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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).
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).
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).
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.
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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).
Translated from Fiziko-Khimicheskaya Mekhanika Materialov, Vol. 20, No. 2, pp. 99–102, March–April, 1984.
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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
- Aluminum Alloy
- Semifinished Product
- Load Structure
- Airplane Wing