Fluid-Structure Interation of a Rigid Wing for Minesto Deep Green, a Tidal Energy Device

Daniel Hung, A. Mosquera, D. Mcglinchey
{"title":"Fluid-Structure Interation of a Rigid Wing for Minesto Deep Green, a Tidal Energy Device","authors":"Daniel Hung, A. Mosquera, D. Mcglinchey","doi":"10.59972/ef8rt5x2","DOIUrl":null,"url":null,"abstract":"Fluid structure interaction (FSI) analysis has been performed on the main wing structure of an underwater renewable energy tidal flow device using methods of different fidelity. A lower fidelity method represented the wing as a series of beams (1D line elements) which deflect and rotate under hydrodynamic load. These deflections and rotations were used to update the geometry for the hydrodynamic model where updated forces and moments were calculated using potential flow theory with integral boundary layer (2D panel methods). The higher fidelity method represented the wing using a combination of 3D solid elements for the foam structure inside the wing and 2D shell elements for the carbon fibre wing stiffening beams and fibre glass wing skin. The results of a modal analysis of the wing structure were used in a 3D CFD simulation that coupled the modal equations with the Navier-Stokes equations to compute the deformed shape of the wing under hydrodynamic load. In both cases, the maximum deformations of the wing were quite small (<25mm) compared to the wing size (12m span, 3.3m maximum chord) but the effect on hydrodynamic characteristics was quite different. The low fidelity analysis made the assumption that the wing cross-sectional shape profile did not change, although it could move and rotate. There was no significant change in the predicted hydrodynamic characteristics between the deformed and undeformed wing shapes. The contribution of the foam to the stiffness of the wing was not included in the low fidelity analysis as it was thought to be minor contributor due the much lower Young’s Modulus compared to the carbon fibre and fibre glass of the main wing structure. In contrast, the high fidelity method resulted in about a 15% reduction in lift and 6% in drag forces due to deformation of the wing cross-section profiles rather than bending and twisting of the wing which the low fidelity analysis showed not to be significant. The effect on energy yield of these changes is estimated to be very small.","PeriodicalId":183819,"journal":{"name":"NAFEMS International Journal of CFD Case Studies","volume":"24 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2020-02-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"0","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"NAFEMS International Journal of CFD Case Studies","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.59972/ef8rt5x2","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 0

Abstract

Fluid structure interaction (FSI) analysis has been performed on the main wing structure of an underwater renewable energy tidal flow device using methods of different fidelity. A lower fidelity method represented the wing as a series of beams (1D line elements) which deflect and rotate under hydrodynamic load. These deflections and rotations were used to update the geometry for the hydrodynamic model where updated forces and moments were calculated using potential flow theory with integral boundary layer (2D panel methods). The higher fidelity method represented the wing using a combination of 3D solid elements for the foam structure inside the wing and 2D shell elements for the carbon fibre wing stiffening beams and fibre glass wing skin. The results of a modal analysis of the wing structure were used in a 3D CFD simulation that coupled the modal equations with the Navier-Stokes equations to compute the deformed shape of the wing under hydrodynamic load. In both cases, the maximum deformations of the wing were quite small (<25mm) compared to the wing size (12m span, 3.3m maximum chord) but the effect on hydrodynamic characteristics was quite different. The low fidelity analysis made the assumption that the wing cross-sectional shape profile did not change, although it could move and rotate. There was no significant change in the predicted hydrodynamic characteristics between the deformed and undeformed wing shapes. The contribution of the foam to the stiffness of the wing was not included in the low fidelity analysis as it was thought to be minor contributor due the much lower Young’s Modulus compared to the carbon fibre and fibre glass of the main wing structure. In contrast, the high fidelity method resulted in about a 15% reduction in lift and 6% in drag forces due to deformation of the wing cross-section profiles rather than bending and twisting of the wing which the low fidelity analysis showed not to be significant. The effect on energy yield of these changes is estimated to be very small.
潮汐能装置Minesto Deep Green刚性机翼流固耦合
采用不同保真度的方法对水下可再生能源潮汐装置主翼结构进行了流固耦合分析。一种较低保真度的方法将机翼表示为在水动力载荷下偏转和旋转的一系列梁(一维线元)。这些偏转和旋转被用来更新水动力模型的几何形状,其中更新的力和力矩使用积分边界层势流理论(二维面板方法)计算。更高保真度的方法使用三维实体元素来表示机翼内部的泡沫结构,二维壳元素用于碳纤维机翼加强梁和玻璃纤维机翼蒙皮。利用机翼结构模态分析结果进行了三维CFD仿真,将模态方程与Navier-Stokes方程耦合,计算了机翼在水动力载荷作用下的变形形状。在这两种情况下,机翼的最大变形量(<25mm)都小于机翼尺寸(跨度12m,最大弦长3.3m),但对水动力特性的影响却大不相同。低保真度分析假设机翼横截面形状轮廓没有变化,尽管它可以移动和旋转。变形翼与未变形翼之间的预测水动力特性没有显著变化。泡沫对机翼刚度的贡献没有包括在低保真度分析中,因为与主要机翼结构的碳纤维和玻璃纤维相比,泡沫的杨氏模量要低得多,因此它被认为是次要的贡献者。相比之下,高保真度方法导致升力减少15%,阻力减少6%,这是由于机翼横截面轮廓的变形,而不是低保真度分析显示的机翼弯曲和扭曲。据估计,这些变化对产能的影响非常小。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
求助全文
约1分钟内获得全文 求助全文
来源期刊
自引率
0.00%
发文量
0
×
引用
GB/T 7714-2015
复制
MLA
复制
APA
复制
导出至
BibTeX EndNote RefMan NoteFirst NoteExpress
×
提示
您的信息不完整,为了账户安全,请先补充。
现在去补充
×
提示
您因"违规操作"
具体请查看互助需知
我知道了
×
提示
确定
请完成安全验证×
copy
已复制链接
快去分享给好友吧!
我知道了
右上角分享
点击右上角分享
0
联系我们:info@booksci.cn Book学术提供免费学术资源搜索服务,方便国内外学者检索中英文文献。致力于提供最便捷和优质的服务体验。 Copyright © 2023 布克学术 All rights reserved.
京ICP备2023020795号-1
ghs 京公网安备 11010802042870号
Book学术文献互助
Book学术文献互助群
群 号:481959085
Book学术官方微信