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In this study, an experimental study was carried out on the fatigue life of a carbon fiber composite (CFC) T-joint under a standard transport aircraft spectrum load sequence and compared with predictions based on empirical methods. The co-cured CFC T-joints of size 175 mm × 150 mm × 2.7 mm skin (flange) and centrally placed 2 mm thick, 120 mm high web, were fabricated by autoclave process. The fatigue...
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