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Development and Persistence of 2D Leading Edge Vortices on Flexible Wings in Low Reynolds Number Flow Applications

机译：低雷诺数流动应用中柔性翅膀上的2D领先边缘涡旋的开发与持久性

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作者
Monteiro, Antonio.;
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作者单位

University of Massachusetts Lowell.;

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授予单位 University of Massachusetts Lowell.;
学科
学位 M.S.Eng.
年度 2021
页码 140 p.
总页数 140
原文格式 PDF
正文语种 eng
中图分类
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专利

1. Vortices evolution in the flow over a sharp leading edge at low Reynolds number [J] . Experimental Thermal and Fluid Science: International Journal of Experimental Heat Transfer, Thermodynamics, and Fluid Mechanics . 2020,第期

机译：在低雷诺数的尖锐前沿的流动中的漩涡演变
2. Leading-edge tubercles delay flow separation for a tapered swept-back wing at very low Reynolds number [J] . Wei Zhaoyu, New T. H., Lian Lian, Ocean Engineering . 2019,第JUNa1期

机译：前缘结节在非常低的雷诺数下延迟了锥形后掠式机翼的气流分离
3. Leading-edge tubercles delay flow separation for a tapered swept-back wing at very low Reynolds number [J] . Wei Zhaoyu, New T. H., Lian Lian, Ocean Engineering . 2019,第Juna1期

机译：前沿结节在非常低的雷诺数下锥形扫反翼延迟流分离
4. A Computational Study of the Impact of Fluid Structure Interaction on the Development and Persistence of 2D LEVs in Low Reynolds Number Flow Applications [C] . Antonio Monteiro, Katherine M. Vail, Anya Jones, AIAA Aviation Forum . 2020

机译：流体结构相互作用对低雷诺数流动应用中2D levs开发和持续性影响的计算研究
5. Development of a Navier-Stokes solver to analyze compressible flow about airfoils and wings altered by leading edge ice accretions. [D] . Falabella, Gregory Joseph. 1999

机译：开发了Navier-Stokes求解器，以分析由前缘冰块增加而改变的机翼和机翼周围的可压缩流。
6. Leading-edge vortices over swept-back wings with varying sweep geometries [O] . William B. Lambert, Mathew J. Stanek, Roi Gurka, 2019

机译：后掠翼上的前缘涡旋具有不同的掠掠几何形状
7. Force production and flow structure of the leading edge vortex on flapping wings at high and low Reynolds numbers [O] . Birch James M., Dickson William B., Dickinson Michael H. 2004

机译：雷诺数高和低时拍翼上前缘涡流的力产生和流动结构

Development and Persistence of 2D Leading Edge Vortices on Flexible Wings in Low Reynolds Number Flow Applications

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