Random 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). Ten coupons were tested until failure and the folders contain Acoustic Emission, Lamb waves and optical fibres (FBGs) data as well as information regarding Lamb wave acquisition intervals. This dataset is the third series of the 4 testing campaigns.

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落地页
https://doi.org/10.34894/ABR2WX
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
condition_monitoring

故障工况

fault_type: delamination

传感器

sensor_type: acoustic_emission_sensor
sensor_type: fiber_bragg_grating_sensor

运行工况

condition_type: load
关联论文(30 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

仅列前 20 篇(首发/综述优先,按年份倒序);全量见 API

溯源(12 条)
来源链接: https://doi.org/10.34894/ABR2WX 日期: 2026-07-09
日期: 2026-07-10
日期: 2026-07-10
日期: 2026-07-10
日期: 2026-07-10
日期: 2026-07-10
日期: 2026-07-10
日期: 2026-07-11
日期: 2026-07-11
日期: 2026-07-14
日期: 2026-07-25
日期: 2026-07-26