Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures:
"This monograph presents a Guided Wave Structural Health Monitoring (GWSHM) system for aeronautical composite structures. Particular attention is paid to the development of a reliable and reproducible system with the capability to detect and localise barely visible impact damage (BVID) in Carbo...
Gespeichert in:
| Hauptverfasser: | , , |
|---|---|
| Format: | Elektronisch E-Book |
| Sprache: | English |
| Veröffentlicht: |
New Jersey ; London ; Singapore ; Beijing ; Shanghai ; Hong Kong ; Taipei Chennai ; Tokyo
World Scientific
[2024]
|
| Schriftenreihe: | Computational and experimental methods in structures
vol. 14 |
| Schlagworte: | |
| Online-Zugang: | Volltext |
| Zusammenfassung: | "This monograph presents a Guided Wave Structural Health Monitoring (GWSHM) system for aeronautical composite structures. Particular attention is paid to the development of a reliable and reproducible system with the capability to detect and localise barely visible impact damage (BVID) in Carbon-Fibre Reinforced Polymer (CFRP) structures. A novel sensor installation method that offers ease of application and replacement as well as excellent durability is introduced. Electromechanical Impedance (EMI) is also introduced to assess the durability of the sensor installation methods in simulated aircraft operational conditions, including thermal cycles, fatigue loading and hot-wet conditions. Damage characterisation using GWSHM is described and used to investigate damage in different CFRP structures. Key issues in guided wave-based damage identification are highlighted and addressed, including wave mode and frequency selection, the influence of dynamic load, the validity of simulated damage, and the sensitivity of guided waves to impact damage in different CFRP materials. The influence of temperature on guided wave propagation in anisotropic CFRP structures is described, and a novel baseline reconstruction approach for temperature compensation is presented. Finally, a multi-level hierarchical approach for the quantification of an ultrasonic GWSHM system is presented"-- |
| Beschreibung: | Literaturverzeichnis: Seite 177-183 |
| Beschreibung: | 1 Online-Ressource (xii, 188 Seiten) Illustrationen, Diagramme |
| ISBN: | 9781800614703 |
Internformat
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| 490 | 1 | |a Computational and experimental methods in structures |v vol. 14 | |
| 500 | |a Literaturverzeichnis: Seite 177-183 | ||
| 520 | 3 | |a "This monograph presents a Guided Wave Structural Health Monitoring (GWSHM) system for aeronautical composite structures. Particular attention is paid to the development of a reliable and reproducible system with the capability to detect and localise barely visible impact damage (BVID) in Carbon-Fibre Reinforced Polymer (CFRP) structures. A novel sensor installation method that offers ease of application and replacement as well as excellent durability is introduced. Electromechanical Impedance (EMI) is also introduced to assess the durability of the sensor installation methods in simulated aircraft operational conditions, including thermal cycles, fatigue loading and hot-wet conditions. Damage characterisation using GWSHM is described and used to investigate damage in different CFRP structures. Key issues in guided wave-based damage identification are highlighted and addressed, including wave mode and frequency selection, the influence of dynamic load, the validity of simulated damage, and the sensitivity of guided waves to impact damage in different CFRP materials. The influence of temperature on guided wave propagation in anisotropic CFRP structures is described, and a novel baseline reconstruction approach for temperature compensation is presented. Finally, a multi-level hierarchical approach for the quantification of an ultrasonic GWSHM system is presented"-- | |
| 653 | 0 | |a Airframes / Testing | |
| 653 | 0 | |a Structural health monitoring | |
| 653 | 0 | |a Composite materials / Testing | |
| 653 | 0 | |a Measurement uncertainty (Statistics) | |
| 653 | 0 | |a Wave guides | |
| 700 | 1 | |a Khodaei, Z. Sharif |e Verfasser |0 (DE-588)1153215799 |4 aut | |
| 700 | 1 | |a Aliabadi, Mohammad H. |d 1956- |e Verfasser |0 (DE-588)101222158X |4 aut | |
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| 830 | 0 | |a Computational and experimental methods in structures |v vol. 14 |w (DE-604)BV047846203 |9 14 | |
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| 912 | |a ZDB-124-WOP | ||
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Datensatz im Suchindex
| _version_ | 1819862806711762944 |
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| author | Yue, Nan Khodaei, Z. Sharif Aliabadi, Mohammad H. 1956- |
| author_GND | (DE-588)1153215799 (DE-588)101222158X |
| author_facet | Yue, Nan Khodaei, Z. Sharif Aliabadi, Mohammad H. 1956- |
| author_role | aut aut aut |
| author_sort | Yue, Nan |
| author_variant | n y ny z s k zs zsk m h a mh mha |
| building | Verbundindex |
| bvnumber | BV049940859 |
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| dewey-full | 629.134/310287 |
| dewey-hundreds | 600 - Technology (Applied sciences) |
| dewey-ones | 629 - Other branches of engineering |
| dewey-raw | 629.134/310287 |
| dewey-search | 629.134/310287 |
| dewey-sort | 3629.134 6310287 |
| dewey-tens | 620 - Engineering and allied operations |
| discipline | Verkehr / Transport |
| format | Electronic eBook |
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| id | DE-604.BV049940859 |
| illustrated | Illustrated |
| indexdate | 2024-12-30T11:00:18Z |
| institution | BVB |
| isbn | 9781800614703 |
| language | English |
| oai_aleph_id | oai:aleph.bib-bvb.de:BVB01-035279089 |
| open_access_boolean | |
| owner | DE-83 |
| owner_facet | DE-83 |
| physical | 1 Online-Ressource (xii, 188 Seiten) Illustrationen, Diagramme |
| psigel | ZDB-124-WOP |
| publishDate | 2024 |
| publishDateSearch | 2024 |
| publishDateSort | 2024 |
| publisher | World Scientific |
| record_format | marc |
| series | Computational and experimental methods in structures |
| series2 | Computational and experimental methods in structures |
| spelling | Yue, Nan Verfasser aut Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures Nan Yue (Delft University of Technology, The Netherlands), Zahra Sharif Khodaei (Imperial College London, UK), M H Ferri Aliabadi (Imperial College London, UK) New Jersey ; London ; Singapore ; Beijing ; Shanghai ; Hong Kong ; Taipei Chennai ; Tokyo World Scientific [2024] 1 Online-Ressource (xii, 188 Seiten) Illustrationen, Diagramme txt rdacontent c rdamedia cr rdacarrier Computational and experimental methods in structures vol. 14 Literaturverzeichnis: Seite 177-183 "This monograph presents a Guided Wave Structural Health Monitoring (GWSHM) system for aeronautical composite structures. Particular attention is paid to the development of a reliable and reproducible system with the capability to detect and localise barely visible impact damage (BVID) in Carbon-Fibre Reinforced Polymer (CFRP) structures. A novel sensor installation method that offers ease of application and replacement as well as excellent durability is introduced. Electromechanical Impedance (EMI) is also introduced to assess the durability of the sensor installation methods in simulated aircraft operational conditions, including thermal cycles, fatigue loading and hot-wet conditions. Damage characterisation using GWSHM is described and used to investigate damage in different CFRP structures. Key issues in guided wave-based damage identification are highlighted and addressed, including wave mode and frequency selection, the influence of dynamic load, the validity of simulated damage, and the sensitivity of guided waves to impact damage in different CFRP materials. The influence of temperature on guided wave propagation in anisotropic CFRP structures is described, and a novel baseline reconstruction approach for temperature compensation is presented. Finally, a multi-level hierarchical approach for the quantification of an ultrasonic GWSHM system is presented"-- Airframes / Testing Structural health monitoring Composite materials / Testing Measurement uncertainty (Statistics) Wave guides Khodaei, Z. Sharif Verfasser (DE-588)1153215799 aut Aliabadi, Mohammad H. 1956- Verfasser (DE-588)101222158X aut Erscheint auch als Druck-Ausgabe, Hardcover 978-1-80061-469-7 Computational and experimental methods in structures vol. 14 (DE-604)BV047846203 14 https://www.worldscientific.com/worldscibooks/10.1142/q0434#t=toc Verlag URL des Erstveröffentlichers Volltext |
| spellingShingle | Yue, Nan Khodaei, Z. Sharif Aliabadi, Mohammad H. 1956- Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures Computational and experimental methods in structures |
| title | Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures |
| title_auth | Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures |
| title_exact_search | Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures |
| title_full | Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures Nan Yue (Delft University of Technology, The Netherlands), Zahra Sharif Khodaei (Imperial College London, UK), M H Ferri Aliabadi (Imperial College London, UK) |
| title_fullStr | Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures Nan Yue (Delft University of Technology, The Netherlands), Zahra Sharif Khodaei (Imperial College London, UK), M H Ferri Aliabadi (Imperial College London, UK) |
| title_full_unstemmed | Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures Nan Yue (Delft University of Technology, The Netherlands), Zahra Sharif Khodaei (Imperial College London, UK), M H Ferri Aliabadi (Imperial College London, UK) |
| title_short | Uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures |
| title_sort | uncertainty quantification of guided wave structural health monitoring for aeronautical composite structures |
| url | https://www.worldscientific.com/worldscibooks/10.1142/q0434#t=toc |
| volume_link | (DE-604)BV047846203 |
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