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Effect of Airfoil Thickness, Camber and Reynolds Number on Plunging Airfoil Propulsion

机译：翼型厚度，弯度和雷诺数对插入翼型推进力的影响

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《AIAA Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition》|2009年|P.1-10|共10页
会议地点 Orlando FL(US)
作者
M. Ashraf; J. Young; J. Lai;
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作者单位

University of New South Wales at the Australian Defence Force Academy Canberra ACT Australia;

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1. Reynolds number, thickness and camber effects on flapping airfoil propulsion [J] . M. A. Ashraf, J. Young, J. C. S. Lai Journal of Fluids and Structures . 2011,第2期

机译：雷诺数，厚度和外倾角对拍翼推进的影响
2. Airfoil Thickness Effects on the Thrust Generation of Plunging Airfoils [J] . Meilin Yu, Z. J. Wang, Hui Hu Journal of Aircraft . 2012,第5期

机译：翼型厚度对插入翼型推力产生的影响
3. High fidelity numerical simulation of airfoil thickness and kinematics effects on flapping airfoil propulsion [J] . Meilin Yu, Z. J. Wang, Hui Hu Journal of Fluids and Structures . 2013,第Null期

机译：翼型厚度的高保真数值模拟和运动学对拍翼推进的影响
4. Effect of Airfoil Thickness, Camber and Reynolds Number on Plunging Airfoil Propulsion [C] . M. Ashraf, J. Young, J. Lai American Institute of Aeronautics and Astronautics Aerospace Sciences Meeting Including The New Horizons Forum and Aerospace Exposition . 2009

机译：翼型厚度，壁虎和雷诺数对锚固翼型推进的影响
5. Direct Numerical Simulations of a Cambered NACA 65(1)-412 Airfoil at Low Reynolds Numbers: Flow Separation, Instabilities and Lagrangian Aerodynamics [D] . Klose, Bjoern Fabian. 2021

机译：低雷诺数的弧形Naca 65（1）-412翼型的直接数值模拟：流动分离，稳定性和拉格朗日空气动力学
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. Self-Noise Effects on Aerodynamics of Cambered Airfoils at Low Reynolds Number [O] . Tomoaki Ikeda, Takashi Atobe, Daisuke Fujimoto, 2015

机译：低雷诺数伐木翼型空气动力学的自噪声效应
8. Effect of thickness, camber, and thickness distribution on airfoil characteristics at mach numbers up to 1.0 [R] . Bernard N. Daley, Richard S. Dick 1956

机译：厚度，弯度和厚度分布对马赫数特征的影响，最大为1.0

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