首页> 美国政府科技报告 >Transonic aerodynamic characteristics of a supersonic transport model with variable-sweep auxiliary wing panels, outboard tail surfaces, and a design Mach number of 2.6

【24h】

Transonic aerodynamic characteristics of a supersonic transport model with variable-sweep auxiliary wing panels, outboard tail surfaces, and a design Mach number of 2.6

机译：具有可变扫描辅助翼板，外侧尾翼和设计马赫数2.6的超音速运输模型的跨音速空气动力学特性

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
Harris, R. V.; Corlett, W. A.;
展开▼
作者单位

展开▼
年度 1965
页码 1-93
总页数 93
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
LONGITUDINAL STABILITY; SUPERSONIC COMMERCIAL AIR TRANSPORT; AERODYNAMIC CHARACTERISTICS; LIFT DRAG RATIO; SUPERSONIC FLOW; TRANSONIC FLOW;

机译：纵向稳定性;超级商业航空运输;空气动力学特征;升降比;超音速流;跨音流;

相似文献

外文文献
中文文献
专利

1. Influence of aerodynamic nonlinearity due to static panel-curvature on flutter of panels at transonic and low supersonic Mach numbers [J] . Bhatia Manav, Beran Philip Journal of Fluids and Structures . 2018,第期

机译：气体动力学非线性引起的静态面板曲率对跨音和低超声波马赫数的颤振
2. Steady/unsteady aerodynamic analysis of wings at subsonic, sonic and supersonic Mach numbers using a 3D panel method [J] . Jeonghyun Cho, Cheolheui Han, Leesang Cho, International Journal for Numerical Methods in Fluids . 2003,第10期

机译：使用3D面板方法对亚音速，声速和超音速马赫数的机翼进行稳定/不稳定的空气动力学分析
3. METHOD OF COMPUTATION OF AERODYNAMIC CHARACTERISTICS OF THE WING-TAIL CONFIGURATION IN TRANSONIC CRUISE FLIGHT [J] . L.L. Teperin, L.N. Teperina, Myo Thein TsAGI science journal . 2018,第6期

机译：跨音巡航飞行中翼尾结构的空气动力学特性计算方法
4. INFLUENCE OF AERODYNAMIC NONLINEARITY ON FLUTTER OF CURVED PANELS AT TRANSONIC AND LOW SUPERSONIC MACH NUMBERS [C] . Manav Bhatia, Philip S. Beran International Forum on Aeroelasticity and Structural Dynamics . 2018

机译：空气动力学非线性对跨音和低超音马赫数弯曲板颤动的影响
5. Aerodynamic performance of transonic and subsonic airfoils: Effects of surface roughness, turbulence intensity, Mach number, and streamline curvature-airfoil shape. [D] . Zhang, Qiang. 2005

机译：跨音速和亚音速机翼的空气动力学性能：表面粗糙度，湍流强度，马赫数和流线曲率翼型的影响。
6. Aerodynamic Characteristics of the Ventilated Design for Flapping Wing Micro Air Vehicle [O] . G. Q. Zhang, S. C. M. Yu -1

机译：拍打翼微型飞机通风设计的空气动力学特性
7. Supersonic aerodynamic characteristics of a tail-control cruciform maneuverable missile with and without wings [O] . Spearman, M. L. 1983

机译：带有和不带有机翼的尾部控制十字形机动导弹的超音速气动特性
8. Aerodynamic characteristics at mach numbers from 1.61 to 2.86 of a supersonic transport model with a blended wing-body, variable- sweep auxiliary wing panels, outboard tail surfaces, and a design mach number of 2.2 [R] . Corlett, W. A., Driver, C., Spearman, M. L. 1963

机译：具有混合翼体，可变扫掠辅助翼板，外侧尾翼和2.2的设计马赫数的超音速运输模型的马赫数为1.61至2.86的空气动力学特性

Transonic aerodynamic characteristics of a supersonic transport model with variable-sweep auxiliary wing panels, outboard tail surfaces, and a design Mach number of 2.6

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅