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Longitudinal stability and control characteristics from a flight investigation of a cruciform canard missile configuration having an exposed wing-canard area ratio of 16:1

机译：纵向稳定性和控制特性来自飞行调查的十字形鸭翼导弹配置，暴露的机翼 - 鸭翼面积比为16：1

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Moul, Martin T; Wineman, Andrew R;
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年度 1952
页码 1-36
总页数 36
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Numerical study of leading edge separated flow over wing-canard configuration, with emphasis on aerodynamic coefficients estimation [J] . Abdulhamid Ghmmam, Zdobyslaw Goraj The Archive of Mechanical Engineering . 1998,第1期

机译：机翼-机翼构型前缘分离流的数值研究，重点是空气动力系数估计
2. 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
3. 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
4. Longitudinal Flight Stability Augmentation of a Small Blended Wing-Body Aircraft with Canard as Control Surface [C] . Rizal E. M. Nasir, Wahyu Kuntjoro International Conference on Advances in Mechanical Engineering . 2013

机译：纵向飞行稳定性，使用豆类作为控制面的小混纺机翼机架增强
5. Investigation of air-breathing, hypersonic missile configurations within external box constraints. [D] . Starkey, Ryan Peter. 2000

机译：在外箱约束下研究呼吸空气，高超音速导弹的配置。
6. Experimental investigation on the characteristics of supersonic fuel spray and configurations of induced shock waves [O] . Yong Wang, Yu-song Yu, Guo-xiu Li, -1

机译：超音速燃油喷雾特性及激波配置的实验研究。
7. A High Angle Of Attack Aerodynamic Prediction Code For Cruciform Missile Configurations.ud [O] . Venugopal S, Krishnamurthy M 1992

机译：十字形导弹配置的高攻角气动预测代码。 ud

Longitudinal stability and control characteristics from a flight investigation of a cruciform canard missile configuration having an exposed wing-canard area ratio of 16:1

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