Analytical Estimates of Peak Amplitudes of Oscillations of the Angle of Attack For an Uncontrolled Spacecraft Entering into the Atmosphere: A Case of Plane Motion

V. A. Yaroshevskii

首页> 外文期刊>Космические исследования >Analytical Estimates of Peak Amplitudes of Oscillations of the Angle of Attack For an Uncontrolled Spacecraft Entering into the Atmosphere: A Case of Plane Motion

【24h】

Analytical Estimates of Peak Amplitudes of Oscillations of the Angle of Attack For an Uncontrolled Spacecraft Entering into the Atmosphere: A Case of Plane Motion

机译：不受控制的航天器进入大气的迎角振荡峰值振幅的分析估计：平面运动的情况

获取原文

获取原文并翻译 | 示例

掌桥外文数据库（机构版） >>

开具论文收录证明 >>

文献代查 >>

页面导航

著录项
相似文献
相关主题

著录项

来源
《Космические исследования》 |2000年第4期|p.437-442|共6页
作者
V. A. Yaroshevskii;
展开▼
作者单位

展开▼
收录信息
原文格式 PDF
正文语种 rus
中图分类航天（宇宙航行）;
关键词
analytical estimation; spacecraft entering; atmosphere; plane motion;

机译：分析估计;航天器进入;大气层;平面运动;

相似文献

外文文献
中文文献
专利

1. Studying transient motion modes with respect to the landing module angle of attack with the restoring moment triharmonic characteristic on entering the atmosphere [J] . Barinova E. V., Timbai I. A. Cosmic research . 2015,第3期

机译：利用进入大气时的恢复力矩三谐波特性研究着陆模块攻角的瞬态运动模式
2. Investigation of Conditions for Plane Autorotation of a Spacecraft Entering the Atmosphere [J] . V. A. Yaroshevskii Космические исследования . 2001,第1期

机译：航天器进入大气层的平面自转条件研究
3. Experimental-Analytical Method to Construct Mathematical Models Of Uncontrolled Spacecraft Motion [J] . Yu. G. Bulychev, A.A. Manin, A.G. Zhukovskii Космические исследования . 1999,第3期

机译：建立飞机失控运动数学模型的实验分析方法
4. Influence of Effective Angle of Attack Oscillation Amplitude on Force Generation by Pitching-Plunging Flat Plates [C] . Victor Pinedo, Luis Bernal AIAA fluid dynamics conference and exhibit . 2012

机译：有效攻角振幅对俯仰平板产生力的影响
5. MEASUREMENT OF TRUE ANGLE OF ATTACK AND TRUE ANGLE OF SIDESLIP BY SENSING THE MOTIONS OF AN AIRCRAFT. [D] . SMETANA, FREDERICK OTTO. 1961

机译：通过感测飞机的运动来测量攻击的真实角度和侧滑的真实角度。
6. Posterior Tibial Slope Angle Correlates With Peak Sagittal and Frontal Plane Knee Joint Loading During Robotic Simulations of Athletic Tasks [O] . Nathaniel A. Bates, Rebecca J. Nesbitt, Jason T. Shearn, -1

机译：运动任务的机器人模拟过程中后胫骨倾斜角与矢状矢状和额面膝关节负荷相关
7. Transitional Characteristics of Vortices Issued From A Body Which Creates Asymmetric Flow Field. In A Case of Thin Symmetrical Airfoil With Angle of Attack Under Rotational Oscillation of Small Amplitude. [O] . Hiroyuki HANIU, Hiroshi SAKAMOTO, Yoshihiro OBATA, 1992

机译：从创造非对称流场发出的涡流的过渡特征。在较小振幅的旋转振荡下具有呈现角度的薄对称翼型的情况。
8. MOTIONS OF A SHORT 10 DEG BLUNTED CONE ENTERING A MARTIAN ATMOSPHERE AT ARBITRARY ANGLES OF ATTACK AND ARBITRARY PITCHING RATES [R] . Peterson, V. L. 1962

机译：短暂十分之一的锥体在任意角度攻击和任意俯仰速度下进入马尔坦大气层的运动

Analytical Estimates of Peak Amplitudes of Oscillations of the Angle of Attack For an Uncontrolled Spacecraft Entering into the Atmosphere: A Case of Plane Motion

著录项

相似文献

相关主题

期刊订阅