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Aluminum alloys are widely used in aerospace applications and energy generation due to its strength with respect to low densities. In application they are subjected to different static and cyclic loading conditions, so it is necessary to understand fatigue behavior in those loading condition. The objective of this investigation is to determine the fatigue strength of Aluminum 6061-T6 alloy. Stress and no of cycles are used for description of a fatigue curve. Here we study the effect of natural frequency, modal parameters and mode shape subjected to fatigue loading. And comparing the results of fatigue life prediction model with the experimental fatigue life values. There are two experimental setups required one of them is setup for Fatigue Test Machine in Plane Bending and other one is setup for modal testing.
Keywords:
Aluminum Alloy, 6061-T6
Cite Article:
"Investigation of Fatigue Life of Al 6061-T6 and its Modal analysis", International Journal for Research Trends and Innovation (www.ijrti.org), ISSN:2455-2631, Vol.3, Issue 4, page no.35 - 39, April-2018, Available :http://www.ijrti.org/papers/IJRTI1804007.pdf
Downloads:
000205269
ISSN:
2456-3315 | IMPACT FACTOR: 8.14 Calculated By Google Scholar| ESTD YEAR: 2016
An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 8.14 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator