Aeroengine Safety - 5:54:542:5422<a style="color:#000" href="https://www.tugraz.at/institute/ittm">Institute of Thermal Turbomachinery and Machine Dynamics</a></br><a href="https://www.tugraz.at">Graz University of Technology</a>
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2026-06-10T01:44:31+00:00Aeroengine Safety
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https://aeroenginesafety.tugraz.at/lib/exe/fetch.php?media=wiki:logo.pngtext/html2020-06-25T20:43:39+00:00Anonymous (anonymous@undisclosed.example.com)5.4.2.2 Damage due to Stress Corrosion Cracking (SCC)
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5.4.2.2 Damage due to Stress Corrosion Cracking (SCC)
SCC can cause engine parts to fail prematurely through crack initiation and fracture. It must be remembered, that SCC not only increases the subcritical crack growth rate, minimizing the remaining life span in the crack growth phase, but also decreases the critical fracture toughness considerably, shortening the critical crack length and further decreasing the crack growth phase.<a id="vulnerable-components"></a><a id="sensitization-during…