Fatigue crack growth in AlCu4Mg1 under nonproportional bending with torsion loading

The paper presents the experimental results of fatigue crack growth on AlCu4Mg1 aluminium alloy under proportional and non-proportional bending with torsion obtained at Opole University of Technology. Specimens with square sections and stress concentrations in the form of external one-sided sharp no...

Повний опис

Збережено в:
Бібліографічні деталі
Дата:2010
Автори: Rozumek, D., Marciniak, Z.
Формат: Стаття
Мова:English
Опубліковано: Фізико-механічний інститут ім. Г.В. Карпенка НАН України 2010
Назва видання:Фізико-хімічна механіка матеріалів
Онлайн доступ:http://dspace.nbuv.gov.ua/handle/123456789/137186
Теги: Додати тег
Немає тегів, Будьте першим, хто поставить тег для цього запису!
Назва журналу:Digital Library of Periodicals of National Academy of Sciences of Ukraine
Цитувати:Fatigue crack growth in AlCu4Mg1 under nonproportional bending with torsion loading / D. Rozumek, Z. Marciniak // Фізико-хімічна механіка матеріалів. — 2010. — Т. 46, № 5. — С. 102-108. — Бібліогр.: 14 назв. — англ.

Репозитарії

Digital Library of Periodicals of National Academy of Sciences of Ukraine
Опис
Резюме:The paper presents the experimental results of fatigue crack growth on AlCu4Mg1 aluminium alloy under proportional and non-proportional bending with torsion obtained at Opole University of Technology. Specimens with square sections and stress concentrations in the form of external one-sided sharp notches were used. The tests were performed in the high cycle fatigue regime for the stress ratio R = –1 and phase shift between bending and torsion loading equal to φ = 0; 45° and 90°. Three paths of loading were used: line, ellipse and circle. The fatigue crack growth was cyclically measured with use of the optical microscope (magnification of 25 times), strain gauges and computer allow to register signals of loading. In the tested specimens, it was possible to observe growth of cracks conforming with mixed mode I + III. The crack growths were non-uniform at both sides of the specimen surface, however the difference between crack lengths was rather small. In the biaxial tests, influence of bending was six times greater because of the notches in the bending plane. The test results were described by the stress intensity factor range, ∆K.