Model Fabrication 51 Laminaturbulent boundary layer transition

CHAPTER TITLE PAGE

CHAPTER 4 4.4 Splitting the Volume 36

4.5 Edge Meshing 38 4.6 Volume meshing 39 4.7 Mesh Quality Check 39 4.7.1 Mesh quality at x-direction 40 4.7.2 Mesh quality at y-direction 41 4.7.3 Mesh quality at z-direction 41 4.7.4 Mesh quality of combination of 42 x, y and z-direction 4.8 Mesh export 42 CHAPTER 5 MODEL SETUP 43 5.1 Model Setup Step 43 5.1.1 Selecting viscous model 43 5.1.2 Determine the equation into 44 Simulation 5.1.3 Creating Material 45 5.1.4 Boundary condition setup 46 5.1.5 Iteration 49 CHAPTER 6 WIND TUNNEL TESTING 50 6.1 Introduction 50

6.2 Model Fabrication 51

6.3 Preparation process of Wind Tunnel Testing 54 6.4 Calibration 55 6.5 Wind Tunnel Testing 57 CHAPTER 7 RESULT AND DISCUSSION 58 7.1 Introduction 59 7.2 Computational Fluid Dynamics CFD 59 Result 7.2.1 Drag Force Result 62 7.3 Wind Tunnel Testing Result 64 7.3.1 Coefficient of drag calculation 65 7.4 Discussion 66 7.4.1 Comparison of Drag Force 66 7.5 Difference between result between CFD 67 and Wind Tunnel Testing CHAPTER 8 CONCLUSION 68 8.1 Conclusion 68 8.2 Recommendations 69 REFERENCES 70 BIBLIOGRAFI 72 APPENDICES 73 LIST OF TABLE NO. TITLE PAGE 1 Model data 50 2 Spring balance reading 56 3 Technical Data for UteM Wind Tunnel 57 4 Wind Tunnel Testing Data 64 LIST OF FIGURES NO. TITLE PAGE 2.1 Figure of Ahmed model 5 2.2 Boundary layer velocity gradient 10 2.3 Laminaturbulent boundary layer transition 12 Low speed

2.4 Laminaturbulent boundary layer transition

13 High speed 2.5 Flow separation and reattachment 13 2.6 Project Flow Chart 24 2.7 Rounded boundaries and rear end sector of 26 Ahmed model 2.8 Front and back body of the model with a 26 rectangular cross section 2.9 One side of half model 27 3.0 The two parts of the model will be combined at 28 the dwell, denoted in dotted lines in the center 3.1 Fused Deposition Modeling machine 31 3.2 Model tested at 0 o of angle of attack and 31 zero yaw plan view 3.3 Subsonic Wind Tunnel 32 3.4 Ahmed model in Solidworks 35 3.5 Ahmed model in GAMBIT before 36 modification 3.6 The Ahmed model is sweep from selected 36 face to form a volume 3.7 The new volume is split rom its main 36 volume 3.8 The extra volume out of the geometry is 37 deleted 3.9 New volume created from sweep the face 37 selected by reference to vertex 4.0 Complete volume of Ahmed model CFD 38 simulation 4.1 Plotting node on the edge 38 4.2 3 edges selected before meshing the volume 38 4.3 Volume meshed side view 39 4.4 Volume meshed 39 4.5 Cell aspect ratio 39 4.6 Cell skewness 39 4.7 Cell growth rate 40 4.8 Alignment to the flow 40 4.9 View of mesh quality at equiangle skew 40 5.0 View of mesh quality at aspect ratio 40 5.1 View of mesh quality at equiangle skew 41 5.2 View of mesh quality at aspect ratio 41 5.3 View of mesh quality at equiangle skew 41 5.4 View of mesh quality at aspect ratio 41 5.5 View of mesh quality at equiangle skew 42 full volume 5.6 Figure of complete mesh model 42 5.7 Viscous model screen Ahmed model 44 5.8 Energy Equation screen 45 5.9 Materials screen 45 6.0 Boundary conditions on Ahmed model CFD geometry 46 6.1 Boundary conditions screen 47 6.2 Velocity Inlet screen 47 6.3 Ahmed model 48 6.4 Iterate screen 49 6.5 CAD model drawing 51 6.6 ABS plastic 6.7 Process of making the model in rapid prototyping machine 52 6.8 Rapid prototyping machine 53 6.9 The 1:9 scale of Ahmed model 53 7.0 Side view of Ahmed model 54 7.1 Mounting is made for center of gravity position 54 7.2 Lift Calibration 55 7.3 Drag calibration 55 7.4 Drag calibration 55 7.5 Calibration Graph for Wind Tunnel Test 56 7.6 Wind Tunnel 57 7.7 Wind Tunnel Testing 58 7.8 The converged result 60 7.9 Contours of Velocity Magnitude 61 8.0 Contours of Static Pressure on Ahmed model 62 8.1 Value of Ahmed model drag at 30ms 63 8.2 Model testing figure 64 8.3 Comparison of Drag force 66 LIST OF ABBREVIATION CFD = Computational Fluid Dynamics CHAPTER 1 INTRODUCTION

1.1 Background research