首页> 美国政府科技报告 >Wind-tunnel investigation of the effects of lip geometry on drag and pressure recovery of a normal-shock nose inlet on a body of revolution at Mach numbers of 1.41 and 1.81

【24h】

Wind-tunnel investigation of the effects of lip geometry on drag and pressure recovery of a normal-shock nose inlet on a body of revolution at Mach numbers of 1.41 and 1.81

机译：风洞研究唇形几何形状对马赫数为1.41和1.81的旋转体上正常冲击鼻入口的阻力和压力恢复的影响

获取原文

页面导航

摘要
著录项
相似文献
相关主题

摘要

No Abstract Available

著录项

作者
Robins, A Warner;
展开▼
作者单位

展开▼
年度 1958
页码 1-99
总页数 99
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. Mach Number of Drag Convergence for the Riabouchinsky Nose Part of a Body of Revolution in a Near-Sonic Gas Flow [J] . V. A. Barinov, E. N. Kuznetsov, S. I. Skomorokhov, Doklady. Physics . 2005,第9期

机译：近音速气流中Riabouchinsky鼻部旋转部分的阻力收敛的马赫数
2. Drag Reduction for Spike Attached to Blunt-Nosed Body at Mach 6 [J] . R Kalimuthu, Rakhab C. Mehta, E Rathakrishnan Journal of Spacecraft and Rockets . 2010,第1期

机译：减少减震力，以使附着在马赫数为6的钝头物体上的尖刺
3. Drag Reduction for Spike Attached to Blunt-Nosed Body at Mach 6 [J] . R. Kalimuthu, R. C. Mehta, E. Rathakrishnan Journal of Spacecraft and Rockets . 2010,第1期

机译：减少减震力，以使附着在马赫数为6的钝头物体上的尖刺
4. Pressures and Drag Characteristics of Bodies of Revolution at Near Sonic Speeds Including the Effects of Viscosity and Wind Tunnel Walls [C] . B. Kulfan, J. Bussoletti, C. Hilmes AIAA Aerospace Sciences Meeting and Exhibit . 2007

机译：接近声速时旋转体的压力和阻力特性，包括粘度和风洞壁的影响
5. Experimental study on the effects of nose geometry on drag over axisymmetric bodies in supersonic flow. [D] . Brooker, B. Tyler. 2014

机译：鼻子几何形状对超声速流中轴对称物体上阻力的影响的实验研究。
6. An experimental investigation of the pressure distributions on five bodies of revolution at Mach numbers of 2.45 and 3.19 [O] . Marson G. B., Socha W., Keates R. E. 1954

机译：马赫数为2.45和3.19的五个公转体上压力分布的实验研究

Wind-tunnel investigation of the effects of lip geometry on drag and pressure recovery of a normal-shock nose inlet on a body of revolution at Mach numbers of 1.41 and 1.81

摘要

著录项

相似文献

相关主题

期刊订阅