DEFORMATION RELIEF AS AN INDICATOR OF THE TEMPERATURE FLUCTUATIONS INFLUENCE ON THE FATIGUE DAMAGE ACCUMULATION
Journal Title: Проблеми тертя та зношування - Year 2016, Vol 71, Issue
Abstract
The article describes the methods and the preliminary results of the research di-rected on the investigation of temperature influence on D16AT aluminium alloy fa-tigue. The initial stage of fatigue has been studied by the analysis of the surface de-formation relief. Test temperature regime corresponds to the aircraft structure tem-perature spectrum at the airfield. The level of cyclic stresses is about to those that arise when the airplane moves on airdrome surface.
Authors and Affiliations
M. KARUSKEVICH, T. P. MASLAK, V. V. KRAVCHENKO, О. P. KLYMENKO
Keywords
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