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Aerothermodynamics of gas turbine and rocket propulsion /
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Reston, VA :
American Institute of Aeronautics and Astronautics,
©1997.
|
| Edición: | 3rd ed. |
| Colección: | AIAA education series.
|
| Temas: | |
| Acceso en línea: | Texto completo |
Tabla de Contenidos:
- Cover
- Title
- Copyright
- Foreword
- Acknowledgments
- Table of Contents
- Preface
- Chapter 1. Introduction
- 1.1 Purpose
- 1.2 Chemical Rockets
- 1.3 Nonchemical Rockets
- 1.4 Airbreathing Engines
- 1.5 Summary
- Chapter 2. Thermodynamics and Quasi-One-Dimensional Fluid Flows
- 2.1 Introduction
- 2.2 Definitions
- 2.3 The Laws of Thermodynamics
- 2.4 The Zeroth Law of Thermodynamics
- 2.5 The First Law of Thermodynamics
- 2.6 The Reversible Process
- 2.7 Derived Properties: Enthalpy and Specific Heats
- ""2.8 The Second Law of Thermodynamics""""2.9 The Gibbs Equation""; ""2.10 The Gibbs Function and the Helmholtz Function""; ""2.11 Maxwell's Relations""; ""2.12 General Relationships between Properties""; ""2.13 The Perfect Gas""; ""2.14 Quasi-One-Dimensional Fluid Flows""; ""2.15 The First Law for a Flowing System�The Control Volume""; ""2.16 The Channel Flow Equations""; ""2.17 Stagnation Properties""; ""2.18 Property Variations in Channels""; ""2.19 The Nozzle Flow Equations""; ""2.20 Numerical Solutions of Equations""; ""Problems""; ""Chapter 3. Chemical Rockets""; ""3.1 Introduction""
- 3.2 Expression for the Thrust3.3 Acceleration of a Rocket
- 3.4 Rocket Nozzle Performance
- 3.5 Elementary Chemistry
- 3.6 Determination of Chamber Conditions
- 3.7 Nozzle Flow of a Reacting Gas
- 3.8 Solid-Propellant Rockets
- Problems
- Chapter 4. Nonchemical Rockets
- 4.1 Introduction
- 4.2 The Nuclear-Heated Rocket
- 4.3 Electrically Powered Rockets
- Problems
- Chapter 5. Ideal Cycle Analysis
- 5.1 Introduction
- 5.2 Notation
- 5.3 Ideal Component Behaviors
- 5.4 The Ideal Thermodynamic Cycle
- ""5.5 The Effect of Burning at Finite Mach Number""""5.6 The Propulsive Efficiency, η[sub(p)]""; ""5.7 Systems of Units""; ""5.8 The Ideal Turbojet""; ""5.9 Interpretation of the Behavior of the Specific Fuel Consumption""; ""5.10 The Maximum Thrust Turbojet""; ""5.11 The Ideal Turbojet with Afterburning""; ""5.12 The Turbofan with Separate Exhaust Streams""; ""5.13 The Ideal Turbofan with Mixed Exhaust Streams""; ""5.14 The Ideal Constant-Pressure Mixer""; ""5.15 The Ideal Turbofan with Afterburning""; ""Problems""; ""Chapter 6. Component Performance""; ""6.1 Introduction""
- 6.2 The Thrust Equation6.3 Averages
- 6.4 The Inlet
- 6.5 The Compressor
- 6.6 The Burner
- 6.7 The Turbine
- 6.8 The Nozzle
- 6.9 Summary of Component Figures of Merit
- Problems
- Chapter 7. Nonideal Cycle Analysis
- 7.1 Introduction
- 7.2 The Turbojet
- 7.3 The Turbofan
- 7.4 The Turboprop or Prop Fan
- 7.5 The Effects of Nonconstant Specific Heats
- 7.6 Summary and Conclusions
- Problems
- Chapter 8. Engine Off-Design Performance
- 8.1 Introduction
- 8.2 Off-Design Analysis of the Turbojet