| 乘波飞行器的优化设计和气动热计算研究 |
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| 引用本文： | 梅东牧,武哲,李天.乘波飞行器的优化设计和气动热计算研究[J].航空计算技术,2008,38(6):13-16. |
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| 作者姓名： | 梅东牧 武哲 李天 |
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| 作者单位： | 北京航空航天大学,航空科学与工程学院,北京,100083;沈阳飞机设计研究所,辽宁,沈阳,110035 |
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| 摘 要： | 以高超声速技术为研究背景,开展高超声速乘波飞行器设计方法研究.在已有乘波构型生成方法基础上,采用相交楔锥生成多级压缩的乘波构形.并通过对乘波器的前缘进行钝化,进行了气动热特性数值研究.使乘波体在气动力层面上具有尖前缘,保持高升阻比特性,而在气动热层面上具有钝前缘,降低气动加热强度.结果表明,这为高超声速飞行器的气动防热设计开辟了新途径.
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| 关 键 词： | 高超声速乘波飞行器 气动热 数值模拟 |
Research of the Waverider Optimization Design and Aerothermodynamics |
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| MEI Dong-mu,WU Zhe,LI Tian.Research of the Waverider Optimization Design and Aerothermodynamics[J].Aeronautical Computer Technique,2008,38(6):13-16. |
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| Authors: | MEI Dong-mu WU Zhe LI Tian |
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| Institution: | MEI Dong-mu1,WU Zhe1,LI Tian2(1.School of Aeronautics Science , Technology,Beijing University of Aeronautics , Astronautics,Beijing 100083,China,2.Shenyang Aircraft Design , Research Institute,Shenyang 110035,China) |
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| Abstract: | To study hypersonic technology,several methods are investigated to design Waverider aerodynamic configuration.Base on the study of waverider,a new conceptual hypersonic waverider is designed by showing a sharp leading edge in aerodynamic perspective and an artificially blunt leading edge,in aerothermal perspective.The results show that it can be used for the design of aerothermodynamics. |
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| Keywords: | hypersonic waverider aerothermodynamics numerical simulation |
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