首页> 美国政府科技报告 >A new ''free-flight'' mount system for high- speed wind-tunnel flutter models

【24h】

A new ''free-flight'' mount system for high- speed wind-tunnel flutter models

机译：用于高速风洞颤振模型的新型“自由飞行”安装系统

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
Abbott, F. T., Jr.; Reed, W. H., III;
展开▼
作者单位

展开▼
年度 1963
页码 1-37
总页数 37
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AEROELASTICITY; FLUTTER ANALYSIS; FREE FLIGHT; HIGH SPEED; SUPPORTS; WIND TUNNEL MODELS;

机译：气动弹性; FLUTTER分析;免费飞行;高速;支撑物;风洞模型;

相似文献

外文文献
中文文献
专利

1. A generalised force equivalence-based modelling method for a dry wind-tunnel flutter test system [J] . Zhang Z., Gao B., Wang J., The Aeronautical Journal . 2021,第1286期

机译：干式隧道颤动试验系统的一种广义力等效的模型方法
2. Dynamic modeling of sail mounted hydroplanes system-part II: Hydroelastic behavior and the impact of structural parameters and free-play on flutter [J] . Chen Dongyang, Abbas Laith K., Rui Xiaoting, Ocean Engineering . 2017,第FEBa1期

机译：帆式水上飞机系统的动力学建模-第二部分：水弹性行为以及结构参数和游隙对颤振的影响
3. Electromagnetic Torque-Based Model Reference Adaptive System Speed Estimator for Sensorless Surface Mount Permanent Magnet Synchronous Motor Drive [J] . Prabhakaran K. K., Karthikeyan A. IEEE Transactions on Industrial Electronics . 2020,第7期

机译：基于电磁扭矩的模型参考自适应系统速度估计，用于无传感器表面安装永磁同步电动机驱动
4. THE FLUTTER MODEL CHARACTERISTIC STUDY AND WIND-TUNNEL TEST FOR WING-MOUNTED CIVIL AIRCRAFT [C] . Chen Lei, Dou Zhongqian Congress of the International Council of the Aeronautical Sciences;International Council of the Aeronautical Sciences . 2014

机译：机翼民用飞机颤振模型特性研究及风洞试验
5. Finite element modal formulation for panel flutter at hypersonic speeds and elevated temperatures. [D] . Cheng, Guanfeng. 2002

机译：在超音速和高温下，面板颤振的有限元模态公式。
6. Enhancements to AERMOD’s Building Downwash Algorithms based on Wind-Tunnel and Embedded-LES Modeling [O] . E. M. Monbureau, D. K. Heist, S. G. Perry, -1

机译：基于风洞和嵌入式LES建模的AERMOD建筑物冲洗算法的增强
7. Flutter Characteristics of Winged Vehicle in Free-Flight/Launching Configuration and Development of Model Supporting Systems. [O] . Atsushi KANDA, Tetsuhiko UEDA 2001

机译：飞行飞行中翼车的振动特性/发射配置和模型配套系统的开发。
8. Results of initial wind-tunnel flutter experiments at low speed with a towed airplane model having a 40 degree sweptback wing of aspect ratio 3.62 equipped with pylon-mounted stores [R] . Martina, Albert P, Young, George E 1955

机译：低速初始风洞颤振试验结果，拖曳飞机模型具有纵横比为3.62的40度后掠翼，配有挂架式挂架

A new ''free-flight'' mount system for high- speed wind-tunnel flutter models

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅