IMECH-IR  > 高温气体动力学国家重点实验室
吸气式高超声速飞行器上壁面多约束/多目标优化设计和分析
崔凯; 高太元; 胡守超; 王秀平
Source Publication第四届高超声速科技学术会议会议日程及摘要集
2011
Pages4
Conference Name第四届高超声速科技学术会议
Conference Date2011
Conference Place中国海南三亚
Abstract<正>针对一种吸气式高超声速飞行器构型,应用自行提出的基于修正量的外形参数化方法对其上表面中心型线进行参数化,采用动遗传算法针对二维构型首先在考虑容积约束、升力约束等条件下,以升阻比为目标进行了多约束优化设计。其次同时以容积和升阻比为目标开展了多目标优化设计。最后比较了二维/三维情况的气动性能。结果表明对于飞行器上壁面而言,1)针对二维条件下的优化设
Keyword高超声速 遗传算法 多目标优化 升阻比 容积
DepartmentLHD气动布局优化与计算方法
Funding Organization中国力学学会、中国科学院高超声速科技中心、中国科学院力学研究所、高温气体动力学国家重点实验室
URL查看原文
Language中文
Document Type会议论文
Identifierhttp://dspace.imech.ac.cn/handle/311007/45281
Collection高温气体动力学国家重点实验室
Corresponding Author崔凯
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崔凯,高太元,胡守超,等. 吸气式高超声速飞行器上壁面多约束/多目标优化设计和分析[C]第四届高超声速科技学术会议会议日程及摘要集,2011:4.
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