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Calculation of Airfoil Flutterby an Euler Method with Approximate Boundary Conditions

机译：近似边界条件下的欧拉方法计算翼型颤振

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《AIAA Computational Fluid Dynamics Conference》|2003年|1-10|共10页
会议地点 Orlando FL(US)
作者
C. Gao; S. Luo; F. Liu; D. Schuster;
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University of California Irvine CA;

NASA Langley Hampton VA;

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1. Calculation of Airfoil Flutter by an Euler Method with Approximate Boundary Conditions [J] . Chao Gao, Shuchi Yang, Shijun Luo, AIAA Journal . 2005,第2期

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2. NUMERICAL SOLUTION OF THE UNSTEADY EULER EQUATIONS FOR AIRFOILS USING APPROXIMATE BOUNDARY CONDITIONS [J] . 高超, 罗时钧, 刘锋力学学报：英文版 . 2003,第005期

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3. Calculation of Periodic Metal Nanostructures via the Method of Approximate Boundary Conditions [J] . A. M. Lerer, V. V. Makhno, P. V. Makhno, Journal of Communications Technology and Electronics . 2007,第4期

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4. Calculation of Airfoil Flutterby an Euler Method with Approximate Boundary Conditions [C] . American Institute of Aeronautics and Astronautics Computational Fluid Dynamics Conference . 2003

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6. Approximate Solution for Electroosmotic Flow of Power-Law Fluids in a Planar Microchannel with Asymmetric Electrochemical Boundary Conditions [O] . WooSeok Choi, Sungchan Yun, Du-Soon Choi 2018

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7. Calculations of Flow around an Airfoil with a Trailing Edge Flap by Use of an Immersed Boundary Method [O] . Behrens Tim, Zhu Wei Jun, Shen Wen Zhong, 2009

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8. Development and Validation of Characteristic Boundary Conditions for Cell-Centered Euler Flow Calculations with a Shock-Fee Airfoil [R] . van den Berg, J. I., Boerstoel, J. W. 1989

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