Shape optimization and material gradient design of the sharp hot structure

被引：8

作者：

Ma, Yinji ^{[1
]}

Yao, Xuefeng ^{[1
]}

Su, Yunquan ^{[1
]}

机构：

[1] Tsinghua Univ, Dept Engn Mech, Appl Mech Lab, Beijing 100084, Peoples R China

来源：

ACTA ASTRONAUTICA | 2014年 / 103卷

基金：

中国国家自然科学基金;

关键词：

Multi-objective optimization; Sharp hot structure; Genetic algorithm; Gradient materials; Design; LAMINAR HEAT TRANSFER; EVOLUTIONARY ALGORITHMS; MULTIOBJECTIVE OPTIMIZATION; GENETIC ALGORITHM; REENTRY VEHICLE; BODIES;

D O I：

10.1016/j.actaastro.2014.06.043

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

In this paper, the shape and material gradient of the sharp hot structure are designed and optimized to meet the hypersonic flight conditions. First, based on the single-objective optimization for the volume, the aerodynamic loading and the heat flow, respectively, the genetic algorithm (GA) is employed for optimizing the shape of the sharp hot structure. Second, the shape of the sharp hot structure is optimized using multi-objective GA by means of the objectives of the volume, the aerodynamic loading and the heat flow. Finally, the ABAQUS software is used to simulate both the temperature and the stress distribution with different material gradient distributions for the sharp hot structure. The optimal distributions of gradient materials for the sharp hot structure are proposed. The results will provide an important guidance for the design of the sharp hot structure. (C) 2014 IAA. Published by Elsevier Ltd. All rights reserved.

引用

页码：106 / 112

页数：7

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