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• W2897560841 abstract "Research Article| October 23 2018 Effect of Simulated Accelerated Atmospheric Environment Conditions on Fatigue Crack Growth Rates Jason Niebuhr; Jason Niebuhr *SAFE Inc, 3290 Hamal Cir, Monument, CO 80132. Search for other works by this author on: This Site PubMed Google Scholar Sarah Galyon Dorman; Sarah Galyon Dorman ‡ *SAFE Inc, 3290 Hamal Cir, Monument, CO 80132. ‡Corresponding author. E-mail: sgd@saf-engineering.com. Search for other works by this author on: This Site PubMed Google Scholar Saravanan Arunachalam; Saravanan Arunachalam *SAFE Inc, 3290 Hamal Cir, Monument, CO 80132. Search for other works by this author on: This Site PubMed Google Scholar Justin Rausch; Justin Rausch *SAFE Inc, 3290 Hamal Cir, Monument, CO 80132. Search for other works by this author on: This Site PubMed Google Scholar Scott Fawaz Scott Fawaz *SAFE Inc, 3290 Hamal Cir, Monument, CO 80132. Search for other works by this author on: This Site PubMed Google Scholar CORROSION (2019) 75 (5): 506–512. https://doi.org/10.5006/2974 Article history Received: July 16 2018 Revision Received: October 11 2018 Accepted: October 11 2018 Views Icon Views Article contents Figures & tables Video Audio Supplementary Data Share Icon Share Facebook Twitter LinkedIn Email Tools Icon Tools Get Permissions Cite Icon Cite Search Site Citation Jason Niebuhr, Sarah Galyon Dorman, Saravanan Arunachalam, Justin Rausch, Scott Fawaz; Effect of Simulated Accelerated Atmospheric Environment Conditions on Fatigue Crack Growth Rates. CORROSION 1 May 2019; 75 (5): 506–512. doi: https://doi.org/10.5006/2974 Download citation file: Ris (Zotero) Reference Manager EasyBib Bookends Mendeley Papers EndNote RefWorks BibTex toolbar search Search nav search search input Search input auto suggest Search Corrosion significantly impacts the usable structural life of an airframe. Such systems are primarily designed to withstand a well-defined load spectrum that is a function of flight profile and mission type. However, the airframe is also exposed to a spectrum of environmental conditions including variations in temperature, humidity, atmospheric gas composition, salt concentration, pollution, and ultraviolet light exposure which tend to degrade structural capabilities over time. The detrimental influence of chlorides on fatigue performance for metallic materials has been documented in mechanical tests typically performed in an aqueous solution. Yet aqueous solutions are poor predictors of atmospheric corrosion phenomena. The presence of water vapor has generally been shown to accelerate fatigue crack growth rates (FCGR) when comparing baseline results to those from experiments at low-temperature, low-pressure, dry air, or in inert gas. Recent research has shown promise in improving the correlation between laboratory results and field exposures by incorporating ozone and salt into atmospheric corrosion studies. The current test program aims to incorporate those effects into the study of FCGR in aerospace aluminum. Full fatigue crack growth rate curves for both baseline laboratory air and accelerated atmospheric environments were produced. The effect of ozone in combination with relative humidity was examined and found to slow crack growth rates at mid-range ΔK values. The effect of wetting and drying on atmospheric fatigue crack growth rates was examined using constant ∆K testing and the drying cycle was observed to accelerate the fatigue crack growth in line with other research. © 2019, NACE International2019 You do not currently have access to this content." @default.
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• W2897560841 date "2018-10-23" @default.
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• W2897560841 title "Effect of Simulated Accelerated Atmospheric Environment Conditions on Fatigue Crack Growth Rates" @default.
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