Effect of airfoil (trailing-edge) thickness on the numerical solution of panel methods based on the dirichlet boundary condition

被引：0
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作者：
Yon, Steven [1 ]
Katz, Joseph [1 ]
Plotkin, Allen [1 ]
机构：
[1] San Diego State Univ, San Diego, United States
来源：
AIAA journal | 1992年 / 30卷 / 03期
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页码：697 / 702
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