Turbine Aerodynamics: Axial-Flow and Radial-Inflow Turbine Design and Analysis
Table Of Contents
Preface
1.0 Introduction
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1.1 Basic Turbine Configurations
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1.2 Radial-Inflow and Axial-Flow Turbine Features
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1.3 Velocity Diagrams for a Stage
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1.4 Similitude and Performance Characteristics
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1.5 Units and Conventions
2.0 Thermodynamics
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2.1 First and Second Laws of Thermodynamics
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2.2 Efficiency
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2.3 Fluid Equation-of-State Fundamentals
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2.4 The Caloric Equation of State
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2.5 Entropy and the Speed of Sound
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2.6 The Thermal Equation of State for Real Gases
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2.7 Thermodynamic Properties of Real Gases
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2.8 Thermally and Calorically Perfect Gases
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2.9 The Pseudo-Perfect Gas Model
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2.10 Liquid-Phase Properties
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2.11 Gas Viscosity
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2.12 Component Performance Parameters
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2.13 A Computerized Equation of State Package
3.0 Fluid Mechanics
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3.1 Flow in a Rotating Coordinate System
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3.2 Adiabatic Inviscid Compressible Flow
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3.3 Adiabatic Inviscid Compressible Flow Applications
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3.4 Boundary Layer Analysis
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3.5 Two-Dimensional Boundary Layer Analysis
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3.6 Axisymmetric Three-Dimensional Boundary Layer Analysis
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3.7 Vector Operators in Natural Coordinates
4.0 Empirical Performance Models for Axial-Flow Turbine Blade Rows
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4.1 Blade Row Geometry
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4.2 Fluid Deviation Angle
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4.3 Overview of the Loss System
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4.4 Profile Loss Coefficient
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4.5 Secondary Flow Loss Coefficient
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4.6 Trailing-Edge Loss Coefficient
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4.7 Shock loss Coefficient
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4.8 Supersonic Expansion Loss Coefficient
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4.9 Blade Clearance Loss Coefficient
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4.10 Lashing Wire Loss Coefficient
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4.11 Leakage Bypass Loss
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4.12 Partial Admission Loss
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4.13 Disk Friction Loss
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4.14 Clearance Gap Windage Loss
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4.15 Moisture Loss
5.0 Aerodynamic Performance Analysis of Axial-Flow Turbines
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5.1 The Meridional Coordinate System
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5.2 The Approximate Normal Equilibrium Model
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5.3 Inviscid Adiabatic Flow on A Quasi-Normal
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5.4 Linking Quasi-Normals
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5.5 The Flow Profiles on a Quasi-Normal
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5.6 Turbine Performance Analysis
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5.7 Typical Performance Analysis Results
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5.8 Diaphragm-Disk Rotor Leakage Flows
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5.9 Blade Forces and Rotor Thrust
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5.10 Concluding Remarks
6.0 Preliminary Aerodynamic Design of Axial-Flow Turbine Stages
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6.1 Preliminary Aerodynamic Design Strategy
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6.2 Velocity Triangles at the Design Radius
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6.3 The Vortex Type and Swirl Velocity Distributions
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6.4 Stage Efficiency
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6.5 The Optimum Pitch-To-Chord Ratio
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6.6 Initializing the Total Thermodynamic Conditions
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6.7 The Stage Inlet Flow Profiles
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6.8 Sizing the Annulus
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6.9 Selecting the Blade Row Geometry
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6.10 A Computerized Preliminary Design System
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6.11 Selection of the Dimensionless Performance Parameters
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6.12 Selection of the Swirl Velocity Vortex Type
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6.13 Concluding Remarks
7.0 Detailed Airfoil Design for Axial-Flow Turbines
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7.1 Definition of the Airfoil Geometry
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7.2 The Airfoil Profile Model
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7.3 Determining the Polynomial Coefficients
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7.4 Leading and Trailing Edge Profiles
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7.5 The Passage Throat Calculation
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7.6 Adjusting the Uncovered Turning
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7.7 Design of a Complete Blade
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7.8 The Optional Defining Points
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7.9 Evaluation of the Airfoil Design
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7.10 A Computerized Airfoil Design System
8.0 Industrial Axial-Flow Turbine Application Procedures
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8.1 Stage Performance Rating Curves
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8.2 Reynolds Number Effects
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8.3 Reaction Rating Curves
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8.4 Application Procedures Based On Rating Curves
9.0 Aerodynamic Performance Analysis of Radial-Inflow Turbines
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9.1 Radial-Inflow Turbine Stage Geometry
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9.2 Boundary Layer Analysis
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9.3 The Boundary Layer Loss Coefficient
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9.4 Inlet Volute Analysis
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9.5 Nozzle Row Analysis
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9.6 Rotor Analysis
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9.7 Vaneless Annular Passage Analysis
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9.8 Exhaust Diffuser Analysis
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9.9 Imposed Total Pressure Loss
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9.10 Inlet Station Analysis
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9.11 The Performance Analysis Strategy
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9.12 Mass Balance Procedures
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9.13 Sub-Critical Performance Analysis
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9.14 Super-Critical Performance Analysis
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9.15 Typical Performance Analysis Results
10.0 Preliminary Aerodynamic Design of Radial-Inflow Turbine Stages
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10.1 Preliminary Aerodynamic Design Strategy
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10.2 Rotor Tip Sizing
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10.3 Rotor Design Specifications
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10.4 Rotor Sizing
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10.5 Evaluating the Rotor Design
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10.6 Rotor End-Wall Contours
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10.7 Straight-line Element Rotor Blade Camberlines
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10.8 Radial Element Rotor Blade Camberlines
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10.9 Nozzle Blade Geometry
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10.10 Nozzle Row Sizing
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10.11 Evaluating the Nozzle Design
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10.12 Initial Estimates of the Nozzle Design Specifications
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10.13 Volute Preliminary Design
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10.14 Exhaust Diffuser Sizing
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10.15 A Typical Preliminary Design Example
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10.16 A Computerized Preliminary Design System
11.0 Detailed Aerodynamic Design of Radial-Inflow Turbine Components
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11.1 Nozzle Blade Detailed Design
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11.2 A General Approach to Gaspath Detailed Design
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11.3 Useful Curve Forms
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11.4 Constructing the Annulus and Quasi-Normals
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11.5 Constructing the Blade Camberline
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11.6 Constructing the Blade Surfaces
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11.7 The Blade Passage Throat Geometry
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11.8 An Effective Gaspath Design System
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11.9 Application to Impeller Design
12.0 Aerodynamic Design and Performance Analysis of Exhaust Diffusers
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12.1 Basic Diffuser Technology
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12.2 An Approximate Performance Analysis
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12.3 Sizing the Exhaust Diffuser
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12.4 A Detailed Aerodynamic Performance Analysis
13.0 Two-Dimensional Analysis of the Flow in the Blade-To-Blade Plane
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13.1 The Blade-to-Blade Flow Problem
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13.2 Coordinate System and Velocity Components
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13.3 The Potential Flow Solution Procedure
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13.4 A Linearized Potential Flow Procedure
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13.5 The Time-Marching Solution Procedure
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13.6 Blade Surface Boundary Layer Analysis
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13.7 Summary
14.0 Quasi-Three-Dimensional Blade Passage Flow Field Analysis
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14.1 Quasi-Three-Dimensional Flow
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14.2 The Quasi-Normal Coordinate System
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14.3 Numerical Integration of the Governing Equations
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14.4 Repositioning the Stream Surfaces
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14.5 The Hub-To-Shroud Flow Analysis
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14.6 Coupling the Two Basic Flow Analyses
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14.7 Boundary Layer Analysis
References
About the Author
Index