Experimental evaluation of effective stress intensity factor using thermoelastic stress analysis and digital image correlation

•Calculation of effective stress intensity factor range by TSA and DIC.•Combination of full-field optical techniques with models for characterising crack tip fields.•Retardation effect on fatigue crack growth by analysing the range of stress intensity factor.•Potential ability of TSA and DIC to acco...

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Veröffentlicht in:International journal of fatigue 2020-06, Vol.135, p.105567-10, Article 105567
Hauptverfasser: Díaz, F.A., Vasco-Olmo, J.M., López-Alba, E., Felipe-Sesé, L., Molina-Viedma, A.J., Nowell, D.
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container_end_page 10
container_issue
container_start_page 105567
container_title International journal of fatigue
container_volume 135
creator Díaz, F.A.
Vasco-Olmo, J.M.
López-Alba, E.
Felipe-Sesé, L.
Molina-Viedma, A.J.
Nowell, D.
description •Calculation of effective stress intensity factor range by TSA and DIC.•Combination of full-field optical techniques with models for characterising crack tip fields.•Retardation effect on fatigue crack growth by analysing the range of stress intensity factor.•Potential ability of TSA and DIC to account for the shielding effect during fatigue crack growth. During the last decades, the debate over the mechanisms governing fatigue crack shielding has been mainly focused on demonstrating the existence of fatigue crack closure and the difficulties on quantifying the induced stress during crack propagation. Hence, most adopted experimental methods have been based on the direct or indirect measurement of contact loads between crack surfaces as the crack starts closing. Nevertheless, these methods depend on many factors sometime difficult to control, which has contributed to question their reliability by many authors. For this reason, two modern well established, full-field, non-contact experimental techniques, namely Thermoelastic Stress Analysis (TSA) and 2D Digital Image Correlation (2D-DIC), have been analysed to evaluate the influence of crack shielding during fatigue experiments conducted on two aluminium alloys (Al2024-T3 and Al7050) tested at different stress ratios. In the particular case of TSA, the technique appears to have a great potential in the evaluation of fatigue crack shielding since crack tip events are inferred directly from the temperature changes occurring at the crack tip rather than from remote data. Experimental data from both techniques have been employed in combination with two different mathematical models based on Muskhelishvili’s complex potentials to infer the effective range of stress intensity factor. Results from both techniques agree quite well, showing a variation in the stress intensity factor range as the R-ratio changes from 0.1 to 0.5 and illustrating the potential ability of both techniques to account for the shielding effect due to crack closure.
doi_str_mv 10.1016/j.ijfatigue.2020.105567
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source ScienceDirect Journals (5 years ago - present)
subjects Aluminum base alloys
Contact loads
Contact stresses
Correlation analysis
Crack closure
Crack propagation
Crack shielding
Crack tips
Digital image correlation (DIC)
Digital imaging
Evaluation
Fatigue crack growth
Fatigue failure
Fatigue tests
Materials fatigue
Mathematical analysis
Reliability aspects
Shielding
Stress analysis
Stress intensity factor
Stress intensity factors
Stress propagation
Thermoelastic stress analysis (TSA)
Two dimensional analysis
title Experimental evaluation of effective stress intensity factor using thermoelastic stress analysis and digital image correlation
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