NASA NTRS · 19930002960
A comparison of high cycle fatigue methodologies
Abstract
To evaluate alternate turbopump development (ATD) high cycle fatigue (HCF) methodology, a comparison was made with the space shuttle main engine (SSME) methodology. This report documents the comparison and evaluates ATD's HCF system.
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Herda, D. A.. 1992-08-01. A comparison of high cycle fatigue methodologies. https://ntrs.nasa.gov/citations/19930002960
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