首页> 美国政府科技报告 >Wind-tunnel investigation at high subsonic speeds of some effects of fuselage cross-section shape and wing height on the static longitudinal and lateral stability characteristics of a model having a 45 degree swept wing

【24h】

Wind-tunnel investigation at high subsonic speeds of some effects of fuselage cross-section shape and wing height on the static longitudinal and lateral stability characteristics of a model having a 45 degree swept wing

机译：高亚音速风洞研究机身横截面形状和机翼高度的一些影响对具有45度后掠翼的模型的静态纵向和横向稳定性特征

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
King, Thomas J , Jr;
展开▼
作者单位

展开▼
年度 1956
页码 1-63
总页数 63
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词

相似文献

外文文献
中文文献

1. Computational analysis of static height stability and aerodynamics of vehicles with a fuselage, wing and tail in ground effect [J] . Lee Juhee Ocean Engineering . 2018,第NOVa15期

机译：具有地面，机翼和机尾的车辆的静态高度稳定性和空气动力学的计算分析
2. Transonic static aeroelastic and longitudinal aerodynamic characteristics of a low-aspect-ratio swept wing [J] . Junli Wang AIP Advances . 2019,第4期

机译：低纵横比后掠翼的跨音速静态气动弹性和纵向气动特性
3. Transonic static aeroelastic and longitudinal aerodynamic characteristics of a low-aspect-ratio swept wing [J] . Junli Wang AIP Advances . 2019,第4期

机译：低纵横比后掠翼的跨音速静态气动弹性和纵向气动特性
4. Static stability of Baseline-II blended wing- body aircraft at low subsonic speed: Investigation via computational fluid dynamics simulation [C] . Nasir Rizal E. M., Kuntjoro Wahyu, Wisnoe Wirachman, 2010 International Conference on Science and Social Research . 2010

机译：低速亚音速下Baseline-II混合机翼飞机的静态稳定性：通过计算流体动力学模拟进行研究
5. Estimation of the effects of distortion on longitudinal stability of swept wing aircraft at high speeds (sub-critical mach numbers) [O] . Campion B. S. 1954

机译：估计畸变对高速后掠机翼纵向稳定性的影响（亚临界马赫数）

Wind-tunnel investigation at high subsonic speeds of some effects of fuselage cross-section shape and wing height on the static longitudinal and lateral stability characteristics of a model having a 45 degree swept wing

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅