首页> 美国政府科技报告 >Experimental investigation of the stability, control, and induced rolling moments of a canard missile airframe at a Mach number of 1.7

【24h】

Experimental investigation of the stability, control, and induced rolling moments of a canard missile airframe at a Mach number of 1.7

机译：对马赫数为1.7的鸭式导弹机体的稳定性，控制和诱导滚动力矩的实验研究

获取原文

页面导航

摘要
著录项
引文网络
相似文献
相关主题

摘要

No Abstract Available

著录项

作者
Chubb, Robert S;
展开▼
作者单位

展开▼
年度 1952
页码 1-28
总页数 28
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词

相似文献

外文文献
中文文献
专利

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. Experimental study on integrated servo control for canard-controlled missiles [J] . IEEE Transactions on Aerospace and Electronic Systems . 2016,第3期

机译：鸭式导弹综合伺服控制实验研究
4. An Improved Method to Calculate the Nonlinear Rolling Moment Due to Differential Fin Deflection of Canard Controlled Missiles [C] . F. G. Moore, L. Y. Moore, Gregory McGowan AIAA atmospheric flight mechanics conference;AIAA SciTech forum . 2015

机译：计算Canard控制导弹微分鳍挠度引起的非线性滚动力矩的一种改进方法
5. An experimental investigation on stability and transition at Mach 3. [D] . Graziosi, Paolo. 1999

机译：关于3马赫稳定和过渡的实验研究。
6. Cytoplasmic anchorage of L-selectin controls leukocyte capture and rolling by increasing the mechanical stability of the selectin tether [O] . Oren Dwir, Geoffrey S. Kansas, Ronen Alon 2001

机译：L-选择蛋白的细胞质锚定通过增加选择素系链的机械稳定性来控制白细胞的捕获和滚动
7. Analysis on Roll Damping Induced by Propulsion Jet of Rolling Airframe Missile [O] . 2004

机译：轧制机构导弹推进射流轧辊阻尼分析

Experimental investigation of the stability, control, and induced rolling moments of a canard missile airframe at a Mach number of 1.7

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅