, (2007)

[3] Wei L., Pan Q., Huang H., Feng L., Wang Y., Influence of grain structure and crystallographic orientation on fatigue crack propagation behavior of 7050 alloy thick plate, Int J Fatigue, 66, pp. 55-64, (2014)

[4] Chen J., Zhen L., Yang S., Shao W., Dai S., Investigation of precipitation behavior and related hardening in AA 7055 aluminum alloy, Mater Sci Eng A, 500, 1-2, pp. 34-42, (2009)

[5] Dixit M., Mishra R.S., Sankaran K.K., Structure-property correlations in Al 7050 and Al 7055 high-strength aluminum alloys, Mater Sci Eng A, 478, 1-2, pp. 163-172, (2008)

[6] Deshpande N.U., Gokhale A.M., Denzer D.K., Liu J., Relationship between fracture toughness, fracture path, and microstructure of 7050 aluminum alloy: part I. quantitative characterization, Metall Mater Trans A Phys Metall Mater Sci, 29, 4, pp. 1191-1201, (1998)

[7] Chen J., Zhang X., Zou L., Yu Y., Li Q., Effect of precipitate state on the stress corrosion behavior of 7050 aluminum alloy, Mater Charact, 114, pp. 1-8, (2016)

[8] Liu M., Klobes B., Maier K., On the age-hardening of an Al-Zn-mg-cu alloy: a vacancy perspective, Scr Mater, 64, 1, pp. 21-24, (2011)

[9] Yang W., Ji S., Wang M., Li Z., Precipitation behaviour of Al-Zn-Mg-Cu alloy and diffraction analysis from η' precipitates in four variants, J Alloys Compd, 610, pp. 623-629, (2014)

[10] Berg L.K., Waterloo G., Schryvers D., Et al., GP-ZONES IN Al–Zn–Mg alloys and their role in artificial aging, Acta Mater, 49, 2001, pp. 3443-3451, (2001)

[1] Fridlyander I.N., Aluminum alloys in aircraft in the periods of, Met Sci Heat Treat, 43, 1, pp. 5-9, (2001)

[2] Wanhill R.J.H., Fatigue crack initiation in aerospace aluminium alloys, components and structures, Natl Aerosp Lab NLR, (2007)

[3] Wei L., Pan Q., Huang H., Feng L., Wang Y., Influence of grain structure and crystallographic orientation on fatigue crack propagation behavior of 7050 alloy thick plate, Int J Fatigue, 66, pp. 55-64, (2014)

[4] Chen J., Zhen L., Yang S., Shao W., Dai S., Investigation of precipitation behavior and related hardening in AA 7055 aluminum alloy, Mater Sci Eng A, 500, 1-2, pp. 34-42, (2009)

[5] Dixit M., Mishra R.S., Sankaran K.K., Structure-property correlations in Al 7050 and Al 7055 high-strength aluminum alloys, Mater Sci Eng A, 478, 1-2, pp. 163-172, (2008)

[6] Deshpande N.U., Gokhale A.M., Denzer D.K., Liu J., Relationship between fracture toughness, fracture path, and microstructure of 7050 aluminum alloy: part I. quantitative characterization, Metall Mater Trans A Phys Metall Mater Sci, 29, 4, pp. 1191-1201, (1998)

[7] Chen J., Zhang X., Zou L., Yu Y., Li Q., Effect of precipitate state on the stress corrosion behavior of 7050 aluminum alloy, Mater Charact, 114, pp. 1-8, (2016)

[8] Liu M., Klobes B., Maier K., On the age-hardening of an Al-Zn-mg-cu alloy: a vacancy perspective, Scr Mater, 64, 1, pp. 21-24, (2011)

[9] Yang W., Ji S., Wang M., Li Z., Precipitation behaviour of Al-Zn-Mg-Cu alloy and diffraction analysis from η' precipitates in four variants, J Alloys Compd, 610, pp. 623-629, (2014)

[10] Berg L.K., Waterloo G., Schryvers D., Et al., GP-ZONES IN Al–Zn–Mg alloys and their role in artificial aging, Acta Mater, 49, 2001, pp. 3443-3451, (2001)