您的位置: 专家智库 > >

国家自然科学基金(s50906100)

作品数:2 被引量:3H指数:1
发文基金:国家自然科学基金更多>>
相关领域:机械工程理学更多>>

文献类型

  • 2篇中文期刊文章

领域

  • 1篇机械工程
  • 1篇理学

主题

  • 1篇SEPARA...
  • 1篇EFFECT...
  • 1篇EXPERI...
  • 1篇CAL
  • 1篇CASCAD...
  • 1篇OPTI
  • 1篇COMPRE...
  • 1篇CORNER

传媒

  • 1篇Chines...
  • 1篇Plasma...

年份

  • 1篇2014
  • 1篇2012
2 条 记 录,以下是 1-2
排序方式:
Effects of Plasma Aerodynamic Actuation on Corner Separation in a Highly Loaded Compressor Cascade被引量:1
2014年
This paper reports experimental results on the effects of plasma aerodynamic actua- tion (PAA) on corner separation control in a highly loaded, low speed, linear compressor cascade. Total pressure loss coefficient distribution was adopted to evaluate the corner separation control effect in wind tunnel experiments. Results of pressure measurements and particle image velocime- try (PIV) show that the control effect of pitch-wise PAA on the endwall is much better than that of stream-wise PAA on the suction surface. When both the pitch-wise PAA on the endwall and stream-wise PAA on the suction surface are turned on simultaneously, the control effect is the best among all three PAA types. The mechanisms of nanosecond discharge and microsecond discharge PAA are different in corner separation control. The control effect of microsecond discharge PAA turns out better with the increase of discharge voltage and duty cycle. Compared with microsec- ond discharge PAA, nanosecond discharge PAA is more effective in preventing corner separation when the freestream velocity increases. Frequency is one of the most important parameters in plasma flow control. The optimum excitation frequency of microsecond discharge PAA is 500 Hz, which is different from the frequency corresponding to the case with a Strouhal number of unity.
王学德赵小虎李应红吴云赵勤
关键词:COMPRESSORCASCADE
Experimental investigation of nanosecond discharge plasma aerodynamic actuation被引量:2
2012年
In this paper we report on an experimental study of the characteristics of nanosecond pulsed discharge plasma aerodynamic actuation. The N2 (C3IIu) rotational and vibrational temperatures are around 430 K and 0.24 eV, respectively. The emission intensity ratio between tile first negative system and the second positive system of N2, as a rough indicator of the temporally and spatially averaged electron energy, has a minor dependence on applied voltage amplitude. The induced flow direction is not parallel, but vertical to the dielectric layer surface, as shown by measurements of body force, velocity, and vorticity. Nanosecond discharge plasma aerodynamic actuation is effective in airfoil flow separation control at freestream speeds up to 100 m/s.
吴云李应红贾敏梁华宋慧敏
共1页<1>
聚类工具0