Flapping-Wing Fluid–Structural Interaction Analysis Using Corotational Triangular Planar Structural Element
| Autor: | SangJoon Shin, JunYoung Kwak, Seungsoo Lee, Haeseong Cho, Namhun Lee |
|---|---|
| Rok vydání: | 2016 |
| Předmět: |
Engineering
business.industry Structure (category theory) Aerospace Engineering Structural engineering Degrees of freedom (mechanics) Computational fluid dynamics 01 natural sciences Displacement (vector) 010305 fluids & plasmas Structural element 010101 applied mathematics Complex geometry Planar 0103 physical sciences 0101 mathematics Element (category theory) business |
| Zdroj: | AIAA Journal. 54:2265-2276 |
| ISSN: | 1533-385X 0001-1452 |
| DOI: | 10.2514/1.j054567 |
| Popis: | In this paper, a triangular planar element is developed for a geometrically nonlinear structural analysis, which includes the drilling degrees of freedom using a corotational framework. Based on the assumptions of a small degree of strain and large displacement, the corotational framework allows an accurate geometrically nonlinear structural analysis. The presently improved corotational framework accommodates in-plane rotational behavior (that is, the drilling degrees of freedom) by using the corotational framework corresponding to a solidlike planar element. It focuses on triangular planar elements that will be useful for three-dimensional analysis using a reduced number of degrees while targeting a structure with a complex geometry, such as a flapping wing. Regarding the present analysis, validation by solving both static and time-transient problems is conducted. The fluid–structure interaction framework is then developed by using the present structural analysis. During this validation procedure, the pr... |
| Databáze: | OpenAIRE |
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