位置：成果数据库 > 期刊 > 期刊详情页
Experimental Study of Plasma Flow Control on Highly Swept Delta Wing
  • ISSN号：0001-1452
  • 期刊名称：AIAA Journal
  • 时间：0
  • 页码：249-252
  • 语言：英文
  • 相关项目：等离子体激励控制后掠翼前缘集中涡破裂机理及应用研究
作者： Wang, G. B.|Feng, L. H.|Wang, J. J.|Zhang, P. F.|
同期刊论文项目
等离子体激励控制后掠翼前缘集中涡破裂机理及应用研究
期刊论文 14 获奖 1
同项目期刊论文
The effect of actuation frequency on the plasma synthetic jet
激励频率对等离子体合成射流的影响
非定常等离子激励器诱导平板边界层的流动结构
Flow Characteristics of Synthetic Jet Induced by Plasma Actuator
Flow structures in flat plate boundary layer induced by pulsed plasma actuator
Numerical Simulation on Plasma Circulation Control Airfoil
基于唯象模型的等离子激励诱导流场数值模拟
Numerical simulation on the flow around the dome and the mean pressure distribution
Experimental study on lift enhancement of supercritical airfoil in subsonic by Gurney flap
Aerodynamic Modification of a NACA 0012 Airfoil by Trailing-Edge Plasma Gurney Flap
超临界翼型Gurney襟翼增升技术实验研究
穹顶结构表面平均压力分布及绕流结构数值模拟
激励强度对等离子体合成射流的影响