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020 _aTHE0007230(Local)
039 9 _a201905141036
_bfawwaz
_c201110041145
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040 _aUMP
090 _aTL245 .S93 2010 rs Bc.
100 0 _aMohd Syazrul Shafiq Saad
245 1 0 _aStudy of F1 car aerodynamics front wing using computational fluid dynamics (CFD) /
_cMohd Syazrul Shafiq Saad
246 3 _aStudy of F1 car aerodynamics front wing using computational fluid dynamics (CFD)
_h[computer file]
260 _aKuantan, Pahang :
_bUMP,
_c2010
300 _axiv, 43 p. :
_bill. (some col.) ;
_c30 cm.+
_e1 computer disc
502 _aProject paper (Bachelor of Mechanical Engineering with Automotive Engineering) -- Universiti Malaysia Pahang - 2010
504 _aBibliography : p. 37
520 3 _aThe aim of this thesis is to analyze a basic front wing of a typical Formula One car using Computational Fluid Dynamics (CFD). Commercial software Gambit and Fluent was used in this CFD analysis and SolidWorks as tool for designing the front wing. The front wing is crucial in term of its influence on the handling and dynamics of the car and efficiently directing the flow to other parts of the car. Design used for the front wing is based on NACA 23012, based on research from Freddie Mehta (2006). The validation study show that CFD capable of predicting the CL with sufficient refine mesh and turbulence model assumptions. Turbulence model used in this analysis is Spalart- Allmaras turbulence model. CL value for inverted NACA 23012 is -0.24, -0.49, -0.67, and -0.80 for angle of attack 20, 40, 60, and 80 respectively. For CD is 0.06, 0.07, 0.09, and 0.12 for angle of attack 20, 40, 60, and 80 respectively. While for multiple wing CL is -1.5 and CD is 0.26. All the analysis was run around 90000 numbers of cells at interval size 5. The CL values were approximately matched with the experimental result.
650 0 _aAutomobiles
_xAerodynamics
650 0 _aComputational fluid dynamics
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