The finite element algorithm for transonic flows about wing and blended wing-body configuration is investigated based on the full potential equations.
从全速位方程出发研究了机翼和翼身融合体跨音速绕流的有限元算法。
Using the pressure minimum integral, finite element equations are obtained based on the full potential equation.
从全速位方程出发，利用压强极小积分得到有限元方程组。
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