Inductive Reactance of a Rigid Wing at Harmonic Linear Oscillations and Angle of Attack

E. V. Romanenko; S. G. Pushkov; V. N. Lopatin

首页> 外文期刊>Biology Bulletin Reviews >Inductive Reactance of a Rigid Wing at Harmonic Linear Oscillations and Angle of Attack

【24h】

Inductive Reactance of a Rigid Wing at Harmonic Linear Oscillations and Angle of Attack

机译：刚性机翼在谐波线性振荡和迎角下的感应电抗

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

摘要
著录项
相似文献
相关主题

摘要

The inductive reactance of a flat and rigid wing performing harmonic oscillations with a sufficiently large amplitude at an arbitrary position of the axis of rotation was estimated. In the plane problem, analytical expressions for the components of inductive reactance through the coefficients of hydrodynamic derivatives for harmonic variations in the angle of attack were obtained.

机译：估计了平坦且刚性的机翼在旋转轴的任意位置以足够大的幅度执行谐波振荡的感应电抗。在平面问题中，通过针对迎角谐波变化的流体力学导数系数，获得了感抗成分的解析表达式。

著录项

来源
《Biology Bulletin Reviews》 |2013年第2期|共10页
作者
E. V. Romanenko; S. G. Pushkov; V. N. Lopatin;
展开▼
作者单位

展开▼
收录信息
原文格式 PDF
正文语种 eng
中图分类生物科学;
关键词
inductive reactance; propulsive coefficient; power factor; rigid wing; modeling;

机译：感应电抗推进系数功率因数刚性机翼造型;

相似文献

外文文献
中文文献
专利

1. Inductive Reactance of a Rigid Wing at Harmonic Linear Oscillations and Angle of Attack [J] . E. V. Romanenko, S. G. Pushkov, V. N. Lopatin Biology Bulletin Reviews . 2013,第2期

机译：刚性机翼在谐波线性振荡和迎角下的感应电抗
2. Aerodynamic characteristics for a passenger aircraft model with harmonic oscillations on rolling and yawing angles at high angles of attack [J] . Petoshin V.I., Chasovnikov E.A. Thermophysics and Aeromechanics . 2013,第1期

机译：在高攻角下具有侧倾角和偏航角谐波振动的客机模型的气动特性
3. Aerodynamic characteristics of passenger and transport aircraft models at harmonic oscillations on the pitch angle for high angles of attack [J] . V.I. Petoshin, E.A. Chasovnikov Thermophysics and Aeromechanics . 2011,第3期

机译：客机和运输机模型在高迎角俯仰角上的谐波振荡下的气动特性
4. A CHARACTERIZATION OF LIMIT CYCLE OSCILLATIONS IN MEMBRANE WING MICRO AIR VEHICLES AT LOW ANGLE OF ATTACK [C] . Peter J. Attar, Jordan W. Johnston, William A. Romberg, ASME Joint US-European Fluids Engineering Division summer meeting;FEDSM2010 . 2011

机译：低攻角下机翼微空中飞行器极限循环振动的表征
5. Trim angle of attack of flexible wings using non-linear aerodynamics. [D] . Cohen, David Erik. 1998

机译：使用非线性空气动力学来修剪柔性机翼的迎角。
6. Nonlinearity Analysis and Parameters Optimization for an Inductive Angle Sensor [O] . Lin Ye, Ming Yang, Liang Xu, 2014

机译：感应角传感器的非线性分析和参数优化
7. Wing rock as a lateral-directional aircraft limit cycle oscillations induced by nonlinear aerodynamics occurring at high angle of attack [O] . Young Paul David 1977

机译：作为横向飞机的机翼岩石限制了在高迎角下发生的非线性空气动力学引起的循环振荡

Inductive Reactance of a Rigid Wing at Harmonic Linear Oscillations and Angle of Attack

摘要

著录项

相似文献

相关主题

期刊订阅