Author:
Lavrov A. V.,Mitrakov O. V.,Davydenko A. N.,Yastrebov A. S.
Reference28 articles.
1. Aviation Rules. Part 25: Airworthiness Standards for Transport Category Aircraft (Aviaizdat, Moscow, 2009) [in Russian].
2. O. V. Mitrakov, N. O. Yakovlev, N. A. Yakusheva, and A. V. Grinevich, “Peculiarities of fracture of steel 20KhGSN2MFA-VD during fracture toughness testing,” Aviats. Mater. Tekhnol., No. 1, 49–56 (2019). https://doi.org/10.18577/2071-9140-2019-0-1-49-56
3. A. I. Astashkin, V. V. Babanov, A. A. Selivanov, and E. A. Tkachenko, “Structure and properties of massive forgings with a reduced level of residual stresses from aluminum alloy 1933sb of balanced composition,” Trudy VIAM, No. 7, 02 (2021). https://doi.org/10.18577/2307-6046-2021-0-7-13-21
4. V. V. Avtaev and N. O. Yakovlev, “Study of static crack resistance and fracture resistance of thin sheet aluminum alloy using digital image correlation method,” Deform. Razrush. Mater., No. 2, 29–35 (2020).
5. V. S. Erasov, G. A. Nuzhny, A. V. Grinevich, and A. L. Terekhin, “Crack resistance of aircraft materials during fatigue testing,” Trudy VIAM, No. 10, 06 (2013).