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THE INFLUENCE OF LASER SHOCK PEENING ON THE BEHAVIOR OF Ti6Al4V TITANIUM ALLOY UNDER GIGACYCLE FATIGUE CONDITIONS
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This study investigates the gigacycle fatigue behavior of Ti6Al4V
titanium alloy – a critical aerospace material – following laser shock
peening (LSP). While prior work by the authors demonstrated LSP enhances
fatigue life by up to 8 times in stress-concentrated samples, the
present research reveals a paradoxical deterioration under gigacycle
conditions (
N
=10
10
using ultrasonic testing
(Shimadzu USF-2000). Contrary to established LSP benefits, treated
specimens exhibited a significant reduction in fatigue limit compared to
as-received material. Infrared thermography confirmed substantially
higher energy dissipation in LSP-processed specimens, while fractography
showed a complete transition in failure origin: cracks invariably
initiated centrally in LSP specimens versus near-surface initiation in
untreated counterparts. These findings are attributed to tensile
residual stresses in the specimen core and microstructural alterations
induced by LSP.
Title: THE INFLUENCE OF LASER SHOCK PEENING ON THE BEHAVIOR OF Ti6Al4V TITANIUM ALLOY UNDER GIGACYCLE FATIGUE CONDITIONS
Description:
This study investigates the gigacycle fatigue behavior of Ti6Al4V
titanium alloy – a critical aerospace material – following laser shock
peening (LSP).
While prior work by the authors demonstrated LSP enhances
fatigue life by up to 8 times in stress-concentrated samples, the
present research reveals a paradoxical deterioration under gigacycle
conditions (
N
=10
10
using ultrasonic testing
(Shimadzu USF-2000).
Contrary to established LSP benefits, treated
specimens exhibited a significant reduction in fatigue limit compared to
as-received material.
Infrared thermography confirmed substantially
higher energy dissipation in LSP-processed specimens, while fractography
showed a complete transition in failure origin: cracks invariably
initiated centrally in LSP specimens versus near-surface initiation in
untreated counterparts.
These findings are attributed to tensile
residual stresses in the specimen core and microstructural alterations
induced by LSP.
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