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Euromech 75 Lecture: Iterative Calculation of Subcritical Flow Around Thick Cambered Wings: Direct and Design Problems.

机译:Euromech 75讲座:厚厚的弧形翼周围亚临界流动的迭代计算:直接和设计问题。

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This is a written version of a lecture given by the author at Euromech Colloquium 75 which was held at Rhode, near Braunschweig in May 1976. The subject of the colloquium was 'The calculation of flow fields by panel methods' and this paper describes iterative calculations of the classic problems of steady inviscid flow around a thick cambered wing, providing improved accuracy in relation to the so-called RAE Standard Method. (Author)

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