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Static longitudinal and lateral stability and control characteristics of a model of a swept-wing fighter-bomber-type airplane with a top inlet at Mach numbers from 1.6 to 2.35

机译：一架掠翼式战斗轰炸机型飞机模型的静态纵向和横向稳定性及控制特性，顶部入口的马赫数为1.6至2.35

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Gnos, A Vernon; Kurkowski, Richard L;
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年度 1958
页码 1-56
总页数 56
原文格式 PDF
正文语种 eng
中图分类工业技术;
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3. Influence of aeroelastic control reversal problem in the airplane lateral stability modes [J] . J Bruce Ralphin Rose, GR Jinu Proceedings of the Institution of Mechanical Engineers . 2015,第g3期

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7. Evaluation Method of Longitudinal Static Stability of Tailless Airplane. [O] . Shigenori ANDO, Hiroshi KAJITA 1992

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Static longitudinal and lateral stability and control characteristics of a model of a swept-wing fighter-bomber-type airplane with a top inlet at Mach numbers from 1.6 to 2.35

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