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A theoretical analysis of a simple aerodynamic device to improve the longitudinal damping of a cruciform missile configuration at supersonic speeds

机译：一种简单的空气动力学装置的理论分析，以提高超音速下十字形导弹结构的纵向阻尼

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作者
Clements, James E;
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年度 1955
页码 1-37
总页数 37
原文格式 PDF
正文语种 eng
中图分类工业技术;
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入库时间 2022-08-29 11:19:32

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7. A High Angle Of Attack Aerodynamic Prediction Code For Cruciform Missile Configurations.ud [O] . Venugopal S, Krishnamurthy M 1992

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A theoretical analysis of a simple aerodynamic device to improve the longitudinal damping of a cruciform missile configuration at supersonic speeds

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