Static loads evaluation in a flexible aircraft using high-fidelity fluid–structure iteration tool (E2-FSI): extended version

Author:

Verri Angelo A.,Bussamra Flávio L. S.,de Morais Kelvin C.,Becker Gilberto Guerra,Cesnik Carlos E. S.,Luque Filho Gilberto B.,de Oliveira Leonardo C.

Publisher

Springer Science and Business Media LLC

Subject

Mechanical Engineering,General Engineering,Aerospace Engineering,Automotive Engineering,Industrial and Manufacturing Engineering,Applied Mathematics

Cited by 10 articles. 订阅此论文施引文献 订阅此论文施引文献,注册后可以免费订阅5篇论文的施引文献,订阅后可以查看论文全部施引文献

1. Static aeroelastic rolling of a highly flexible wing: Pazy wing with aileron;Journal of the Brazilian Society of Mechanical Sciences and Engineering;2024-07-22

2. Outcomes of Nonlinear Static Aeroelasticity for Wing Stress and Buckling Applied to a Transport Aircraft;AIAA SCITECH 2024 Forum;2024-01-04

3. A Dynamic Nonlinear Inertia Relief Formulation;AIAA SCITECH 2024 Forum;2024-01-04

4. Review of fluid-structure interaction algorithm and its application in the aviation field;Ninth International Conference on Mechanical Engineering, Materials, and Automation Technology (MMEAT 2023);2023-10-25

5. Design, development and approbation of the numerical technique in simulating the wing aeroelastic state based on the finite element and control volumes methods;Engineering Journal: Science and Innovation;2023-07

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