Compression Compression fatigue tests on multi stiffener aerospace structures 核心 · 已核验
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This dataset contains health monitoring data collected during compression compression fatigue and quasi-static tests of multi stiffener (Level 2) aerospace composite panels. The panels were initially or after some time 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). Six coupons were tested until failure (2 Quasi-static and 4 fatigue) and the folders contain Acoustic Emission, optical fibres (distributed sensing) data, Lamb wave data and C-scan images of the different impact damages. Data recorded prior to impact are denoted as BI while those after impact are denoted with AI.
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CC-BY 4.0 许可范围(见关于与许可)。
- 落地页
- https://doi.org/10.34894/0KLFW4
- 许可证
- CC-BY-SA-4.0 (置信:verified_official)
- 国内可访问性
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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
传感器
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sensor_type: acoustic_emission_sensor
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运行工况
溯源(12 条)
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来源链接: https://doi.org/10.34894/0KLFW4
日期: 2026-07-09
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日期: 2026-07-10
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日期: 2026-07-10
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日期: 2026-07-10
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日期: 2026-07-10
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日期: 2026-07-11
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日期: 2026-07-11
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日期: 2026-07-14
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日期: 2026-07-25
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日期: 2026-07-26
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