Variable amplitude Compression Compression fatigue tests on single stiffener aerospace structures

Variable amplitude Compression Compression fatigue tests on single stiffener aerospace structures 核心 · 已核验

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This dataset contains health monitoring data collected during compression compression fatigue tests of single stiffener (Level 1) aerospace composite panels. The coupons were initially damaged either by a low velocity impact or by an artificial disbond, located between the stiffener and the skin (a pdf file highlights the locations). Five coupons were tested in variable amplitude fatigue until failure and the folders contain Acoustic Emission (.DTA), Lamb waves and optical fibres (FBGs) data. This dataset is the second series of the 4 testing campaigns.

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落地页: https://doi.org/10.34894/WCDRLW
许可证: CC-BY-SA-4.0 (置信:verified_official)
国内可访问性: 国内直连:可达 (2026-07-11 检测) 非直连:可达 (2026-07-11 检测)
「直连超时」表示检测窗口内未完成,系慢或不稳定证据,不构成封锁证据。
发布年份: 2025
设备类型: composite_structure
PHM 任务: health_state_assessment

故障工况

传感器

运行工况

关联论文(39 篇)

仅表示这篇论文与本数据集在文献网络中相邻, 不代表该论文确实使用了本数据集。

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仅列前 20 篇(首发/综述优先,按年份倒序);全量见 API。

溯源(12 条)