Computer-aided design analysis of hypersonic aircraft air intake geometry

被引：0
|
作者：
Gainutdinov V.G. [1 ]
机构：
[1] Tupolev Kazan National Research Technical University, Kazan
来源：
Russian Aeronautics (Iz VUZ) | 2013年 / 56卷 / 3期
关键词：
air intake geometry; numerical algorithm; optimization;
D O I：
10.3103/S1068799813030094
中图分类号：
学科分类号：
摘要：
In this paper, a numerical algorithm for design analysis and optimization of hypersonic aircraft air intake geometry is presented. The analysis data show that the algorithms being proposed are sufficiently accurate for preliminary analysis and optimization of design parameters. © 2013 Allerton Press, Inc.
引用
收藏
页码：274 / 279
页数：5
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