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Fatigue Crack Propagation Estimation Based on Direct Strain Measurement during a Full-Scale Fatigue Test
Military aircraft are subjected to variable loads, which are the main cause of initiation and propagation of cracks in the most stressed locations of the airframe. The aim of a Full-Scale Fatigue Test (FSFT) is to represent actual load conditions in such a way that the results obtained are a good re...
| Autores principales: | , , |
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| Formato: | Online Artículo Texto |
| Lenguaje: | English |
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MDPI
2022
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| Acceso en línea: | https://www.ncbi.nlm.nih.gov/pmc/articles/PMC8914641/ https://www.ncbi.nlm.nih.gov/pubmed/35271167 http://dx.doi.org/10.3390/s22052019 |