首页> 美国政府科技报告 >Effect of yaw and angle of attack pressure recovery and mass-flow characteristics of a rectangular supersonic scoop inlet at a Mach number of 2.71

【24h】

Effect of yaw and angle of attack pressure recovery and mass-flow characteristics of a rectangular supersonic scoop inlet at a Mach number of 2.71

机译：马赫数为2.71的矩形超音速铲入口的偏航和迎角压力恢复及质量流量特性的影响

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
Comenzo, Raymond J; Mackley, Ernest A;
展开▼
作者单位

展开▼
年度 1954
页码 1-25
总页数 25
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. Effect if yaw on pressure oscillation frequency within rectangular cavity at mach 2 [J] . Pdter J.Disimile, Paul D.Orkwis AIAA Journal . 1997,第7期

机译：偏航对2马赫矩形腔内压力振荡频率的影响
2. Aerodynamic characteristics for a passenger aircraft model with harmonic oscillations on rolling and yawing angles at high angles of attack [J] . Petoshin V.I., Chasovnikov E.A. Thermophysics and Aeromechanics . 2013,第1期

机译：在高攻角下具有侧倾角和偏航角谐波振动的客机模型的气动特性
3. Aerodynamic Characteristics of a Delta Wing in the Case of Harmonic Oscillations with Respect to the Roll and Yaw Angles at High Angles of Attack [J] . E. A. Karavaev, E. A. Chasovnikov Fluid Dynamics . 2013,第2期

机译：相对于大迎角的侧倾角和横摆角，在谐波振荡情况下三角翼的空气动力学特性
4. Experimental Investigation on the Influence of Yaw Angle on the Inlet Performance at Mach 7 [C] . O. Hohn, A. GÃ AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition . 2010

机译：偏航角对7马赫进气口性能影响的实验研究
5. Study of the Effects of Geometric Parameters and Yaw Angles on Drag Generation in Clean Rectangular Cavities [D] . Shiyani, Dhaval 2018

机译：几何参数和偏航角对清洁矩形腔中阻力产生的影响的研究
6. Variations in hydrodynamic characteristics of netting panels with various twine materials knot types and weave patterns at small attack angles [O] . Hao Tang, Fuxiang Hu, Liuxiong Xu, -1

机译：在小攻角下具有多种麻线材料结类型和编织图案的网状面板的水动力特性变化
7. Two-dimensional cascade tests of MCA blades in the high transonic Mach number region. 2nd report, On the effect of stagger angle on inlet Mach number characteristics. [O] . Hajime SAKAGUCHI, Susumu TAKAMORI 1990

机译：高跨音机马赫数区域的MCA叶片的二维级联试验。第2次报告，关于入口马赫数特征的错开角度。

Effect of yaw and angle of attack pressure recovery and mass-flow characteristics of a rectangular supersonic scoop inlet at a Mach number of 2.71

摘要

著录项

引文网络

相似文献

相关主题

期刊订阅