Effect of Natural Aging and Fatigue Crack Propagation Rate on Welded and Non-Welded Aluminum Alloy (AA2219˗T87)
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 AA...
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| Format: | Article |
| Language: | English |
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Lublin University of Technology
2019-09-01
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| Series: | Advances in Sciences and Technology |
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| Online Access: | http://www.journalssystem.com/astrj/Effect-of-natural-aging-and-Fatigue-Crack-Propagation-Rate-FCPR-on-welded-and-non,110737,0,2.html |