000			02022nam a2200265 a 4500
001			vtls000052083
003			KUKTEM
005			20251114204440.0
008			110317t2010 my da f m 000 0 eng d
020			_aTHE0007228(Local)
039		9	_a201905140904 _bfawwaz _c201110041226 _dFida _c201107140039 _dVLOAD _c201103171414 _dida _y201103171248 _zida
040			_aUMP
090			_aTL245 .S53 2010 rs Bc.
100	0		_aMohd Shahmal Mohd Shahid
245	1	0	_aStudy of F1 car aerodynamics rear wing using computational fluid dynamic (CFD) / _cMohd Shahmal Mohd Shahid
246	3		_aStudy of F1 car aerodynamics rear wing using computational fluid dynamic (CFD) _h[computer file]
260			_aKuantan, Pahang : _bUMP, _c2010
300			_axvi, 59 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.
520	3		_aThis 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 consisit 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.
650		0	_aAutomobiles _xAerodynamics
650		0	_aMotor vehicles _xAerodynamics
999			_aVIRTUA40 _c2215 _d2221
999			_aVTLSSORT0080*0200*0400*0900*1000*2450*2460*2600*3000*5020*5040*5200*6500*6501*9992