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TECHNICAL PAPERS

A Damage Mechanics-Based Fatigue Life Prediction Model for Solder Joints

[+] Author and Article Information
Hong Tang

NEC Electronics Corporation, Detroit, MI

Cemal Basaran

UB Electronic Packaging Laboratory, University at Buffalo, SUNY, Buffalo, NY 14260e-mail: cjb@eng.buffalo.edu

J. Electron. Packag 125(1), 120-125 (Mar 14, 2003) (6 pages) doi:10.1115/1.1536171 History: Received December 10, 2001; Online March 14, 2003
Copyright © 2003 by ASME
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References

Figures

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Uniaixial extension simulation (solid lines) versus Adams’s test under strain rate 1.67E-2 and different temperature
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Uniaixial extension simulation (solid lines) versus Skipor’s test under strain rate 1.0E-1 and different temperature
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Uniaixial extension simulation (solid lines) versus McDowell’s test under strain rate 1.0E-2 and different temperature
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Strain-stress hysteresis loop curves for 20, 100, 400, 700 cycles (inelastic strain range=0.04,35°C)
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Strain-stress hysteresis loop curves for 1010 cycles and damage evolution time-history (inelastic strain range=0.04,35°C)
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Strain-stress hysteresis loop curves for 20, 100, 600, 1100 cycles (inelastic strain range=0.03,35°C)
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Strain-stress hysteresis loop curves for 1010 cycles and damage evolution time-history (inelastic strain range=0.03,35°C)
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Strain-stress hysteresis loop curves for 20,100,600,1500 cycles, (inelastic strain range=0.025,35°C)
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Strain-stress hysteresis loop curves for 2000 cycles and damage evolution time-history (inelastic strain range=0.025,35°C)
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Comparison of fatigue life (Solomon’s test versus FEM)
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Cross section of BGA electronic package
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The thermal loading profile of one cycle
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Shear strain after two and four thermal cycles (with damage model implemented into ABAQUS)
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Shear strain after six and eight thermal cycles (with damage model implemented into ABAQUS)
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Shear strain after 10 thermal cycles (with damage model implemented into ABAQUS)
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Comparison of finite element simulation results with Moiré interferometry test data
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Damage distribution after two and four thermal cycles (with damage model implemented into ABAQUS)
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Damage distribution after six and eight thermal cycles (with damage model implemented into ABAQUS)
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Damage distribution after 10 thermal cycles (with damage model implemented into ABAQUS)
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The evolution of maximum damage under 10 thermal cycles (with damage model implemented into ABAQUS)

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