The airfoil shape is then adjusted until the desired velocity distribution is obtained.
然后是调整翼型的形状，直到取得预期的速度分布。
Direct methods are based on the design-by-analysis approach in which the airfoil shape is specified first.
直接的方法是基于设计逐案分析的方法是机翼形状指定第一。
The variable-domain variation is a specific tool of handling unknown boundaries and suitable for designing airfoil shape.
变域变分是一种处理未知界面的独特工具，极适合于气动外形的设计求解。
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