期刊文献+

翼型襟翼受力的稳定性分析

The stability of the force of flaps
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摘要 采用数值求解N-S方程的方法,用DES湍流模型求解襟翼高度对风力机专用翼型DU95-W-180气动性能的影响。结果表明,添加一定高度的襟翼后,翼型的受力出现波动现象,而且波动幅度随着襟翼高度的增加而增大,进一步研究引起该现象的原因发现,添加襟翼的翼型其失速旋涡的脱落过程会引起翼型周围压力的周期性变化,进而导致翼型受力出现波动现象。 DES turbulence model was used to solve the influence of flap height to the aerodynamic performance of wind dedicated DU95-W-180 airfoil by solving NS equations with numerical methods.The results showed that added a certain height of the flap,the airfoil force appears fluctuate,and the fluctuation range increased with the hight of the flap.The further studies to the reasons causing the phenomenon found that add the flaps,its stall vortex shedding process can cause cyclical changes in pressure around the airfoil,which led to the phenomenon of airfoil force fluctuations.
出处 《空气动力学学报》 EI CSCD 北大核心 2011年第5期664-668,共5页 Acta Aerodynamica Sinica
基金 国家重点基础研究发展973计划项目(2007CB714605)
关键词 襟翼 稳定性 升阻力 数值计算 flap stability lift and drag numerical study
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  • 1包能胜,霍福鹏,叶枝全,倪维斗.表面粗糙度对风力机翼型性能的影响[J].太阳能学报,2005,26(4):458-462. 被引量:37
  • 2申振华,于国亮.翼型弯度对风力机性能的影响[J].动力工程,2007,27(1):136-139. 被引量:22
  • 3夏商周,申振华.改型尾缘对翼型流场影响的数值模拟[J].沈阳航空工业学院学报,2005,22(5):1-3. 被引量:10
  • 4上官云信,周瑞兴,高永卫,肖春生,郗忠祥.翼型相对厚度对失速分离特性的影响[J].空气动力学学报,2000,18(z1):21-26. 被引量:10
  • 5LIEBECK R H. Design of subsonic airfoil for high lift[J]. Journal of Aircraft, 1978,15 ( 9 ) :547-561.
  • 6KENTFIED J A C, CLAELLE E J. The flow physics of the Gurney flaps devices for improving turbine blade performance [J]. Wing Engineering, 1993,19( 1 ) :24-34.
  • 7JANG C S, ROSS J C, CUMMINGS R M. Numerical investi- gation of an airfoil with a Gumey flap [ J ]. Aircraft Design, 1998,1 (2) :75-88.
  • 8JANG C S, ROSS J C, CUMMINGS R M. Numerical investi- gation of an airfoil with a Gumey flap[J]. Aircraft Design, 1998, ( 1 ) :75-88.
  • 9STEFAN S, FRANK T. Detached eddy simulation of flow around a airfoil [J]. Flow, Turbulence and Combustion, 2003, 71 (1-4) :261-278.
  • 10STRELETS M. Detached eddy simulation of massively separated flows[ R] . AIAA-2001- 0879, 2001.

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