基于活塞法的高超声速气动力计算程序开发

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摘要高超声速飞行器设计中面临的高超声速流问题促进了对高超声速气动弹性和气动热弹性的研究,高超声速飞行器在高速飞行时会带来气动热以及气动载荷,在来流、气动力、结构之间产生了复杂的相互作用。并且在气动分析中,速度扰动相对于声速来说很大,高速气流的控制方程需要保留非线性特征。

作者刘金鑫

机构地区南京航空航天大学

出处《江苏航空》 2021年第3期17-20,共4页 Jiangsu Aviation

关键词高超声速流高超声速飞行器气动弹性气动载荷气动热弹性气动力高速气流气动分析

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江苏航空

2021年第3期

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