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Aerodynamic Force and Flow Structures of Two Airfoils in Flapping Motions

机译：拍打时两个翼型的气动力和流动结构议案

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Aerodynamic force and flow structures of two airfoils in tandem configurationperforming flapping motions are studied, using the method of solving theNavier-Stokes equations in moving overset grids. Three typical phasedifferences between the fore- and aft-airfoil flapping cycles are considered.

机译：研究了两个翼型在襟翼运动中的气动力和流动结构，采用了在运动的交叠网格中求解Navier-Stokes方程的方法。考虑了前翼和后翼拍打周期之间的三个典型相位差。

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Lan, Shi Long; Sun, Mao;
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年度 2004
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专利

1. AERODYNAMIC FORCE AND FLOW STRUCTURES OF TWO AIRFOILS IN FLAPPING MOTIONS [J] . 兰世隆, 孙茂力学学报：英文版 . 2001 ,第004期

机译：襟翼摆动运动中两种翼型的气动力和流动结构。
2. Assessing aerodynamic force estimation with experiments and simulations of flapping-airfoil flows on the verge of three-dimensionality [J] . Moriche M., Raiola M., Discetti S., Proceedings of the Institution of Mechanical Engineers . 2020 ,第2期

机译：借助翼型气流在三维边界上的实验和仿真评估空气动力估算
3. Aerodynamic forces and flow structures of the leading edge vortex on a flapping wing considering ground effect [J] . Van Truong T., Byun D., Kim M.J., Bioinspiration & biomimetics . 2013 ,第3期

机译：考虑地面效应的襟翼前缘涡流的空气动力和流动结构
4. Low order modelling of flow features and aerodynamic forces in flapping airfoils [C] . Marco Raiola, Stefano Discetti, Andrea Ianiro AIAA applied aerodynamics conference;AIAA aviation forum . 2016

机译：翼型襟翼流动特性和空气动力的低阶建模
5. Detection of aerodynamic flow structures during hummingbird like flapping motion using hot film anemometry [D] . Vanier, Blake 2008

机译：使用热膜风速仪检测蜂鸟像拍打运动期间的空气流动结构
6. Flexible Flaps Inspired by Avian Feathers Can Enhance Aerodynamic Robustness in low Reynolds Number Airfoils [O] . Yuta Murayama, Toshiyuki Nakata, Hao Liu 2021

机译：灵活的襟翼灵感来自禽羽毛可以增强低雷诺数翼型的空气动力学鲁棒性
7. Measurement of Unsteady Aerodynamic Forces of 3D Flapping Wing in Hovering Flight (2nd Report, Comparison Between Trapezoidal and Sinusoidal Flapping Motions) [O] . Hiroto NAGAI, Takumi ITO, Keita MIURA, 2008

机译：在悬停飞行中的3D拍打翼的非稳态空气动力测量（第2报告，梯形和正弦拍打运动的比较）
8. Measurements of aerodynamic characteristics of a 35 degree sweepback NACA 65-009 airfoil model with 1/4 chord flap having 31 percent flap chord overhang balance by the NACA wing flow method [R] . Johnson, Harold I, Goodman, Harold R 1950

机译：通过NaCa机翼流动方法测量35度后掠NaCa 65-009翼型模型的空气动力学特性，其中1/4弦翼具有31％的襟翼弦悬伸平衡

Aerodynamic Force and Flow Structures of Two Airfoils in Flapping Motions

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