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Static lateral-directional stability characteristics of five contemporary airplane models from wind-tunnel tests at high subsonic and supersonic speeds

机译：五种现代飞机模型在高亚音速和超音速风洞试验中的静态横向稳定性特征

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Smith, Willard G; Ball, Louis H;
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年度 1956
页码 1-100
总页数 100
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Definition system and criteria related to the static stability of airplanes (first report) -definition system, static flight speed stability, and static angle of attack stability- [J] . osamu Kobayashi Transactions of the Japan society for aeronautical and space sciences . 2002,第148期

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4. Static Aeroelastic Analysis of Supersonic Experimental Airplane NEXST- 1 Flight Test [C] . H. Kawakami, T. Takatoya, H. Ishikawa AIAA Applied Aerodynamics Conference . 2007

机译：超音速实验飞机NEXST-1飞行测试的静态气动弹性分析
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7. Definition System and Criteria Related to the Static Stability of Airplanes. (First Report). Definition System, Static Flight Speed Stability, and Static Angle of Attack Stability. [O] . Osamu Kobayashi 2002

机译：定义系统和标准与飞机的静态稳定性相关。（第一个报告）。定义系统，静态飞行速度稳定性和静态攻角稳定。

Static lateral-directional stability characteristics of five contemporary airplane models from wind-tunnel tests at high subsonic and supersonic speeds

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