Fatigue Strength of Peened-Welded Joints after Single High Compressive Load Peaks

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This study investigated how peened-welded out-of-plane gusset welded joints respond under a single high compressive load peak, focusing on the relaxation behavior of compressive residual stress and its relationship to fatigue strength. Using X-ray residual stress measurements at 2 mm from the peened edge during plate bending compression loading, the authors found that compressive residual stresses relaxed proportionally as compression load increased, with strain measurements supporting the relaxation estimation; plate bending fatigue tests at stress ratio R = 0.5 showed fatigue strength decreased with increasing compression load. Fatigue strength approached as-weld conditions at about 5.8 kN (≈ −286 N/mm²), and a newly proposed fatigue strength design curve with a peening cut-off remained applicable if the applied compressive load after peening did not exceed 3.8 kN, with continuous residual stress monitoring indicating improvement persists as long as residual compressive stress is preserved during subsequent loading; the authors also note it is a preprint not yet peer reviewed. This paper does not explicitly discuss endometriosis or adenomyosis; it was included in the corpus via a keyword match in the upstream search index.

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Abstract

Abstract This study investigates the fatigue strength of peened-welded joints after single high compressive load peaks. To understand the relaxation behavior of compressive residual stress, out-of-plane gusset welded joints were treated using different peening methods. Compressive residual stress near the peened edge was measured using an X-ray residual stress analyzer while applying plate bending compression loads. The results showed that compressive residual stresses at 2 mm from the peened edge relaxed proportionally with increasing compression load. Strain measurements at the same location supported the estimation of stress relaxation behavior. Plate bending fatigue tests were then conducted under a stress ratio of R = 0.5. Fatigue strength decreased with increasing compression load, and under a 5.8 kN (approximately − 286 N/mm²), the fatigue strength approached that of as-weld. Finally, the fatigue results were evaluated using a newly proposed fatigue strength design curve with a cut-off limit for peening treatment, based on recommendations from the JSSC. It was concluded that this curve remains applicable if the applied compressive load after peening does not exceed 3.8 kN. Furthermore, continuous residual stress monitoring at the 2 mm confirmed that fatigue strength improvement remains effective as long as residual compressive stress is preserved during subsequent loading.
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Fatigue Strength of Peened-Welded Joints after Single High Compressive Load Peaks | Research Square window.SnipcartSettings = { analytics: { enabled: false } }; (function() { var accessVector = localStorage.getItem('access_vector') || ''; window.dataLayer = window.dataLayer || []; if (accessVector) { window.dataLayer.push({ user: { profile: { profileInfo: { snid: accessVector } } } }); } })(); (function(w,d,s,l,i){w[l]=w[l]||[];w[l].push({'gtm.start':new Date().getTime(),event:'gtm.js'});var f=d.getElementsByTagName(s)[0],j=d.createElement(s),dl=l!='dataLayer'?'&l='+l:'';j.async=true;j.src='https://www.googletagmanager.com/gtm.js?id='+i+dl;f.parentNode.insertBefore(j,f);})(window,document,'script','dataLayer','GTM-K279D39R'); Browse Preprints In Review Journals COVID-19 Preprints AJE Video Bytes Research Tools Research Promotion AJE Professional Editing AJE Rubriq About Preprint Platform In Review Editorial Policies Our Team Advisory Board Help Center Sign In Submit a Preprint Cite Share Download PDF Research Article Fatigue Strength of Peened-Welded Joints after Single High Compressive Load Peaks Yuki Banno, Koji Kinoshita, Toshiyuki Ishikawa, Kengo Anami This is a preprint; it has not been peer reviewed by a journal. https://doi.org/ 10.21203/rs.3.rs-7061494/v1 This work is licensed under a CC BY 4.0 License Status: Under Review Version 1 posted 5 You are reading this latest preprint version Abstract This study investigates the fatigue strength of peened-welded joints after single high compressive load peaks. To understand the relaxation behavior of compressive residual stress, out-of-plane gusset welded joints were treated using different peening methods. Compressive residual stress near the peened edge was measured using an X-ray residual stress analyzer while applying plate bending compression loads. The results showed that compressive residual stresses at 2 mm from the peened edge relaxed proportionally with increasing compression load. Strain measurements at the same location supported the estimation of stress relaxation behavior. Plate bending fatigue tests were then conducted under a stress ratio of R = 0.5. Fatigue strength decreased with increasing compression load, and under a 5.8 kN (approximately − 286 N/mm²), the fatigue strength approached that of as-weld. Finally, the fatigue results were evaluated using a newly proposed fatigue strength design curve with a cut-off limit for peening treatment, based on recommendations from the JSSC. It was concluded that this curve remains applicable if the applied compressive load after peening does not exceed 3.8 kN. Furthermore, continuous residual stress monitoring at the 2 mm confirmed that fatigue strength improvement remains effective as long as residual compressive stress is preserved during subsequent loading. Plate bending fatigue test Peened-welded joints Single high compressive load peaks Residual stress measurement Compressive residual stress relaxation Full Text Cite Share Download PDF Status: Under Review Version 1 posted Reviewers agreed at journal 28 Jul, 2025 Reviewers invited by journal 27 Jul, 2025 Editor invited by journal 23 Jul, 2025 Editor assigned by journal 17 Jul, 2025 First submitted to journal 17 Jul, 2025 You are reading this latest preprint version Research Square lets you share your work early, gain feedback from the community, and start making changes to your manuscript prior to peer review in a journal. As a division of Research Square Company, we’re committed to making research communication faster, fairer, and more useful. We do this by developing innovative software and high quality services for the global research community. Our growing team is made up of researchers and industry professionals working together to solve the most critical problems facing scientific publishing. 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