首页> 美国政府科技报告 >High speed wind-tunnel investigation of the longitudinal stability and control characteristics of a 1/16-scale model of the D-558-2 research airplane at high subsonic Mach number and at a Mach number of 1.2

【24h】

High speed wind-tunnel investigation of the longitudinal stability and control characteristics of a 1/16-scale model of the D-558-2 research airplane at high subsonic Mach number and at a Mach number of 1.2

机译：高速风洞研究D-558-2研究飞机1/16比例模型在高亚音速马赫数和马赫数1.2时的纵向稳定性和控制特性

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
Osborne, Robert S;
展开▼
作者单位

展开▼
年度 1949
页码 1-87
总页数 87
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
专利

1. On the subsonic near-wake of a space launcher configuration without jet: Experimental investigation by means of particle image velocimetry (PIV) on the subsonic (Mach 0.5 to 0.9) near-wake flow of a space launcher configuration [J] . Saile Dominik, Kuhl Viktor, Gulhan Ali Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2019,第4期

机译：在没有喷射的空间发射器配置的亚音图近似：通过亚源（Mach 0.5至0.9）近唤醒空间发射器配置的粒子图像Velocimetry（PIV）的实验研究
2. Numerical investigation of high speed free shear flow instability and Mach wave radiation [J] . Alexey N. Kudryavtsev, Dmitry V. Khotyanovsky International Journal of Aeroacoustics . 2005,第3a4期

机译：高速自由剪切流不稳定性和马赫波辐射的数值研究
3. Aerodynamic Characteristics of a Swept Wing in Close Ground Proximity at High Subsonic Mach Numbers [J] . Graham Doig, Tracie J. Barber, Andrew J. Neely Journal of aerospace engineering . 2012,第4期

机译：在高亚音速马赫数下接近地面的后掠翼的气动特性
4. Low- Speed Characteristics of a High Subsonic Mach Number OHS Aircraft Configuration [C] . J. Kentfield, A. Spragins Aerospace Sciences Meeting and Exhibit . 2003

机译：亚音速马赫数高的OHS飞机配置的低速特性
5. Wind-Tunnel Measurements of the Aerodynamic Damping and Oscillatory Stability in Pitch of a Sphere at Mach Numbers from 0.20 to 4.63. [D] . Kilgore, Robert Ashworth. 1963

机译：风洞测量在0.20至4.63马赫数下球体的空气动力学阻尼和振荡稳定性。
6. Neural-Based Compensation of Nonlinearities in an Airplane Longitudinal Model with Dynamic-Inversion Control [O] . YanBin Liu, YuHui Li, FeiTeng Jin 2017

机译：具有动态反演控制的飞机纵向模型中基于神经的非线性补偿
7. 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）

High speed wind-tunnel investigation of the longitudinal stability and control characteristics of a 1/16-scale model of the D-558-2 research airplane at high subsonic Mach number and at a Mach number of 1.2

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅