Introduction Modeling Study Of A Gas Turbine Burner Cooling Ring Efficiency In A Model Combuster Exit Duct.

CONTENT CHAPTER TITLE PAGES DECLARATION ii DEDICATION iii ACKNOWLEDGEMENT iv ABSTRACT v ABSTRAK vi CONTENT vii LIST OF TABLES x LIST OF FIGURES xi LIST OF ABBREVIATIONS xiii CHAPTER I INTRODUCTION

1.1 Introduction

1 1.2 History of Gas Turbine 3

1.3 Gas Turbine Development

4 1.4 Gas Turbine Theory Operation 6

1.5 Type of Gas Turbine

8 1.6 Blade Cooling 9 1.7 Problem Statement 14 1.8 Objective 15 1.9 Scope of Study 15 CHAPTER TITLE PAGES CHAPTER II LITERATURE REVIEW 2.1 Boundary Layer 18 2.2 Turbulence Intensity 22 2.3 Reynolds’ Number 23 2.4 Conservation Law of Fluid Motion 25 2.5 Navier Stokes Equation 25 2.6 Turbulence Modeling 26 CHAPTER III METHODOLOGY 3.1 Introduction 33 3.2 Flow Chart 34 3.3 Computational Fluid Dynamics 35 3.4 Assumptions 38 3.5 2D Cooling Ring 39 3.6 Meshing Geometry 40 3.7 Iteration 41 CHAPTER IV RESULTS 4.1 Contour of Static Temperature 43 4.2 Velocity Vector 44 4.3 Static Temperature at the Bottom of Wall 45 4.4 Turbulence Intensity at the Bottom of Wall 46 4.5 Effect of Velocity Coolant Inlet, 47 Turbulence Intensity and Coolant Inlet Size 4.6 Different Coolant Inlet Velocity and 49 Turbulence Intensity 4.7 Cooling Effectiveness 50 CHAPTER TITLE PAGES CHAPTER V DISCUSSION 5.1 Effect of Coolant Inlet Velocity 54 5.2 Effect of Turbulence Intensity 54 5.3 Effect of Coolant Inlet Slot Size 54 CHAPTER VII CONCLUSION 55 REFERENCE 57 BIBLIOGRAPHY 59 APPENDIX 61 LIST OF TABLES NO. TITLE PAGES 3.4 Properties of cooling ring 39 3.6 Grid and nodes 40 3.7 Converged criterion 41 LIST OF FIGURES NO. TITLE PAGES 1.1 Cross-Sectional View of a Cooled Vane and Blade 2 Schematic of a Modern Gas Turbine Blade 3 1.2 Current gas turbine 4 1.4 Open cycle for gas turbine 7 Closed cycle for gas turbine 7 1.5 Turbine with regeneration 8 Turbine with intercooling 9 1.6 A typical turbine blade with film cooling holes 10 Cooling holes 10 3D of cooling blade flow 11 Three-dimensional 3D of cooling blade 12 Two-dimensional 2D of cooling blade 12 Convection cooling 13 Impingement cooling 13 2.1 Flow meets the leading edge 18 Layers meet at the centre 18 Velocity profile 18 2.3 Scale effect 24 3.3 CFD insight into the effect of breathing 37 Simulation of flow over male elite swimmer 37 Turbulent mixing inside a rotating impeller 38 NO. TITLE 3.5 Cooling ring 39 3.6 Meshing Geometry 40 3.7 Converged iteration 41 4.1 Contours of static temperature K 43 4.2 Vector velocity 44 4.3 Temperature of the wall 45 4.4 Turbulence Intensity of the wall 46 4.5 Wall Temperature versus Coolant Inlet Velocity 47 Wall Temperature versus Coolant Inlet Turbulence Intensity 48 Wall Temperature versus Coolant Inlet Size 49 4.6 Best static temperature contour 49 Bad static temperature contour 50 4.7 Cooling Efficiency versus Coolant Inlet Velocity 50 Cooling Efficiency versus Coolant Inlet turbulence intensity 51 Cooling Efficiency versus Coolant Inlet size 51 LIST OF ABBREVIATIONS °C = Degree Celcius 2D = Two Dimensional 3D = Three Dimensional BL = Boundary CFD = Computational Fluid Dynamics DNS = Direct Numerical Simulation FEA = Finite Element Analysis GAMBIT = Geometry and Meshing Building Intelligent Toolkit HP = Horse Power HVAC = Heating Ventilation Air Conditioning K = Kelvin k- ε = k-epsilon LES = Large-Eddy Simulation ms = Metre per second Mm = Milimetre PDE = Partial Differential Equation RANS = Reynolds Averaged Navier-Stokes RSM = Reynolds Stress Models CHAPTER 1 INTRODUCTION

1.1 Introduction