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MSc Automotive Engineering

Effect of Residual Stress on Fatigue Crack Growth on CT Samples (AA2024)

An experimental study of how laser shock peening changes residual stress, fatigue crack-growth behaviour and predicted life in aerospace-grade aluminium.

Research objective

Assess the influence of residual stress on fatigue crack-growth rate—and evaluate the life improvement produced by laser shock peening.

The work connects materials engineering, structural durability and data-led analysis: a strong Automotive project with a clear Technology dimension.

Experimental evidence

Inside the testing programme.

Original photographs reproduced from Sayaji Kakade's 2023 MSc dissertation report at Coventry University.

Compact-tension specimen mounted during progressive EDM slitting
01EDM slitting used for residual-stress measurement
AA2024 compact-tension specimen held in the fatigue-test fixture
02AA2024 compact-tension specimen
Instron ElectroPuls fatigue-testing machine used for the dissertation
033 kN Instron ElectroPuls test machine
Fatigue crack-growth test apparatus with the specimen and optical monitoring setup
04Fatigue crack-growth test apparatus

Experimental programme

Three conditions.
One controlled comparison.

Each compact-tension specimen was 5 mm thick. The peened specimens used a 15 × 15 mm treatment patch at two laser intensities.

CT1

Unpeened baseline

The reference compact-tension specimen used to establish baseline crack-growth behaviour.

CT2

LSP · 3 GW/cm²

Laser shock peened over a 15 × 15 mm patch to introduce a compressive residual-stress field.

CT4

LSP · 5 GW/cm²

The higher-intensity peened condition, assessed for the strongest fatigue-life improvement.

Methodology

From loading to
effective stress intensity.

01

Fatigue testing

Tests were conducted on a 3 kN Instron ElectroPuls at a load ratio of R = 0.1, following ASTM E647 practice and managed through Instron Console and WaveMatrix2.

02

Residual-stress measurement

The slitting method combined a strain gauge with progressive EDM cutting to measure released strain and determine the residual-stress intensity contribution, Kres.

03

Crack-growth analysis

Paris’ Law described the propagation regime, while the Walker equation accounted for mean-stress effects and ΔKeff incorporated the measured residual-stress contribution.

Findings

Compressive residual stress improved the predicted fatigue life.

The unpeened CT1 result aligned with the established compact-tension baseline. Both laser-shock-peened conditions indicated life improvement, with the higher-intensity treatment producing the strongest response.

Graph comparing residual stress intensity contribution Kres against crack length for the compact-tension specimens
Measured Kres comparison across the CT specimens
Logarithmic graph comparing fatigue crack-growth rate against stress-intensity range for the tested specimens
Fatigue crack-growth rate comparison, da/dN versus ΔK

Research outputs

Evidence developed through the study.