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NACA4415翼型失速特性的二维数值研究 被引量:6
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作者 曲立群 汪建文 +2 位作者 朱德臣 吴克启 高志鹰 《内蒙古工业大学学报(自然科学版)》 2009年第1期48-51,共4页
本文利用CFD软件对NACA 4415翼型的失速特性进行二维数值研究,计算了来流攻角分别为-4度、0度、6度、14度、16度时翼型周围流场的速度分布和压力分布,并与二维P IV实验图片对比,掌握了NACA 4415翼型的失速特性,为加小翼风轮的三维动态... 本文利用CFD软件对NACA 4415翼型的失速特性进行二维数值研究,计算了来流攻角分别为-4度、0度、6度、14度、16度时翼型周围流场的速度分布和压力分布,并与二维P IV实验图片对比,掌握了NACA 4415翼型的失速特性,为加小翼风轮的三维动态数值模拟和P IV实验奠定基础和做出预测. 展开更多
关键词 naca4415 失速特性 数值研究 PIV实验
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Experimental and Numerical Investigation of the Effects of Passive Vortex Generators on Aludra UAV Performance 被引量:7
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作者 Tan Kar ZHEN Muhammed ZUBAIR Kamarul Arifin AHMAD 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2011年第5期577-583,共7页
A study of the effects of passive vortex generators (VGs) on Aludra unmanned aerial vehicle (UAV) aerodynamic characteristics is presented. Both experimental and numerical works are carried out where an array of V... A study of the effects of passive vortex generators (VGs) on Aludra unmanned aerial vehicle (UAV) aerodynamic characteristics is presented. Both experimental and numerical works are carried out where an array of VGs is attached on Aludra UAV's wing. The flow measurements are made at various angles of attack by using 3-axis component balance system. In the numerical investigation, the Reynolds-averaged Navier-Stokes (RANS) code FLUENT 6.3TM is used in the simulations with fully structured mesh with Spalart-Allmaras (S-A) turbulence model and standard wall function. The comparison between the experimental and numerical results reveals a satisfactory agreement. The parametric study shows that higher maximum lift coefficient is achieved when the VGs are placed nearer to the separation point. In addition to this, shorter spanwise distance between the VGs also increases the maximum lift coefficient, rectangular and curve-edge VG performs better than triangular VG. 展开更多
关键词 passive VG naca4415 flow control computational fluid dynamics skin friction coefficient lift coefficient
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