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Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.16 of a Blunt-Nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins

机译：具有三角形截面和固定三角形鳍的钝头导弹模型的1.60至2.16马赫数的空气动力学特性

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作者
Monta, W. J.;
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年度 1971
页码 1-2
总页数 2
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Aerodynamic characteristics ; Blunt bodies ; Graphs (charts) ; Missile design ; Nose cones ; Static stability ; Wind tunnel models;

机译：空气动力学特性;钝体;图形（图表）;导弹设计;鼻锥;静态稳定性;风洞模型;
入库时间 2022-08-29 11:13:44

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Aerodynamic Characteristics at Mach Numbers from 1.60 to 2.16 of a Blunt-Nose Missile Model Having a Triangular Cross Section and Fixed Triform Fins

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