中国科学院机构知识库网格系统: 检索

浏览/检索结果: 共5条，第1-5条

帮助

条数/页：排序方式：
	Alleviation of lateral spillage of two-dimensional hypersonic inlet using waverider-configuration chines 期刊论文 OAI收割 INTERNATIONAL JOURNAL OF MODERN PHYSICS B, 2020, 卷号: 34, 期号: 14-16, 页码: 5 作者: Zhai J; Zhang CA(张陈安); Wang FM(王发民); Zhang WW \| 收藏 \| 浏览/下载：36/0 \| 提交时间：2020/08/26 Hypersonic inlet lateral spillage waverider design method streamline tracing technology mass-flow ratio
	Regulation effectiveness of a window-check dam on debris flows 期刊论文 OAI收割 ENGINEERING GEOLOGY, 2019, 卷号: 253, 页码: 205-213 作者: Li, Shuai; You, Yong; Chen, Xiaoqing; Liu, Jinfeng; Chen, Jiangang \| 收藏 \| 浏览/下载：55/0 \| 提交时间：2019/06/12 Debris flow Window-check dam Sediment control Flume experiments Unit weight attenuation ratio Mass retention ratio
	Physical Modeling And Parametric Study On Two-Degree-Of-Freedom Viv Of A Cylinder Near Rigid Wall 期刊论文 OAI收割 China Ocean Engineering, 2009, 卷号: 23, 期号: 1, 页码: 119-132 作者: Yang B(杨兵); Gao FP(高福平); Li DH(李东晖); Wu YX(吴应湘); Yang B 收藏 \| 浏览/下载：1075/232 \| 提交时间：2009/08/03 Vortex-Induced Vibration Cylinder Near A Wall Two Degrees Of Freedom Steady Flow Gap-To-Diameter Ratio Mass Ratio Vortex-Induced Vibrations Very-Low Mass Plane Boundary Dynamics Currents Freedom Forces
	Investigation on a truncated streamline-traced hypersonic Busemann inlet 会议论文 OAI收割 15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference, Dayton, OH, United states, April 28, 2008 - May 1, 2008 作者: Xiao YB(肖雅彬); Yue LJ(岳连捷); Gong P; Chang XY(张新宇) 收藏 \| 浏览/下载：34/0 \| 提交时间：2017/06/01 Boundary layer corrections Busemann inlet Core flow Correction method Design points Finite differential methods Internal contraction ratio Internal flows Mass flow
	Research on three-dimensional scramiet inlet 会议论文 OAI收割 14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006 作者: Yue LJ(岳连捷); Chen LH(陈立红) 收藏 \| 浏览/下载：24/0 \| 提交时间：2017/06/01 Capture ratio Mass flow Surface oil dot visualization Three-dimensional scramjet inlet