首页> 外文OA文献 >Study of F1 car aerodynamics rear wing using computational fluid dynamic (CFD)
【2h】

Study of F1 car aerodynamics rear wing using computational fluid dynamic (CFD)

机译:使用计算流体力学(CFD)研究F1赛车的空气动力学尾翼

摘要

This thesis deals with the study on the rear wing of the F1 car. This research is about the analysis of drag coefficient, and lift coefficient, using the Ansys software. The analysis consist of two cases. First case by 2D analysis and other case by using 3D analysis. The design the rear wing of formula one car, based on the FIA 2009 regulation by using Solidwork software. NACA of NACA 2312, NACA 2308 and NACA 2104 were used. The = 1.2 × 106 and = 0.147 are use in the research. 2D result obtained from the research of the NACA 2312, NACA 2308 and NACA 2104 for the drag coefficient, are in range 0.01697 until 0.04340 and for lift coefficient, are in range -0.26427 until -0.35808. 3D result for NACA 2312, NACA 2308 and NACA 2104 on drag coefficient, are in range 0.02979 until 0.04046 and lift coefficient, in range -0.00386 until -0.00434.
机译:本文主要研究F1赛车的尾翼。这项研究是关于使用Ansys软件分析阻力系数和升力系数。分析包括两种情况。第一个案例通过2D分析,其他案例通过3D分析。根据国际汽联2009年规定,使用Solidwork软件设计一级方程式赛车的尾翼。使用了NACA 2312,NACA 2308和NACA 2104的NACA。 = 1.2×106和= 0.147用于研究。从NACA 2312,NACA 2308和NACA 2104的研究获得的2D结果,阻力系数在0.01697至0.04340范围内,升力系数在-0.26427至-0.35808范围内。 NACA 2312,NACA 2308和NACA 2104的3D阻力系数在0.02979至0.04046范围内,升力系数在-0.00386至-0.00434范围内。

著录项

  • 作者

    Mohd Shahmal Mohd Shahid;

  • 作者单位
  • 年度 2010
  • 总页数
  • 原文格式 PDF
  • 正文语种
  • 中图分类

相似文献

  • 外文文献
  • 中文文献
  • 专利

客服邮箱:kefu@zhangqiaokeyan.com

京公网安备:11010802029741号 ICP备案号:京ICP备15016152号-6 六维联合信息科技 (北京) 有限公司©版权所有
  • 客服微信

  • 服务号