Optimised laser peening strategies for damage tolerant aircraft structures
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DOI: 10.1016/j.ijfatigue.2020.105890
Abstract: Abstract Simulation models were constructed to explore the influence of compressive residual stress on fatigue crack growth rates in aluminium sheet. Balanced residual stress fields resulting from imposition of compressive stresses in laser peen patches… read more here.
Keywords: laser peening; growth rates; damage tolerant; residual stress ... See more keywords