期刊文献+

后掠翼人工诱导横流驻波的升华法研究 被引量:1

Sublimation investigation of artificial abduction crossflow stationary wave in swept wing
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摘要 改进了添加粗糙带方法,使用丝网印刷方式在后掠机翼前缘添加特定间距的粗糙带。成功地在边界层内引入了特定波长的驻波,提高了人工诱导驻波波长精度。在西北工业大学低湍流度风洞中使用升华法研究了单一波长驻波的发展趋势,其扰动发展趋势与计算结果吻合得很好。 The author improved the method of appending roughness, and by silk-screen method appended the specific space roughness to the leading-edge of swept wing. This technique has been successful in introducing specific wavelength disturbance into the boundary layer, and improves the artificial abduction wavelength precision. The single disturbance evolution was investigated by using sublimation technique in the low-turbulence wind tumel of NWPU, and its evolution trend is consistent with the calculation results.
作者 李悦立 李栋 杨永 左岁寒 Li, Yue-Li[1]; Li, Dong[1]; Yang, Yong[1]; Zuo, Sui-Han[1]
出处 《实验流体力学》 EI CAS CSCD 北大核心 2009年第4期41-45,共5页 Journal of Experiments in Fluid Mechanics
关键词 粗糙带 横流驻波 人工诱导 丝网印刷 单一扰动 roughness crossflow artificial abduction silk-screen single disturbance
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参考文献9

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二级参考文献3

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共引文献18

同被引文献11

  • 1Atktin CJ,Mughal MS. Parametric studies on the application of distributed roughness elements for laminar flow control. AIAA 2005-5263, 2005.
  • 2Saric, WS, Reed HL. Toward practical laminar flow control--remaining challenges. AIAA 2004-2311, 2004.
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  • 5Cebeci Tuncer. Stability and Transition: Theory and Application. Long Beach, Calif. Horizons Publishing Inc. 2004. 85-111, 114-148.
  • 6Cebeci Tuncer. Modeling and Computation of Boundary- Layer Flows. Long Beach, Calif. Horizons Publishing Inc.2005. 262-263.
  • 7Reibert MS, Saric WS. Review of swept-wing transition. AIAA-1997-1816, 1997.
  • 8Saric WS, Carrillo RB, Reibert MS. Leading-edge roughness as a transition control mechanism. AIAA-98-0781, 1998.
  • 9Saric WS, Reed HL. Supersonic laminar flow control on swept wings using distributed roughness. AIAA 2002-0147, 2002.
  • 10Atktin C J, Sunderland R, Mughal MS. Parametric PSE studies on distributed roughness laminar flow control. AIAA 2006-3694. 2006.

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