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Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a Mach number of 2.01

机译：一系列具有鸭式控制器的十字形翼导弹俯仰的空气动力学特性，马赫数为2.01

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Spearman, M Leroy;
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年度 1953
页码 1-42
总页数 42
原文格式 PDF
正文语种 eng
中图分类工业技术;
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1. Aerodynamic Shape Optimization System of a Canard-Controlled Missile Using Trajectory-Dependent Aerodynamic Coefficients [J] . Young Rok Yang, Sung Ki Jung, Tae Hwan Cho, Journal of Spacecraft and Rockets . 2012,第2期

机译：弹道相关气动系数的鸭嘴控制型导弹气动形状优化系统
2. Numerical and Experimental Determination of Canard Controlled Missile Aerodynamic Coefficients in Subsonic Regime [J] . Al Kaabi Hamad, Petrovi? Zlatko, Djukanovi? Gordana Technical Gazette . 2019,第3期

机译：亚音区中Canard控制导弹空气动力学系数的数值和实验测定
3. Aerodynamic performance improvement of a canard control missile [J] . Tahani M., Masdari M., Kazemi M. Aircraft engineering . 2017,第6期

机译：鸭式控制导弹的气动性能改进
4. Analysis of aerodynamic characteristics of a modular assembled missile with canard rudder and arc tail [C] . Han Chen, Kewei Li, Chao Wang, International Conference on Modelling, Identification and Control . 2017

机译：带有鸭舵和弧尾的模块化组合导弹的气动特性分析
5. Wind-Tunnel Measurements of the Aerodynamic Damping and Oscillatory Stability in Pitch of a Sphere at Mach Numbers from 0.20 to 4.63. [D] . Kilgore, Robert Ashworth. 1963

机译：风洞测量在0.20至4.63马赫数下球体的空气动力学阻尼和振荡稳定性。
6. Analyses of aerodynamic characteristics of the oropharynx applying CBCT: obstructive sleep apnea patients versus control subjects [O] . Hui Chen, Yingguang Li, Johan HC Reiber, 2018

机译：应用CBCT分析口咽的空气动力学特征：阻塞性睡眠呼吸暂停患者与对照组
7. Numerical and Experimental Determination of Canard Controlled Missile Aerodynamic Coefficients in Subsonic Regime [O] . 2019

机译：亚音区政治中Canard控制导弹气动系数的数值和实验测定

Aerodynamic characteristics in pitch of a series of cruciform-wing missiles with canard controls at a Mach number of 2.01

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