Please use this identifier to cite or link to this item:
https://doi.org/10.21256/zhaw-30074Full metadata record
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Ferrari, Viola | - |
| dc.contributor.author | Liao, Min | - |
| dc.contributor.author | Ferrari, Michea | - |
| dc.contributor.author | Guillaume, Michel | - |
| dc.date.accessioned | 2024-03-01T08:25:44Z | - |
| dc.date.available | 2024-03-01T08:25:44Z | - |
| dc.date.issued | 2023 | - |
| dc.identifier.uri | https://www.icaf.aero/icaf2023/proceedings/documents/121.pdf | de_CH |
| dc.identifier.uri | https://digitalcollection.zhaw.ch/handle/11475/30074 | - |
| dc.description.abstract | Structural risk assessments are highly relevant to assure the structural integrity over the whole life-cycle of an aircraft. The Aircraft Structural Integrity Program (ASIP) from the US Air Force introduces design guidance based on deterministic crack growth prediction for safety critical components. Today, with the increase of computational power, probabilistic methods instead of deterministic analysis can be deployed. Probabilistic Risk Assessment (PRA) offers the benefit of taking uncertainty into account and leads to less conservative estimates while meeting safety requirements. Research organizations such as the National Research Council Canada (NRC) or the Defence Science and Technology Organization in Australia (DSTO) are already assessing safety critical elements with PRA. RUAG AG is interested in the application of this method for current and future military aviation systems. Based on the research performed by these organizations, the application of PRA is assessed. The probabilistic calculations are performed with the software tool SMART|DT. Structural engineering and fatigue data is needed for such an assessment, which includes equivalent crack growth data, pre-crack size distributions (EPS), loading distributions and probability of detection (POD). The possibilities of the tool are demonstrated with a case study from the Swiss F/A-18 fleet at knife edge of inner wing trailling edge flap hinge. The results will be compared with analyses from ProDTA from NRC and with PROF from the United States Air Force (USAF). | de_CH |
| dc.language.iso | en | de_CH |
| dc.publisher | International Committee on Aeronautical Fatigue and Structural Integrity | de_CH |
| dc.rights | http://creativecommons.org/licenses/by/3.0/ | de_CH |
| dc.subject | Structural integrity | de_CH |
| dc.subject | Structural risk assessment | de_CH |
| dc.subject | Probabilistic | de_CH |
| dc.subject | ASIP | de_CH |
| dc.subject | Fighter jet | de_CH |
| dc.subject | SMART|DT | de_CH |
| dc.subject.ddc | 629: Luftfahrt- und Fahrzeugtechnik | de_CH |
| dc.title | Practical application of structural risk assessment with SMART DT | de_CH |
| dc.type | Konferenz: Paper | de_CH |
| dcterms.type | Text | de_CH |
| zhaw.departement | School of Engineering | de_CH |
| zhaw.organisationalunit | Zentrum für Aviatik (ZAV) | de_CH |
| dc.identifier.doi | 10.21256/zhaw-30074 | - |
| zhaw.conference.details | 31st Symposium of the International Committee on Aeronautical Fatigue and Structural Integrity (ICAF), Delft, The Netherlands, 28-29 June 2023 | de_CH |
| zhaw.funding.eu | No | de_CH |
| zhaw.originated.zhaw | Yes | de_CH |
| zhaw.parentwork.editor | Marcel, Bos | - |
| zhaw.publication.status | publishedVersion | de_CH |
| zhaw.publication.review | Editorial review | de_CH |
| zhaw.title.proceedings | Proceedings of the 31st Symposium of ICAF | de_CH |
| zhaw.author.additional | No | de_CH |
| zhaw.display.portrait | Yes | de_CH |
| Appears in collections: | Publikationen School of Engineering | |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| 2023_Ferrari-etal_Practical-application-of-structural-risk-asessment-SMART-DT.pdf | 1.11 MB | Adobe PDF |  View/Open |
Show simple item record
Ferrari, V., Liao, M., Ferrari, M., & Guillaume, M. (2023). Practical application of structural risk assessment with SMART DT [Conference paper]. In B. Marcel (Ed.), Proceedings of the 31st Symposium of ICAF. International Committee on Aeronautical Fatigue and Structural Integrity. https://doi.org/10.21256/zhaw-30074
Ferrari, V. et al. (2023) ‘Practical application of structural risk assessment with SMART DT’, in B. Marcel (ed.) Proceedings of the 31st Symposium of ICAF. International Committee on Aeronautical Fatigue and Structural Integrity. Available at: https://doi.org/10.21256/zhaw-30074.
V. Ferrari, M. Liao, M. Ferrari, and M. Guillaume, “Practical application of structural risk assessment with SMART DT,” in Proceedings of the 31st Symposium of ICAF, 2023. doi: 10.21256/zhaw-30074.
FERRARI, Viola, Min LIAO, Michea FERRARI und Michel GUILLAUME, 2023. Practical application of structural risk assessment with SMART DT. In: Bos MARCEL (Hrsg.), Proceedings of the 31st Symposium of ICAF [online]. Conference paper. International Committee on Aeronautical Fatigue and Structural Integrity. 2023. Verfügbar unter: https://www.icaf.aero/icaf2023/proceedings/documents/121.pdf
Ferrari, Viola, Min Liao, Michea Ferrari, and Michel Guillaume. 2023. “Practical Application of Structural Risk Assessment with SMART DT.” Conference paper. In Proceedings of the 31st Symposium of ICAF, edited by Bos Marcel. International Committee on Aeronautical Fatigue and Structural Integrity. https://doi.org/10.21256/zhaw-30074.
Ferrari, Viola, et al. “Practical Application of Structural Risk Assessment with SMART DT.” Proceedings of the 31st Symposium of ICAF, edited by Bos Marcel, International Committee on Aeronautical Fatigue and Structural Integrity, 2023, https://doi.org/10.21256/zhaw-30074.
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