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dc.contributor.authorIgnatovich, S.R.-
dc.contributor.authorKrasnopolskii, V.S.-
dc.descriptionКонгресс Авіація в 21 ст., Безпека авіації та космічні технологіїuk_UA
dc.description.abstractThis paper investigates the description of the fatigue cracks growth in sheet aluminum alloy D16AT by exponential dependence. The results show that the propagation of all investigated fatigue cracks can be satisfactorily described by this dependence with grate values of the determination coefficient.uk_UA
dc.titleFatigue cracks growth features in aluminum alloy D16ATuk_UA
dc.specialityFatigue and fracture of aircraft structuresuk_UA
Appears in Collections:Матеріали конференцій кафедри конструкції літальних апаратів

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