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Computational Fluid Dynamics (CFD) is now an essential and effective tool used in the design of all types of turbomachine, and this topic constitutes the main theme of this book. With over 50 years of experience in the field of aerodynamics, Professor Naixing Chen has developed a wide range of numerical methods covering almost the entire spectrum of turbomachinery applications. Moreover, he has also made significant contributions to practical experiments and real-life designs. The book focuses on rigorous mathematical derivation of the equations governing flow and detailed descriptions of the…mehr
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- Produktdetails
- Verlag: John Wiley & Sons
- Seitenzahl: 480
- Erscheinungstermin: 30. September 2010
- Englisch
- ISBN-13: 9780470825013
- Artikelnr.: 37299617
- Verlag: John Wiley & Sons
- Seitenzahl: 480
- Erscheinungstermin: 30. September 2010
- Englisch
- ISBN-13: 9780470825013
- Artikelnr.: 37299617
Introduction to the Study of the Aerothermodynamics of Turbomachinery. 1.2
Brief Description of the Development of the Numerical Study of the
Aerothermodynamics of Turbomachinery. 1.3 Summary. Further Reading. 2
Governing Equations Expressed in Non-Orthogonal Curvilinear Coordinates to
Calculate 3D Viscous Fluid Flow in Turbomachinery. 2.1 Introduction. 2.2
Aerothermodynamics Governing Equations (Navier-Stokes Equations) of
Turbomachinery. 2.3 Viscous and Heat Transfer Terms of Equations. 2.4
Examples of Simplification of Viscous and Heat Transfer Terms. 2.5 Tensor
Form of Governing Equations. 2.6 Integral Form of Governing Equations. 2.7
A Collection of the Basic Relationships for Non-Orthogonal Coordinates. 2.8
Summary. 3 Introduction to Boundary Layer Theory. 3.1 Introduction. 3.2
General Concepts of the Boundary Layer. 3.2.1 Nature of Boundary Layer
Flow. 3.3 Summary. 4 Numerical Solutions of Boundary Layer Differential
Equations. 4.1 Introduction. 4.2 Boundary Layer Equations Expressed in
Partial Differential Form. 4.3 Numerical Solution of the Boundary Layer
Differential Equations for a Cascade on the Stream Surface of Revolution.
4.4 Calculation Results and Validations. 4.5 Application to Analysis of the
Performance of Turbomachinery Blade Cascades. 4.6 Summary. 5 Approximate
Calculations Using Integral Boundary Layer Equations. 5.1 Introduction. 5.2
Integral Boundary Layer Equations. 5.3 Generalized Method for Approximate
Calculation of the Boundary Layer Momentum Thickness. 5.4 Laminar Boundary
Layer Momentum Integral Equation. 5.5 Transitional Boundary Layer Momentum
Integral Equation. 5.6 Turbulent Boundary Layer Momentum Integral Equation.
5.7 Calculation of a Compressible Boundary Layer. 5.8 Summary. 6
Application of Boundary Layer Techniques to Turbomachinery. 6.1
Introduction. 6.2 Flow Rate Coefficient and Loss Coefficient of
Two-Dimensional Blade Cascades. 6.3 Studies on the Velocity Distributions
Along Blade Surfaces and Correlation Analysis of the Aerodynamic
Characteristics of Plane Blade Cascades. 6.4 Summary. 7 Stream Function
Methods for Two- and Three-Dimensional Flow Computations in Turbomachinery.
7.1 Introduction. 7.2 Three-Dimensional Flow Solution Methods with Two
Kinds of Stream Surfaces. 7.3 Two- Stream Function Method for
Three-Dimensional Flow Solution. 7.4 Stream Function Methods for
Two-Dimensional Viscous Fluid Flow Computations. 7.5 Stream Function Method
for Numerical Solution of Transonic Blade Cascade Flow on the Stream
Surface of Revolution. 7.6 Finite Analytic Numerical Solution Method (FASM)
for Solving the Stream Function Equation of Blade Cascade Flow. 7.7
Summary. Appendix 7.A Formulas for Estimating the Coefficients of the
Differential Equations of the 3D Two-Stream Function Coordinate Method. 8
Pressure Correction Method for Two-Dimensional and Three-Dimensional Flow
Computations in Turbomachinery. 8.1 Introduction. 8.2 Governing Equations
of Three-Dimensional Turbulent Flow and the Pressure Correction Solution
Method. 8.3 Two-Dimensional Turbulent Flow Calculation Examples. 8.4
Three-Dimensional Turbulent Flow Calculation Examples. 8.5 Summary. 9
Time-Marching Method for Two-Dimensional and Three-Dimensional Flow
Computations in Turbomachinery. 9.1 Introduction. 9.2 Governing Equations
of Three-Dimensional Viscous Flow in Turbomachinery. 9.3 Solution Method
Based on Multi-Stage Runge-Kutta Time-Marching Scheme. 9.4 Two-Dimensional
Turbulent Flow Examples Calculated by the Multi-Stage Runge-Kutta
Time-Marching Method. 9.5 Three-Dimensional Flow Examples Calculated by the
Multi-Stage Runge-Kutta Time-Marching Method. 9.6 Summary. 10 Numerical
Study on the Aerodynamic Design of Circumferentialand Axial-Leaned and
Bowed Turbine Blades. 10.1 Introduction. 10.2 Circumferential Blade-Bowing
Study. 10.3 Axial Blade-Bowing Study. 10.4 Circumferential Blade-Bowing
Study of Turbine Nozzle Blade Row with Low Span-Diameter Ratio. 10.5
Summary. 11 Numerical Study on Three-Dimensional Flow Aerodynamics and
Secondary Vortex Motions in Turbomachinery. 11.1 Introduction. 11.2
Post-Processing Algorithms. 11.3 Axial Turbine Secondary Vortices. 11.4
Some Features of Straight-Leaned Blade Aerodynamics of a Turbine Nozzle
with Low Span-Diameter Ratio. 11.5 Numerical Study on the Three-Dimensional
Flow Pattern and Vortex Motions in a Centrifugal Compressor Impeller. 11.6
Summary. 12 Two-Dimensional Aerodynamic Inverse Problem Solution Study in
Turbomachinery. 12.1 Introduction. 12.2 Stream Function Method. 12.3 A
Hybrid Problem Solution Method Using the Stream Function Equation with
Prescribed Target Velocity for the Blade Cascades of Revolution. 12.4
Stream-Function-Coordinate Method (SFC) for the Blade Cascades on the
Surface of Revolution. 12.5 Stream-Function-Coordinate Method (SFC) with
Target Circulation for the Blade Cascades on the Surface of Revolution.
12.6 Two-Dimensional Inverse Method Using a Direct Solver with Residual
Correction Technique. 12.7 Summary. 13 Three-Dimensional Aerodynamic
Inverse Problem Solution Study in Turbomachinery. 13.1 Introduction. 13.2
Two-Stream-Function-Coordinate-Equation Inverse Method. 13.3
Three-Dimensional Potential Function Hybrid Solution Method. 13.4 Summary.
14 Aerodynamic Design Optimization of Compressor and Turbine Blades. 14.1
Introduction. 14.2 Parameterization Method. 14.3 Response Surface Method
(RSM) for Blade Optimization. 14.4 A Study on the Effect of Maximum Camber
Location for a Transonic Fan Rotor Blading by GPAM. 14.5 Optimization of a
Low Aspect Ratio Turbine by GPAM and a Study of the Effects of Geometry on
the Aerodynamics Performance. 14.6 Blade Parameterization and Aerodynamic
Design Optimization for a 3D Transonic Compressor Rotor. 14.7 Summary.
References. Index.
Introduction to the Study of the Aerothermodynamics of Turbomachinery. 1.2
Brief Description of the Development of the Numerical Study of the
Aerothermodynamics of Turbomachinery. 1.3 Summary. Further Reading. 2
Governing Equations Expressed in Non-Orthogonal Curvilinear Coordinates to
Calculate 3D Viscous Fluid Flow in Turbomachinery. 2.1 Introduction. 2.2
Aerothermodynamics Governing Equations (Navier-Stokes Equations) of
Turbomachinery. 2.3 Viscous and Heat Transfer Terms of Equations. 2.4
Examples of Simplification of Viscous and Heat Transfer Terms. 2.5 Tensor
Form of Governing Equations. 2.6 Integral Form of Governing Equations. 2.7
A Collection of the Basic Relationships for Non-Orthogonal Coordinates. 2.8
Summary. 3 Introduction to Boundary Layer Theory. 3.1 Introduction. 3.2
General Concepts of the Boundary Layer. 3.2.1 Nature of Boundary Layer
Flow. 3.3 Summary. 4 Numerical Solutions of Boundary Layer Differential
Equations. 4.1 Introduction. 4.2 Boundary Layer Equations Expressed in
Partial Differential Form. 4.3 Numerical Solution of the Boundary Layer
Differential Equations for a Cascade on the Stream Surface of Revolution.
4.4 Calculation Results and Validations. 4.5 Application to Analysis of the
Performance of Turbomachinery Blade Cascades. 4.6 Summary. 5 Approximate
Calculations Using Integral Boundary Layer Equations. 5.1 Introduction. 5.2
Integral Boundary Layer Equations. 5.3 Generalized Method for Approximate
Calculation of the Boundary Layer Momentum Thickness. 5.4 Laminar Boundary
Layer Momentum Integral Equation. 5.5 Transitional Boundary Layer Momentum
Integral Equation. 5.6 Turbulent Boundary Layer Momentum Integral Equation.
5.7 Calculation of a Compressible Boundary Layer. 5.8 Summary. 6
Application of Boundary Layer Techniques to Turbomachinery. 6.1
Introduction. 6.2 Flow Rate Coefficient and Loss Coefficient of
Two-Dimensional Blade Cascades. 6.3 Studies on the Velocity Distributions
Along Blade Surfaces and Correlation Analysis of the Aerodynamic
Characteristics of Plane Blade Cascades. 6.4 Summary. 7 Stream Function
Methods for Two- and Three-Dimensional Flow Computations in Turbomachinery.
7.1 Introduction. 7.2 Three-Dimensional Flow Solution Methods with Two
Kinds of Stream Surfaces. 7.3 Two- Stream Function Method for
Three-Dimensional Flow Solution. 7.4 Stream Function Methods for
Two-Dimensional Viscous Fluid Flow Computations. 7.5 Stream Function Method
for Numerical Solution of Transonic Blade Cascade Flow on the Stream
Surface of Revolution. 7.6 Finite Analytic Numerical Solution Method (FASM)
for Solving the Stream Function Equation of Blade Cascade Flow. 7.7
Summary. Appendix 7.A Formulas for Estimating the Coefficients of the
Differential Equations of the 3D Two-Stream Function Coordinate Method. 8
Pressure Correction Method for Two-Dimensional and Three-Dimensional Flow
Computations in Turbomachinery. 8.1 Introduction. 8.2 Governing Equations
of Three-Dimensional Turbulent Flow and the Pressure Correction Solution
Method. 8.3 Two-Dimensional Turbulent Flow Calculation Examples. 8.4
Three-Dimensional Turbulent Flow Calculation Examples. 8.5 Summary. 9
Time-Marching Method for Two-Dimensional and Three-Dimensional Flow
Computations in Turbomachinery. 9.1 Introduction. 9.2 Governing Equations
of Three-Dimensional Viscous Flow in Turbomachinery. 9.3 Solution Method
Based on Multi-Stage Runge-Kutta Time-Marching Scheme. 9.4 Two-Dimensional
Turbulent Flow Examples Calculated by the Multi-Stage Runge-Kutta
Time-Marching Method. 9.5 Three-Dimensional Flow Examples Calculated by the
Multi-Stage Runge-Kutta Time-Marching Method. 9.6 Summary. 10 Numerical
Study on the Aerodynamic Design of Circumferentialand Axial-Leaned and
Bowed Turbine Blades. 10.1 Introduction. 10.2 Circumferential Blade-Bowing
Study. 10.3 Axial Blade-Bowing Study. 10.4 Circumferential Blade-Bowing
Study of Turbine Nozzle Blade Row with Low Span-Diameter Ratio. 10.5
Summary. 11 Numerical Study on Three-Dimensional Flow Aerodynamics and
Secondary Vortex Motions in Turbomachinery. 11.1 Introduction. 11.2
Post-Processing Algorithms. 11.3 Axial Turbine Secondary Vortices. 11.4
Some Features of Straight-Leaned Blade Aerodynamics of a Turbine Nozzle
with Low Span-Diameter Ratio. 11.5 Numerical Study on the Three-Dimensional
Flow Pattern and Vortex Motions in a Centrifugal Compressor Impeller. 11.6
Summary. 12 Two-Dimensional Aerodynamic Inverse Problem Solution Study in
Turbomachinery. 12.1 Introduction. 12.2 Stream Function Method. 12.3 A
Hybrid Problem Solution Method Using the Stream Function Equation with
Prescribed Target Velocity for the Blade Cascades of Revolution. 12.4
Stream-Function-Coordinate Method (SFC) for the Blade Cascades on the
Surface of Revolution. 12.5 Stream-Function-Coordinate Method (SFC) with
Target Circulation for the Blade Cascades on the Surface of Revolution.
12.6 Two-Dimensional Inverse Method Using a Direct Solver with Residual
Correction Technique. 12.7 Summary. 13 Three-Dimensional Aerodynamic
Inverse Problem Solution Study in Turbomachinery. 13.1 Introduction. 13.2
Two-Stream-Function-Coordinate-Equation Inverse Method. 13.3
Three-Dimensional Potential Function Hybrid Solution Method. 13.4 Summary.
14 Aerodynamic Design Optimization of Compressor and Turbine Blades. 14.1
Introduction. 14.2 Parameterization Method. 14.3 Response Surface Method
(RSM) for Blade Optimization. 14.4 A Study on the Effect of Maximum Camber
Location for a Transonic Fan Rotor Blading by GPAM. 14.5 Optimization of a
Low Aspect Ratio Turbine by GPAM and a Study of the Effects of Geometry on
the Aerodynamics Performance. 14.6 Blade Parameterization and Aerodynamic
Design Optimization for a 3D Transonic Compressor Rotor. 14.7 Summary.
References. Index.