| 适用于概念设计的再入飞行器外形优化设计方法 |
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| 引用本文： | 张珍铭,丁运亮,刘毅,张铁亮. 适用于概念设计的再入飞行器外形优化设计方法[J]. 航空学报, 2011, 32(11): 1971-1979. DOI: 11-1929/V.20110526.1753.017 |
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| 作者姓名： | 张珍铭 丁运亮 刘毅 张铁亮 |
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| 作者单位： | 1. 南京航空航天大学飞行器先进设计技术国防重点学科实验室,江苏南京,210016
2. 同济大学航空航天与力学学院,上海,200092 |
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| 基金项目： | 国家“863”计划~~ |
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| 摘 要： | 面向再入飞行器概念设计,提出了一种实现外形多目标优化的综合设计方法.基于类型函数/形状函数变换技术建立参数化几何模型,实现了以少量设计变量描述较大范围的设计空间；引入考虑真实气体效应的工程方法估算气动特性,应用非支配排序遗传算法(NSGA-Ⅱ)实现考虑升阻比和容积利用率最大化以及热流量最小化的多目标优化设计；通过减法聚...
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| 关 键 词： | 再入飞行器 概念设计 类型函数/形状函数 气动外形优化 多目标优化 分层图 |
| 收稿时间： | 2011-01-17; |
Shape Optimization Design Method for the Conceptual Design of Reentry Vehicles |
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| ZHANG Zhenming,DING Yunliang,LIU Yi,ZHANG Tieliang. Shape Optimization Design Method for the Conceptual Design of Reentry Vehicles[J]. Acta Aeronautica et Astronautica Sinica, 2011, 32(11): 1971-1979. DOI: 11-1929/V.20110526.1753.017 |
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| Authors: | ZHANG Zhenming DING Yunliang LIU Yi ZHANG Tieliang |
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| Affiliation: | 1.Key Laboratory of Fundamental Science for National Defense—Advanced Design Technology of Flight Vehicle, Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China 2.School of Aerospace Engineering and Applied Mechanics,Tongji University,Shanghai 200092,China |
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| Abstract: | This paper presents a multi-objective shape optimization method for the conceptual design of reentry vehicles.The class function/shape function transformation technique is used to represent briefly the various shapes of the reentry vehicles with relatively few variables.The aerodynamic characteristics of the vehicles are predicted by an engineering method which accounts for the effects of real-gas flow across the oblique shock wave.The multi-objective evolutionary algorithm non-dominated sorting genetic alg... |
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| Keywords: | reentry vehicle conceptual design class function/shape function aerodynamic shape optimization multi-objective optimization level diagram. |
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