- Tytuł:
- Effect of Natural Aging and Fatigue Crack Propagation Rate on Welded and Non-Welded Aluminum Alloy (AA2219-T87)
- Autorzy:
-
Ijaz, Mudasir
Qayyum, Faisal
Elahi, Hassan
Ullah, Mudaser
Eugeni, Marco
Badshah, Saeed
Gaudenzi, Paolo - Powiązania:
- https://bibliotekanauki.pl/articles/102921.pdf
- Data publikacji:
- 2019
- Wydawca:
- Stowarzyszenie Inżynierów i Techników Mechaników Polskich
- Tematy:
-
natural aging
AA2219
crack growth rate
structure health
fatigue
microstructure
stress intensity factor
naturalne starzenie się
tempo wzrostu pęknięć
zmęczenie
mikrostruktura
współczynnik intensywności stresu - Opis:
- Aluminum alloys are widely used for fabrication of aircraft, civil structures, and space vehicles. Fatigue life consideration of a material is the most important design criteria in many such critical applications. In this research work, a widely used Aluminum alloy AA2219-T87 was TIG welded using AA2319 as a filler material. The effect of natural aging on Fatigue Crack Propagation Rate (FCPR) of welded and non-welded compact tension (CT) specimens (AA2219˗T87) is studied. The relationship between stress intensity factor (ΔK) and crack ratio (a/W) for different value of the crack length in base metal and the welded zone is presented. Paris curves for both welded and non-welded specimens and compared to study the effect of natural aging (NA) on FCGR and compared with non-aged specimens. The results obtained provide a base for the development of Structural Health Monitoring systems for the propagation of crack growth in such components.
- Źródło:
-
Advances in Science and Technology. Research Journal; 2019, 13, 3; 129-143
2299-8624 - Pojawia się w:
- Advances in Science and Technology. Research Journal
- Dostawca treści:
- Biblioteka Nauki
Artykuł