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翼型襟翼受力的稳定性分析
引用本文:李银然,李仁年,李德顺,袁尚科.翼型襟翼受力的稳定性分析[J].空气动力学学报,2011,29(5).
作者姓名:李银然  李仁年  李德顺  袁尚科
作者单位:兰州理工大学能源与动力工程学院甘肃省风力机工程技术研究中心,甘肃兰州,730050
基金项目:国家重点基础研究发展973计划项目(2007CB714605)
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。

关 键 词:襟翼  稳定性  升阻力  数值计算  

The stability of the force of flaps
LI Yin-ran,LI Ren-nian,LI De-shun,YUAN Shang-ke.The stability of the force of flaps[J].Acta Aerodynamica Sinica,2011,29(5).
Authors:LI Yin-ran  LI Ren-nian  LI De-shun  YUAN Shang-ke
Institution:LI Yin-ran,LI Ren-nian,LI De-shun,YUAN Shang-ke(School of Energy and Power Engineering,Lanzhou University of Technology,Gansu Provincial Technology Center for Wind Turbine,Lanzhou 730050,China)
Abstract: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 airf...
Keywords:flap  stability  lift and drag  numerical study  
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