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Direct Numerical Simulations of a Cambered NACA 65(1)-412 Airfoil at Low Reynolds Numbers: Flow Separation, Instabilities and Lagrangian Aerodynamics

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

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作者
Klose, Bjoern Fabian.;
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作者单位

University of California San Diego.;

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授予单位 University of California San Diego.;
学科
学位 Ph.D.
年度 2021
页码 217 p.
总页数 217
原文格式 PDF
正文语种 eng
中图分类
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3. Direct numerical simulation of flow separation around a NACA 0012 airfoil [J] . Hua Shan, Li Jiang, Chaoqun Liu Computers & Fluids . 2005,第9期

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4. Direct Numerical Simulation of Flows over an NACA-0012 Airfoil at Low and Moderate Reynolds Numbers [C] . P. Balakumar AIAA Fluid Dynamics Conference;AIAA Aviation Forum . 2017

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5. Direct Numerical Simulations of a Cambered Ca 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CA 65（1）-412翼型的直接数值模拟：流量分离，无限度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

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7. Direct Numerical Simulations of Transonic Flow Around an Airfoil at Moderate Reynolds Numbers [O] . Markus Zauner, Nicola De Tullio, Neil D. Sandham 2019

机译：在适度的雷诺数翼型周围跨越跨越跨型流动的直接数值模拟
8. Direct Numerical Simulation of Flows over an NACA-0012 Airfoil at Low and Moderate Reynolds Numbers. [R] . Balakumar, P. 2017

机译：NaCa-0012型翼型在低和中等雷诺数下的直接数值模拟。

Direct Numerical Simulations of a Cambered NACA 65(1)-412 Airfoil at Low Reynolds Numbers: Flow Separation, Instabilities and Lagrangian Aerodynamics

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