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Residual stresses due to foreign object damage in laser-shock peened aerofoils: Simulation and measurement (2015)

First Author: Lin B

Attributed to: Fatigue Crack Growth in Complex Residual Stress Fields due to Surface Treatment and Foreign Object Damage under Simulated Flight Cycles funded by EPSRC

Abstract

No abstract provided

Bibliographic Information

Digital Object Identifier: http://dx.doi.org/10.1016/j.mechmat.2014.12.001

Publication URI: http://dx.doi.org/10.1016/j.mechmat.2014.12.001

Type: Journal Article/Review

Parent Publication: Mechanics of Materials