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Aerothermodynamics of turbomachinery [[electronic resource] ] : analysis and design / / Naixing Chen
| Aerothermodynamics of turbomachinery [[electronic resource] ] : analysis and design / / Naixing Chen |
| Autore | Chen Naixing <1933-> |
| Pubbl/distr/stampa | Singapore ; ; Hoboken, NJ, : John Wiley & Sons, c2010 |
| Descrizione fisica | 1 online resource (475 p.) |
| Disciplina | 621.406 |
| Soggetto topico |
Turbomachines - Aerodynamics
Turbomachines - Design and construction |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-299-18952-0
0-470-82501-4 0-470-82502-2 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
AEROTHERMODYNAMICS OF TURBOMACHINERY: ANALYSIS AND DESIGN; Contents; Foreword; Preface; Acknowledgments; Nomenclature; 1 Introduction; 1.1 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 Equations2.3.1 Viscous Stress Tensor; 2.3.2 Strain Tensor; 2.3.3 Viscous Force; 2.3.4 Rates of Work Done by the Viscous Stresses and Dissipation Function; 2.3.5 Heat Transfer Term; 2.4 Examples of Simplification of Viscous and Heat Transfer Terms; 2.4.1 Three-Dimensional Flow in Turbomachinery Expressed by Using Arbitrary Non-Orthogonal Coordinates; 2.4.2 S1 Stream-Surface Flow; 2.4.3 S2 Stream-Surface Flow; 2.4.4 Annulus Wall Boundary Layer; 2.4.5 Three-Dimensional Boundary Layer on Rotating Blade Surface; 2.5 Tensor Form of Governing Equations 2.5.1 Continuity Equation2.5.2 Momentum Equation; 2.5.3 Energy Equation; 2.5.4 Entropy Equation; 2.6 Integral Form of Governing Equations; 2.6.1 Continuity Equation; 2.6.2 Momentum Equation; 2.6.3 Energy Equation; 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; 3.2.2 Boundary Layer Thicknesses; 3.2.3 Transition of the Boundary Layer Regime; 3.2.4 Boundary Layer Separation; 3.2.5 Thermal Boundary Layer; 3.3 Summary 4 Numerical Solutions of Boundary Layer Differential Equations4.1 Introduction; 4.2 Boundary Layer Equations Expressed in Partial Differential Form; 4.2.1 Two-Dimensional Laminar Boundary Layer Equations; 4.2.2 Laminar Boundary Layer Equations of Axisymmetrical Flow; 4.2.3 Turbulent Boundary Layer Equations; 4.2.4 Boundary Conditions of Solution; 4.3 Numerical Solution of the Boundary Layer Differential Equations for a Cascade on the Stream Surface of Revolution; 4.3.1 Boundary Layer Equations of S1 Stream Surface Flow of Revolution and Their Solution; 4.3.2 Turbulence Modeling 4.4 Calculation Results and Validations4.4.1 Laminar Boundary Layer Calculation Example; 4.4.2 Turbulent Boundary Layer with Favorable Pressure Gradient; 4.4.3 Turbulent Boundary Layer with Adverse Pressure Gradient (Ludweig and Tillmann); 4.4.4 Turbulent Boundary Layer with Favorable Pressure Gradient (Bell); 4.4.5 Turbulent Boundary Layer with Adverse Pressure Gradient (Schubauer and Spangenberg); 4.5 Application to Analysis of the Performance of Turbomachinery Blade Cascades; 4.5.1 Boundary Layer Momentum Thickness (Bammert's Experiment) 4.5.2 Laminar Boundary Layer Prediction (Turbine and Compressor Blade Profiles) |
| Record Nr. | UNINA-9910133597603321 |
Chen Naixing <1933->
|
||
| Singapore ; ; Hoboken, NJ, : John Wiley & Sons, c2010 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerothermodynamics of turbomachinery [[electronic resource] ] : analysis and design / / Naixing Chen
| Aerothermodynamics of turbomachinery [[electronic resource] ] : analysis and design / / Naixing Chen |
| Autore | Chen Naixing <1933-> |
| Pubbl/distr/stampa | Singapore ; ; Hoboken, NJ, : John Wiley & Sons, c2010 |
| Descrizione fisica | 1 online resource (475 p.) |
| Disciplina | 621.406 |
| Soggetto topico |
Turbomachines - Aerodynamics
Turbomachines - Design and construction |
| ISBN |
1-299-18952-0
0-470-82501-4 0-470-82502-2 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
AEROTHERMODYNAMICS OF TURBOMACHINERY: ANALYSIS AND DESIGN; Contents; Foreword; Preface; Acknowledgments; Nomenclature; 1 Introduction; 1.1 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 Equations2.3.1 Viscous Stress Tensor; 2.3.2 Strain Tensor; 2.3.3 Viscous Force; 2.3.4 Rates of Work Done by the Viscous Stresses and Dissipation Function; 2.3.5 Heat Transfer Term; 2.4 Examples of Simplification of Viscous and Heat Transfer Terms; 2.4.1 Three-Dimensional Flow in Turbomachinery Expressed by Using Arbitrary Non-Orthogonal Coordinates; 2.4.2 S1 Stream-Surface Flow; 2.4.3 S2 Stream-Surface Flow; 2.4.4 Annulus Wall Boundary Layer; 2.4.5 Three-Dimensional Boundary Layer on Rotating Blade Surface; 2.5 Tensor Form of Governing Equations 2.5.1 Continuity Equation2.5.2 Momentum Equation; 2.5.3 Energy Equation; 2.5.4 Entropy Equation; 2.6 Integral Form of Governing Equations; 2.6.1 Continuity Equation; 2.6.2 Momentum Equation; 2.6.3 Energy Equation; 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; 3.2.2 Boundary Layer Thicknesses; 3.2.3 Transition of the Boundary Layer Regime; 3.2.4 Boundary Layer Separation; 3.2.5 Thermal Boundary Layer; 3.3 Summary 4 Numerical Solutions of Boundary Layer Differential Equations4.1 Introduction; 4.2 Boundary Layer Equations Expressed in Partial Differential Form; 4.2.1 Two-Dimensional Laminar Boundary Layer Equations; 4.2.2 Laminar Boundary Layer Equations of Axisymmetrical Flow; 4.2.3 Turbulent Boundary Layer Equations; 4.2.4 Boundary Conditions of Solution; 4.3 Numerical Solution of the Boundary Layer Differential Equations for a Cascade on the Stream Surface of Revolution; 4.3.1 Boundary Layer Equations of S1 Stream Surface Flow of Revolution and Their Solution; 4.3.2 Turbulence Modeling 4.4 Calculation Results and Validations4.4.1 Laminar Boundary Layer Calculation Example; 4.4.2 Turbulent Boundary Layer with Favorable Pressure Gradient; 4.4.3 Turbulent Boundary Layer with Adverse Pressure Gradient (Ludweig and Tillmann); 4.4.4 Turbulent Boundary Layer with Favorable Pressure Gradient (Bell); 4.4.5 Turbulent Boundary Layer with Adverse Pressure Gradient (Schubauer and Spangenberg); 4.5 Application to Analysis of the Performance of Turbomachinery Blade Cascades; 4.5.1 Boundary Layer Momentum Thickness (Bammert's Experiment) 4.5.2 Laminar Boundary Layer Prediction (Turbine and Compressor Blade Profiles) |
| Record Nr. | UNINA-9910829948503321 |
|
Chen Naixing <1933->
|
||
| Singapore ; ; Hoboken, NJ, : John Wiley & Sons, c2010 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerothermodynamics of turbomachinery : analysis and design / / Naixing Chen
| Aerothermodynamics of turbomachinery : analysis and design / / Naixing Chen |
| Autore | Chen Naixing <1933-> |
| Pubbl/distr/stampa | Singapore ; ; Hoboken, NJ, : John Wiley & Sons, c2010 |
| Descrizione fisica | 1 online resource (475 p.) |
| Disciplina | 621.406 |
| Soggetto topico |
Turbomachines - Aerodynamics
Turbomachines - Design and construction |
| ISBN |
1-299-18952-0
0-470-82501-4 0-470-82502-2 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
AEROTHERMODYNAMICS OF TURBOMACHINERY: ANALYSIS AND DESIGN; Contents; Foreword; Preface; Acknowledgments; Nomenclature; 1 Introduction; 1.1 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 Equations2.3.1 Viscous Stress Tensor; 2.3.2 Strain Tensor; 2.3.3 Viscous Force; 2.3.4 Rates of Work Done by the Viscous Stresses and Dissipation Function; 2.3.5 Heat Transfer Term; 2.4 Examples of Simplification of Viscous and Heat Transfer Terms; 2.4.1 Three-Dimensional Flow in Turbomachinery Expressed by Using Arbitrary Non-Orthogonal Coordinates; 2.4.2 S1 Stream-Surface Flow; 2.4.3 S2 Stream-Surface Flow; 2.4.4 Annulus Wall Boundary Layer; 2.4.5 Three-Dimensional Boundary Layer on Rotating Blade Surface; 2.5 Tensor Form of Governing Equations 2.5.1 Continuity Equation2.5.2 Momentum Equation; 2.5.3 Energy Equation; 2.5.4 Entropy Equation; 2.6 Integral Form of Governing Equations; 2.6.1 Continuity Equation; 2.6.2 Momentum Equation; 2.6.3 Energy Equation; 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; 3.2.2 Boundary Layer Thicknesses; 3.2.3 Transition of the Boundary Layer Regime; 3.2.4 Boundary Layer Separation; 3.2.5 Thermal Boundary Layer; 3.3 Summary 4 Numerical Solutions of Boundary Layer Differential Equations4.1 Introduction; 4.2 Boundary Layer Equations Expressed in Partial Differential Form; 4.2.1 Two-Dimensional Laminar Boundary Layer Equations; 4.2.2 Laminar Boundary Layer Equations of Axisymmetrical Flow; 4.2.3 Turbulent Boundary Layer Equations; 4.2.4 Boundary Conditions of Solution; 4.3 Numerical Solution of the Boundary Layer Differential Equations for a Cascade on the Stream Surface of Revolution; 4.3.1 Boundary Layer Equations of S1 Stream Surface Flow of Revolution and Their Solution; 4.3.2 Turbulence Modeling 4.4 Calculation Results and Validations4.4.1 Laminar Boundary Layer Calculation Example; 4.4.2 Turbulent Boundary Layer with Favorable Pressure Gradient; 4.4.3 Turbulent Boundary Layer with Adverse Pressure Gradient (Ludweig and Tillmann); 4.4.4 Turbulent Boundary Layer with Favorable Pressure Gradient (Bell); 4.4.5 Turbulent Boundary Layer with Adverse Pressure Gradient (Schubauer and Spangenberg); 4.5 Application to Analysis of the Performance of Turbomachinery Blade Cascades; 4.5.1 Boundary Layer Momentum Thickness (Bammert's Experiment) 4.5.2 Laminar Boundary Layer Prediction (Turbine and Compressor Blade Profiles) |
| Record Nr. | UNINA-9910876596703321 |
|
Chen Naixing <1933->
|
||
| Singapore ; ; Hoboken, NJ, : John Wiley & Sons, c2010 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||