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Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces

机译：具有全可动翼和尾表面的高超音速导弹配置的机械数为2.01的静态纵向稳定性和控制特性

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摘要

Static longitudinal stability and control characteristics of hypersonic missile configuration with all movable cruciform wing and tail surfaces

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作者
Foster, G. V.; Robinson, R. B.;
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年度 1961
页码 1-29
总页数 29
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
CRUCIFORM WINGS; HYPERSONIC VEHICLES; HYPERSONICS; LONGITUDINAL CONTROL; LONGITUDINAL STABILITY; MACH NUMBER; MISSILE CONFIGURATIONS; STATIC STABILITY; TAIL SURFACES; WINGS; CRUCIFORM WING; HYPERSONIC VEHICLE; LONGITUDINAL STABILITY AND CONTROL; MISSILE CONFIGURATION; STATIC STABILITY AND CONTROL;

机译：CRUCIFORm WINGs;超级摩托车;高超声速;纵向控制;纵向稳定性;马赫数;导弹配置;静态稳定性;尾部表面; WINGs; CRUCIFORm WING;超级摩托车;纵向稳定性和控制;导弹配置;静态稳定性和控制;

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专利

1. Stability Derivatives for a Slender Missile with Application to a Wing-Body-Vertical-Tail Configuration [J] . ARTHUR E. BRYSON JR. Journal of Spacecraft and Rockets . 2003,第6期

机译：细长导弹的稳定导数及其在机翼-垂直-尾翼配置中的应用
2. Effects of structural thermal boundary conditions on hypersonic aerothermoelasticity of all-movable control surface [J] . Ye Kun, Ye ZhengYin, Meng XianZong, Proceedings of the Institution of Mechanical Engineers . 2019,第7期

机译：结构性热边界条件对全动控制面高超声速气动弹性的影响
3. Effects of structural thermal boundary conditions on hypersonic aerothermoelasticity of all-movable control surface [J] . Ye Kun, Ye ZhengYin, Meng XianZong, Proceedings of the Institution of Mechanical Engineers . 2019,第7期

机译：结构热边界条件对全动控制表面高超透速空泡弹性的影响
4. A Wing-by-Wing Approach for Biplane Static Longitudinal Stability and Control Analysis [C] . Michelle Fernandino Westin, Ricardo Luiz Utsch de Freitas Pinto SAE Brasil Congress and Exhibit . 2007

机译：双翼飞机静态纵向稳定性和控制分析方法
5. Static and dynamic analysis of a typical wing section with leading edge-trailing edge control surface configuration. [D] . Platanitis, George. 2003

机译：具有前缘-后缘边缘控制面配置的典型机翼部分的静态和动态分析。
6. Aerodynamic Characteristics of a Feathered Dinosaur Measured Using Physical Models. Effects of Form on Static Stability and Control Effectiveness [O] . Dennis Evangelista, Griselda Cardona, Eric Guenther-Gleason, -1

机译：使用物理模型测量的羽毛恐龙的空气动力学特性。形式对静态稳定性和控制有效性的影响
7. Supersonic aerodynamic characteristics of a tail-control cruciform maneuverable missile with and without wings [O] . Spearman, M. L. 1983

机译：带有和不带有机翼的尾部控制十字形机动导弹的超音速气动特性

Static longitudinal stability and control characteristics at a mach number of 2.01 of a hypersonic missile configuration having all-movable wing and tail surfaces

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