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Longitudinal stability and control characteristics of a canard missile configuration for Mach numbers from 1.1 to 1.93 as determined from free-flight and wind-tunnel investigation

机译：自由飞行和风洞调查确定的马赫数导弹配置的纵向稳定性和控制特性为1.1至1.93马赫数

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Curfman, Howard J , Jr; Grigsby, Carl E;
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年度 1952
页码 1-31
总页数 31
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Rolling Control Characteristic Experimental Investigation of Canard Missile with Free-Spinning Tail [J] . LEI Juan-mian, WU Jia-sheng, MENG Ling-tao Journal of Beijing Institute of Technology . 2006,第1期

机译：自由旋转尾翼式导弹的滚动控制特性实验研究
2. Rolling Control Characteristic Experimental Investigation of a Canard Missile with Free-Spinning Tail [J] . 雷娟棉, 吴甲生, 孟令涛北京理工大学学报：英文版 . 2006,第001期

机译：旋转尾翼鸭式导弹的滚动控制特性实验研究
3. Numerical investigation of aerodynamic characteristics of free-spinning tail projectile with canards roll control [J] . Jiawei Zhang, Juanmian Lei, Jianping Niu Proceedings of the Institution of Mechanical Engineers . 2021,第6期

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4. Comparison Articulating Nosecones and Canards for Missile Flight Control under Mach 2 Conditions [C] . Eric Stephen, Grant Schlichting, Jarrett Van Dyke, AIAA Aviation Forum . 2020

机译：在马赫2条件下对导弹飞行控制的鼻子和迫使鼻子
5. The Analytic Solutions to the Task of Maintaining the Specified Characteristics Stability in Aircraft Flight Control System Reconfiguration [O] . Dmitry Efanov, Vladislav Kosyanchuk 2017

机译：维持飞机飞行控制系统重新配置中规定特征稳定性的任务的分析解决方案

Longitudinal stability and control characteristics of a canard missile configuration for Mach numbers from 1.1 to 1.93 as determined from free-flight and wind-tunnel investigation

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