Abstract
The results of studies of the interrelations between the mechanical characteristics of aluminum alloys applied in rocket and spacecraft engineering and electrical conductivity are presented. The conductivity was measured with a BЭ-26H instrument. The requirements for upgrading the conductivity-measuring device aimed at a further development of the methods for testing of the mechanical characteristics are formulated.
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Bakunov, A.S. and Smolyagin, V.A., VE-26NTs Device for Conductivity Measurements, Defektoskopiya, 1991, no. 3, p. 81.
Gerasimov, V.G., Pokrovskii, A.D., and Sukhorukov, V.V., Nerazrushayushchii kontrol’ Kniga 3, Elektromagnitnyii kontrol’ (Nondestructive Testing: Book 3. Electromagnetic Testing), Moscow: Vysshaya Shkola, 1992.
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Original Russian Text © A.N. Khailov, T.N. Pen’kova, A.S. Bakunov, V.F. Muzhitskii, N.D. Presnov, V.I. Agal’tsov, 2006, published in Defektoskopiya, 2006, Vol. 42, No. 7, pp. 3–14.
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Khailov, A.N., Pen’kova, T.N., Bakunov, A.S. et al. Nondestructive testing of mechanical characteristics of aluminum alloys on the basis of their electrical conductivity. Russ J Nondestruct Test 42, 425–432 (2006). https://doi.org/10.1134/S1061830906070011
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DOI: https://doi.org/10.1134/S1061830906070011