Design and Optimization of a Two-Element Wing Airfoil in a Subsonic Viscous Flow

被引：0
|
作者：
Volkov, P. A.
Il'yinskii, N. B.
机构：
来源：
FLUID DYNAMICS | 2006年 / 41卷 / 01期
基金：
俄罗斯基础研究基金会;
关键词：
optimization; boundary layer; Chaplygin gas; inverse boundary-value problems of aerohydrodynamics; two-element wing airfoil;
D O I：
10.1007/s10697-006-0018-y
中图分类号：
O3 [力学];
学科分类号：
08 ; 0801 ;
摘要：
A numerical and analytical solution of the problem of designing a two-element wing airfoil providing maximum lift-drag ratio in a subsonic viscous flow is presented. In order to bring the theoretical results closer to the facts, viscosity and compressibility are taken into account within the framework of boundary layer theory and the Chaplygin gas model, respectively.
引用
收藏
页码：21 / 28
页数：8
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