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锥形流乘波体优化设计研究
Viscous Optimized Design of Waverider Derived from Cone Flow

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文摘 随着马赫数的升高,波阻和摩阻增加,形成升阻比“屏障”,而乘波构型飞行器是克服这一屏障的有效途径.本文在Ma∞=4.0~20.0、高度H=24.0~52.0 km、圆锥角Ac=5°~10°的条件下,以升阻比为目标函数,进行了乘波体的优化设计,讨论了对乘波体优化外形的影响因素,并给出全马赫数范围的优化乘波体外形及其气动力结果.
其他语种文摘 This paper is concerned with a method of generating the optimized waverider. Both the wave drag and the friction drag increase as the Mach number becomes higher for hypersonic flow; moreover, a technique difficult will appear which is called L/D barrier. The waverider aerodynamic configuration may be a way to overcome this barrier. A family of optimized hypersonic waverider is generated and studied and the detailed viscous effects are included within the optimization progress itself, The viscous optimized process is completed with maximum lift over drag ratio as optimized objections at the conditions of Ma∞=4.0~20.0, attitudes of H=24.0 52.0 km, and cone angle differed from 5° to 10°. Shapes and aerodynamics of waveriders with Maximum L/D at different Mach numbers are obtained.
来源 航空学报 ,2006,27(1):23-28 【核心库】
关键词 乘波体 ; 优化设计 ; 空气动力学 ; 升阻比
地址

中国科学院力学研究所, 中国科学院高温气体动力学重点实验室, 北京, 100080

语种 中文
文献类型 研究性论文
ISSN 1000-6893
学科 航空
基金 国家自然科学基金资助项目
文献收藏号 CSCD:2347784

参考文献 共 8 共1页

1.  Rasmussen M L. Waverider configurations derived from inclined circular and elliptic cones[J]. Journal of Space Craft and Rockets,1980,17(6):537-545 被引 38    
2.  Kim B S. Optimization of waverider configurations generated from axisymmetric conical flows[J]. Journal of Spacecraft and Rockets,1983,20(5):461-469 被引 3    
3.  Bowcutt K G. Viscous optimized wavriders[R]. Viscous optimized wavriders.AIAA Paper 87-0272,1987 被引 1    
4.  Corda S. Viscous optimized hypersonic wavriders designed from axisymmetric flow fields[R]. Viscous optimized hypersonic wavriders designed from axisymmetric flow fields.AIAA Paper 88-0369,1988 被引 1    
5.  Naruhisa Takashima. Navier-Stokes computation of a viscous optimized waverider[J]. Journal of Space and Rockets,1994,31(3):383-391 被引 16    
6.  Lobia M. Design and analysis of pay-load optimized waveriders[R]. Design and analysis of pay-load optimized waveriders.AIAA Paper 2001-1849,2001 被引 1    
7.  Anderson J D Jr. Fundamentals of aerodynamics[M]. Fundamentals of aerodynamics,2001 被引 3    
8.  Nelder J A. A simplex method for function minimization[J]. Computer Journal,1965,7:308-313 被引 328    
引证文献 10

1 侯志强 高超声速乘波飞行器多学科设计优化研究进展 导弹与航天运载技术(中英文),2009(3):15-19,22
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2 王振清 改良锥导乘波构型的数值研究 哈尔滨工程大学学报,2010,31(6):725-730
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