A field-panel method for subsonic and transonic 3D wing calculation

被引：0

作者：

Fokin, D ^{[1
]}

Wagner, S ^{[1
]}

机构：

[1] Univ Stuttgart, IAG, D-70550 Stuttgart, Germany

来源：

ZEITSCHRIFT FUR ANGEWANDTE MATHEMATIK UND MECHANIK | 2001年 / 81卷

关键词：

D O I：

暂无

中图分类号：

O29 [应用数学];

学科分类号：

070104 ;

摘要：

The development of fast numerical methods for calculating sub- and transonic flow over 3D configurations is important for numerical optimization purposes. One efficient approach, namely field panel method, is based on the boundary-element methods solving the full potential equation (see e.g. [1]). The algorithm incorporates panel methods for calculating the basic incompressible flow and compressible field iterations. The purpose of the present work is to develop a mathematically well based and efficient numerical field-panel method for the analysis of transonic flow over 3D wings, that could be further used for design and optimisation of transonic wings in a given range of free stream Mach numbers.

引用

页码：S453 / S454

页数：2

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