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https://doi.org/10.1007/978-3-319-48761-8_67
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Cite Publication Date: Jan 1, 2012 |
 Citations: 3 |
Current aircraft structures have to meet the static, fatigue and damage tolerance (F&DT) criteria according to the actual FAA/EASA regulations. Furthermore, the structures consider common industry design standards, e.g. redundant structure, large damage capability, etc.
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