Static loads evaluation in a flexible aircraft using high-fidelity fluid–structure iteration tool (E2-FSI): extended version
Journal of the Brazilian Society of Mechanical Sciences and Engineering, ISSN: 1806-3691, Vol: 42, Issue: 1
2020
- 12Citations
- 18Captures
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Example: if you select the 1-year option for an article published in 2019 and a metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019. If you select the 3-year option for the same article published in 2019 and the metric category shows 90%, that means that the article or review is performing better than 90% of the other articles/reviews published in that journal in 2019, 2018 and 2017.
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Article Description
This paper presents a fluid–structure iteration method applied as a study case to a conventional transport aircraft with wing aspect ratio of 12. It evaluates the nonlinear structure effect on the calculation of static limit loads. The numerical tool presented herein is named E2-FSI, which stands for nonlinear high-fidelity static fluid–structure iteration, developed for high flexibility static aeroelastic evaluations. A discussion about the use and the applicability of high-fidelity static fluid–structure iteration for the calculation of static loads is presented as part of the conclusion, for both current and future conventional transport aircraft.
Bibliographic Details
http://www.scopus.com/inward/record.url?partnerID=HzOxMe3b&scp=85077399976&origin=inward; http://dx.doi.org/10.1007/s40430-019-2154-4; http://link.springer.com/10.1007/s40430-019-2154-4; http://link.springer.com/content/pdf/10.1007/s40430-019-2154-4.pdf; http://link.springer.com/article/10.1007/s40430-019-2154-4/fulltext.html; https://dx.doi.org/10.1007/s40430-019-2154-4; https://link.springer.com/article/10.1007/s40430-019-2154-4
Springer Science and Business Media LLC
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