Springer Nature is making SARS-CoV-2 and COVID-19 research free. View research | View latest news | Sign up for updates

Crack resistance of extruded and rolled semifinished products of aluminum alloys used in the load structures of an airplane wing

  • 14 Accesses

This is a preview of subscription content, log in to check access.

Literature cited

  1. 1.

    A. G. Vovnyanko, G. Yu. Bengus, and I. S. Vorontsov, “The static strength and fatigue life of large extruded semifinished products of D16chT, V95pchT1, and V95pchT2 alloys,” Fiz.-Khim. Mekh. Mater., No. 1, 76–81 (1982).

  2. 2.

    S. Ya. Yarema, O. P. Ostash, A. G. Vovnyanko, et al., “The influence of anisotropy and operating time on crack growth in extruded and rolled semifinished products of D16chT and V95pchT1 alloys,” Fiz.-Khim. Mekh. Mater., No. 1, 20–24 (1983).

  3. 3.

    S. Ya. Yarema, O. D. Zinyuk, A. G. Vovnyanko, et al., “An investigation of the period of origin and growth of fatigue cracks in extruded panels of aluminum alloys,” Fiz.-Khim. Mekh. Mater., No. 5, 75–80 (1983).

  4. 4.

    S. P. Malashenko, A. G. Vovnyanko, and G. Yu. Bengus, “The influence of sample width and thickness on the fracture toughness and parameters of the fatigue failure curve of aluminum alloy semifinished products,” in: The Crack Resistance of Materials and Structural Elements [in Russian], Naukova Dumka, Kiev (1980), pp. 269–273.

  5. 5.

    S. I. Kishkina, The Fracture Resistance of Aluminum Alloys [in Russian], Metallurgiya, Moscow (1981).

  6. 6.

    S. Ya. Yarema, O. P. Ostash, V. P. Rychik, et al., “The development of fatigue cracks in sheets of D16A and V95A aluminum alloys,” Fiz.-Khim. Mekh. Mater., No. 1, 46–51 (1977).

Download references

Additional information

Translated from Fiziko-Khimicheskaya Mekhanika Materialov, Vol. 20, No. 2, pp. 99–102, March–April, 1984.

Rights and permissions

Reprints and Permissions

About this article

Cite this article

Vovnyanko, A.G., Dotsenko, A.M. Crack resistance of extruded and rolled semifinished products of aluminum alloys used in the load structures of an airplane wing. Mater Sci 20, 189–192 (1984). https://doi.org/10.1007/BF00721352

Download citation

Keywords

  • Aluminum
  • Aluminum Alloy
  • Semifinished Product
  • Load Structure
  • Airplane Wing