首页> 美国政府科技报告 >ANALYTICAL AND EXPERIMENTAL INVESTIGATION OF FLUTTER AND DIVERGENCE OF SPRING MOUNTED CONE CONFIGURATIONS AT SUPERSONIC SPEEDS

【24h】

ANALYTICAL AND EXPERIMENTAL INVESTIGATION OF FLUTTER AND DIVERGENCE OF SPRING MOUNTED CONE CONFIGURATIONS AT SUPERSONIC SPEEDS

机译：超音速下弹簧安装锥形结构的颤振和分离的分析与实验研究

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

Flutter and static divergence of spring mounted conical shell at hypersonic speeds, slender body theories applicable to unsteady conditions

著录项

作者
Hess, R. W.; Sewall, J. L.; Watkins, C. E.;
展开▼
作者单位

展开▼
年度 1962
页码 1-53
总页数 53
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AERODYNAMIC CONFIGURATIONS; CONES; CONICAL BODIES; CONICAL SHELLS; DIVERGENCE; FLUTTER; HYPERSONIC SPEED; NEWTON THEORY; SLENDER BODIES; SUPERSONIC SPEED; VON KARMAN EQUATION; YAW; CONE; FLUTTER; HYPERSONIC SPEED; SHELL; SLENDER BODY; STATIC DIVERGENCE;

机译：空气动力学配置; CONEs;圆锥体;圆锥形壳;发散;扑;超速的;牛顿理论; sLENDER BODIEs;超音速;冯卡尔曼方程;偏航;锥体;扑;超速的;贝壳; sLENDER BODY;静态差异;

相似文献

外文文献
中文文献
专利

1. Experimental investigation of the ELAC 1 configuration at supersonic speeds [J] . Krause E., Kharitonov A.M., Brodetsky M.D., Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 1999,第5期

机译：超音速下ELAC 1配置的实验研究
2. Flutter Instability Speeds of Guided Splined Disks: An Experimental and Analytical Investigation [J] . Mohammadpanah Ahmad, Hutton Stanley G. Shock and vibration . 2015,第pta1期

机译：导向花键盘颤振不稳定性的速度：实验和分析研究。
3. Flutter Instability Speeds of Guided Splined Disks: An Experimental and Analytical Investigation [J] . AhmadMohammadpanah, Stanley G.Hutton Shock and vibration . 2015,第4期

机译：导向花键盘颤振不稳定性速度的实验和分析研究
4. Experimental investigation of shock/vortex interaction for slender canard configurations at supersonic speed [C] . Leopold F., Jagusinski F., Demeautis C. Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03. 20th International Congress on . 2003

机译：超音速细长鸭嘴结构的冲击/涡流相互作用的实验研究
5. An analytical and experimental investigation of potential mechanical work extraction from supersonic jet flow on high speed mini turbines. [D] . Lee, Ken Thye. 2010

机译：高速微型涡轮机上从超音速喷射流中提取潜在机械功的分析和实验研究。
6. Experimental investigation on the characteristics of supersonic fuel spray and configurations of induced shock waves [O] . Yong Wang, Yu-song Yu, Guo-xiu Li, -1

机译：超音速燃油喷雾特性及激波配置的实验研究。
7. EXPERIMENTAL INVESTIGATION ON PERFORATED CONE-CYLINDER CONFIGURATIONS IN AXISYMMETRIC SUPERSONIC FLOW [O] . EUGEN ERBANESCU 1985

机译：轴对称超声波流动锥形圆筒配置的实验研究
8. An Experimental Investigation of the Aerodynamic Characteristics of Nose Mounted Canard Configurations at Supersonic Mach Numbers (1.5through 4.5). [R] . burt,james r. jr 1977

机译：超音速马赫数（1.5至4.5）鼻子安装鸭式结构气动特性的实验研究。

ANALYTICAL AND EXPERIMENTAL INVESTIGATION OF FLUTTER AND DIVERGENCE OF SPRING MOUNTED CONE CONFIGURATIONS AT SUPERSONIC SPEEDS

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅