AIAA Scitech 2020 Forum 2020
DOI: 10.2514/6.2020-2046
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Computational Study of Flapping Wing Response to Vertical Gusts at Low Reynolds Numbers

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Cited by 2 publications
(3 citation statements)
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“…A high-order accurate computational fluid dynamics (CFD) solver based on unstructured moving/deformable grids [14][15][16][17] is used to simulate unsteady flows over a pitching airfoil. This numerical framework has been extensively validated with experiments [8][9][10], and has been used to investigate unsteady flapping wing aerodynamics over a broad range of flow conditions [18][19][20][21][22]. Readers are referred to [15,17] for more technical details about the numerical framework.…”
Section: Pitching Wing Modelmentioning
confidence: 99%
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“…A high-order accurate computational fluid dynamics (CFD) solver based on unstructured moving/deformable grids [14][15][16][17] is used to simulate unsteady flows over a pitching airfoil. This numerical framework has been extensively validated with experiments [8][9][10], and has been used to investigate unsteady flapping wing aerodynamics over a broad range of flow conditions [18][19][20][21][22]. Readers are referred to [15,17] for more technical details about the numerical framework.…”
Section: Pitching Wing Modelmentioning
confidence: 99%
“…๐‘‰/๐‘ˆ โˆž ). The details of the numerical modeling and gust-airfoil interaction flow physics can be found in [8][9][10]. Figure 1 shows a nominal instantaneous vorticity field in a gust-wing interaction at Reynolds number 1,000.…”
Section: Pitching Wing Modelmentioning
confidence: 99%
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