## PDF Free Download | Gas Turbines: Internal Flow Systems Modeling by Bijay Sultanian

**1 Overview of Gas Turbines for Propulsion and Power Generation**1.0 Introduction

1.1 Primary Flow: Energy Conversion

1.2 Internal Flow System (IFS)

1.3 Physics-Based Modeling

1.4 Robust Design Methodology

1.5 Concluding Remarks

Worked Examples

Problems

References

Bibliography

Nomenclature

**2 Review of Thermodynamics, Fluid Mechanics, and Heat Transfer**

2.0 Introduction

2.1 Thermodynamics

2.2 Fluid Mechanics

2.3 Internal Flow

2.4 Heat Transfer

2.5 Concluding Remarks

Worked Examples

Problems

References

Bibliography

Nomenclature

3

**1-D Flow and Network Modeling**

3.0 Introduction

3.1 1-D Flow Modeling of Components

3.2 Description of a Flow Network: Elements and Junctions

3.3 Compressible Flow Network Solution

3.4 Concluding Remarks

Worked Examples

Problems

Project

References

Bibliography

Nomenclature

**4 Internal Flow around Rotors and Stators**

4.0 Introduction

4.1 Rotor Disk

4.2 Cavity

4.3 Windage and Swirl Modeling in a General Cavity

4.4 Compressor Rotor Cavity

4.5 Preswirl System

4.6 Hot Gas Ingestion: Ingress and Egress

4.7 Axial Rotor Thrust

4.8 Concluding Remarks

Worked Examples

Problems

Projects

References

Bibliography

Nomenclature

**5 Labyrinth Seals**

5.0 Introduction

5.1 Straight-Through and Stepped-Tooth Designs

5.2 Tooth-by-Tooth Modeling

5.3 Concluding Remarks

Worked Examples

Project

References

Bibliography

Nomenclature

**6 Whole Engine Modeling**

6.0 Introduction

6.1 Multiphysics Modeling of Engine Transients

6.2 Nonlinear Convection Links

6.3 Role of Computational Fluid Dynamics (CFD)

6.4 CFD Methodology

6.5 Thermomechanical Analysis

6.6 Validation with Engine Test Data

6.7 Concluding Remarks

Project

References

Bibliography

Nomenclature

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The book employs physics-based, design-oriented methodology to compute windage and swirl distributions in a complex rotor cavity formed by surfaces with arbitrary rotation, counter-rotation, and no rotation. This text will be a valuable tool for aircraft engine and industrial gas turbine design engineers as well as graduate students enrolled in advanced special topics courses.

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