期刊文献+

矩形截面弹体法向气动力计算方法 被引量:1

Method Study of Normal Force Engineering Calculation of Missile with Rectangular Cross sectional Shape
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摘要 对Jorgensen非圆截面弹体的计算公式进行了验证 ,推导出适合于矩形截面弹体的计算公式 ,并对两个具体外形进行了计算。计算结果和风洞实验结果比较 ,法向力系数误差在 10 %以内 . In this paper, an improved engineering method based on Jorgensen's method has been developed to compute normal force of missile with rectangular cross section. The calculated results are compared with the wind tunnel experimental data, and the calculated errors of normal force coefficient are less than 10%,the method is suitable for engineering preliminary calculation.
作者 袁伟 居贤铭
出处 《战术导弹技术》 2003年第3期33-36,共4页 Tactical Missile Technology
关键词 矩形截面弹体 法向气动力 Jorgensen方法 算法 noncircular cross sectional missiles aerodynamics calculation
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参考文献3

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  • 2Asher Sigal.Aerodynamic Characteristics of Rectangular Cross-Sectional bodies at Ma = 0.85,1987.
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二级参考文献5

  • 1中国国防科学技术报告,某型巡航导弹靶弹气动特性低速风洞实验,2000年,4页
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共引文献2

同被引文献14

  • 1孙瑞胜,薛晓中,孙传杰,洪建华.三角形截面弹芯的飞行稳定特性[J].南京理工大学学报,2007,31(1):6-9. 被引量:10
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