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Static lateral stability and control characteristics of a model of a 45 degree swept-wing fighter airplane with various vertical tails at Mach numbers of 1.41, 1.61, and 2.01

机译：具有各种垂直尾部的马力数为1.41,1.61和2.01的45度后掠翼战斗机模型的静态横向稳定性和控制特性

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Srearman, M Leroy; Robinson, Ross B;
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年度 1956
页码 1-51
总页数 51
原文格式 PDF
正文语种 eng
中图分类工业技术;
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Static lateral stability and control characteristics of a model of a 45 degree swept-wing fighter airplane with various vertical tails at Mach numbers of 1.41, 1.61, and 2.01

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