Optimization of the Aerodynamic Configuration of the Isolated Wing for the Second-Generation Supersonic Passenger Aircraft

被引：0
|
作者：
Shirokov M.V. [1 ]
Strelets D.Y. [1 ]
Bashkirov I.G. [2 ]
机构：
[1] Moscow Aviation Institute (National Research University), Volokolamskoe sh. 4, Moscow
[2] Central Aerohydrodynamic Institute (TsAGI), ul. Zhukovskogo 1, Zhukovsky
来源：
Russian Aeronautics | 2024年 / 67卷 / 01期
关键词：
algorithm; geometry parameterization; optimization; supersonic passenger aircraft; wing;
D O I：
10.3103/S1068799824010082
中图分类号：
学科分类号：
摘要：
Abstract: The paper proposes the technique based on solutions of the Reynolds-averaged Navier–Stokes (RANS) equations for selecting the optimal aerodynamic configuration of the wing at the early design stages. The general optimization algorithm is presented taking into account a great number of design variables and constraints. A parameterization approach is presented that allows the efficient manipulation of the wing geometry. The results of aerodynamic optimization of the isolated wing of the second-generation supersonic passenger aircraft are presented. © Allerton Press, Inc. 2024.
引用
收藏
页码：70 / 79
页数：9
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