再入飞行器尾迹流场及其雷达散射效应研究

IMECH-IR > 力学所知识产出(1956-2008)

	再入飞行器尾迹流场及其雷达散射效应研究
	牛家玉; 许国斌; 曹荣达; 任爱民
Source Publication	空气动力学学报
	1996
Volume	14 Issue:4 Pages:422
ISSN	0258-1825
Abstract	对再入飞行器等离子体尾迹及其雷达散射特性进行了分析、研究和大量的计算.讨论了物形、流场各因素对尾迹雷达散射截面的影响.流场计算使用准一维粘性尾迹方程,以修正基尔方法(多值法)求解,用一阶Born近似完成亚密雷达散射截面(RCS)计算.给出了研究结果.、
Keyword	等离子体尾迹雷达散射截面再入飞行器湍流回波特性
Indexed By	CSCD
Language	中文
CSCD ID	CSCD:344845
Citation statistics
Document Type	期刊论文
Identifier	http://dspace.imech.ac.cn/handle/311007/35548
Collection	力学所知识产出(1956-2008)
Corresponding Author	牛家玉
Recommended Citation GB/T 7714	牛家玉,许国斌,曹荣达,等. 再入飞行器尾迹流场及其雷达散射效应研究[J]. 空气动力学学报,1996,14,4,:422.
APA	牛家玉,许国斌,曹荣达,&任爱民.(1996).再入飞行器尾迹流场及其雷达散射效应研究.空气动力学学报,14(4),422.
MLA	牛家玉,et al."再入飞行器尾迹流场及其雷达散射效应研究".空气动力学学报 14.4(1996):422.

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