首页> 美国政府科技报告 >On the Question of Static Longitudinal Stability of Motion for a Wing System of Finite Span Above a Solid Screen.

【24h】

On the Question of Static Longitudinal Stability of Motion for a Wing System of Finite Span Above a Solid Screen.

机译：作者：张莹莹，王汝传，王汝传，机械设计与制

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
Plisov, N. B.; Treshkov, V. K.;
展开▼
作者单位

展开▼
年度 1977
页码 1-13
总页数 13
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
Aerodynamic stability; Wings; Aerodynamic loading; Wing body configurations; Coupling(Interaction); Tail assemblies; Dihedral angle; Aerodynamic lift; Ground effect; USSR; Translations;

机译：空气动力学稳定性;翼;气动载荷;翼体结构;耦合（相互作用）;尾部组件;二面角;气动升力;地面效应;苏联;翻译;

相似文献

外文文献
中文文献
专利

1. High-resolution computational fluid dynamics predictions for the static and dynamic stall of a finite-span OA209 wing [J] . Jain Rohit, Le Pape Arnaud, Grubb Amanda, Journal of Fluids and Structures . 2018,第期

机译：有限跨度OA209翼的高分辨率计算流体动力学预测静态和动态档
2. Flow structure on finite-span wings due to pitch-up motion [J] . Yilmaz T.O., Rockwell D. Journal of Fluid Mechanics . 2012,第Null期

机译：俯仰运动在有限跨度机翼上的流动结构
3. Periodic Tail Motion Linked to Wing Motion Affects the Longitudinal Stability of Ornithopter Flight [J] . Jun-seong Lee, Joong-kwan Kim, Jae-hung Han, 仿生工程学报（英文版） . 2012,第001期

机译：与机翼运动相关的周期性尾部运动会影响飞机飞行的纵向稳定性
4. A Wing-by-Wing Approach for Biplane Static Longitudinal Stability and Control Analysis [C] . Michelle Fernandino Westin, Ricardo Luiz Utsch de Freitas Pinto SAE Brasil Congress and Exhibit . 2007

机译：双翼飞机静态纵向稳定性和控制分析方法
5. Investigation of three-dimensional flow structure on maneuvering finite-span wings [D] . Yilmaz, Turgut Oruc 2012

机译：机动有限跨机翼三维流动结构研究
6. Non-monotonic changes in critical solidification rates for stability of liquid-solid interfaces with static magnetic fields [O] . W. L. Ren, Y. F. Fan, J. W. Feng, -1

机译：关键凝固速率的非单调变化以确保具有静磁场的液固界面的稳定性
7. Estimation of the Effect of Lift-drag Ratio caused by Relaxing Longitudinal Static Stability of a certain-type of Joined-Wing Aircraft [O] . Zhen Liang, Weijun Wang 2018

机译：通过释放纵向静态稳定性引起的一定型加入翼飞机稳定性估计升降率估计
8. The effects of horizontal-tail height and a partial-span leading-edge extension on the static longitudinal stability of a wing-fuselage-tail combination having a sweptback wing [R] . Bandettini, Angelo, Selan, Ralph 1954

机译：水平尾翼高度和部分跨度前缘延伸对具有后掠翼的机翼 - 机身 - 尾翼组合的静态纵向稳定性的影响

On the Question of Static Longitudinal Stability of Motion for a Wing System of Finite Span Above a Solid Screen.

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅