AIAA Journal. 1992;30(3):697-702. doi: 10.2514/3.10974 Q13.22025
Effect of airfoil (trailing-edge) thickness on the numerical solution of panel methods based on the Dirichlet boundary condition
翼型(后缘)厚度对基于狄利克雷边界条件的面元法数值解的影响
DOI: 10.2514/3.10974
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