Third Edition. AIAA Education Series, American Institute of
Aeronautics and Astronautics, 1997. 459 p. ISBN:1563472414
Preface
Chapter
Introduction
Purpose
Chemical Rockets
Nonchemical Rockets
Airbreathing Engines
Summary
Fluid Flows
Thermodynamics and Quasi-One-Dimensional
Introduction
Definitions
The Laws of Thermodynamics
The Zeroth Law of Thermodynamics
The First Law of Thermodynamics
The Reversible Process
Derived Properties: Enthalpy and Specific Heats
The Second Law of Thermodynamics
The Gibbs Equation
The Gibbs Function and the Helmholtz Function
Maxwell's Relations
General Relationships between Properties
The Perfect Gas
Quasi-One-Dimensional Fluid Flows
The First Law for a Flowing System-The Control
Volume
The Channel Flow Equations
Stagnation Properties
Property Variations in Channels
The Nozzle Flow Equations
Numerical Solutions of Equations
Problems
Chemical Rockets
Introduction
Expression for the Thrust
Acceleration of a Rocket
Rocket Nozzle Performance
Elementary Chemistry
Determination of Chamber Conditions
Nozzle Flow of a Reacting Gas
Solid-Propellant Rockets
Problems
Chapter
Nonchemical Rockets
Introduction
The Nuclear-Heated Rocket
Electrically Powered Rockets
Problems
Ideal Cycle Analysis
Introduction
Notation
Ideal Component Behaviors
The Ideal Thermodynamic Cycle
The Effect of Buing at Finite Mach Number
The Propulsive Efficiency, rip
Systems of Units
The Ideal Turbojet
Interpretation of the Behavior of the Specific Fuel
Consumption
The Maximum Thrust Turbojet
The Ideal Turbojet with Afterbuing
The Turbofan with Separate Exhaust Streams
The Ideal Turbofan with Mixed Exhaust Streams
The Ideal Constant-Pressure Mixer
The Ideal Turbofan with Afterbuing
Problems
Component Performance
Introduction
The Thrust Equation
Averages
The Inlet
The Compressor
The Buer
The Turbine
The Nozzle
Summary of Component Figures of Merit
Problems
Chapter
Nonideal Cycle Analysis
Introduction
The Turbojet
The Turbofan
The Turboprop or Prop Fan
The Effects of Nonconstant Specific Heats
Summary and Conclusions
Problems
Engine Off-Design Performance
Introduction
Off-Design Analysis of the Turbojet
Off-Design Analysis of the Turbofan
Off-Design Analysis of the Turboprop
The Use of Component Characteristics
Limitations on the Accuracy of Component Characteristics
Engine Acceleration
Problems
Elementary Theory of Blade Aerodynamics
Introduction
Two-Dimensional Incompressible Flow through
Blade Rows
Free Vortex Flow
Radial Equilibrium Flows
The Effects of Compressibility
Problems
Throughflow Theory
Introduction
The Throughflow Equations
The Actuator Disk
Integral Relationships
Example Solutions
Advanced Problems in Throughflow Theory
Problems
Chapter
Cascade Flows
Introduction
Cascade Losses
Cascade Notation
Calculation Methods
Problems
Appendix A. Standard Atmosphere
Appendix B. SAE Gas Turbine Engine Notation
Appendix C. Oates Companion Software
Subject Index
Preface
Chapter
Introduction
Purpose
Chemical Rockets
Nonchemical Rockets
Airbreathing Engines
Summary
Fluid Flows
Thermodynamics and Quasi-One-Dimensional
Introduction
Definitions
The Laws of Thermodynamics
The Zeroth Law of Thermodynamics
The First Law of Thermodynamics
The Reversible Process
Derived Properties: Enthalpy and Specific Heats
The Second Law of Thermodynamics
The Gibbs Equation
The Gibbs Function and the Helmholtz Function
Maxwell's Relations
General Relationships between Properties
The Perfect Gas
Quasi-One-Dimensional Fluid Flows
The First Law for a Flowing System-The Control
Volume
The Channel Flow Equations
Stagnation Properties
Property Variations in Channels
The Nozzle Flow Equations
Numerical Solutions of Equations
Problems
Chemical Rockets
Introduction
Expression for the Thrust
Acceleration of a Rocket
Rocket Nozzle Performance
Elementary Chemistry
Determination of Chamber Conditions
Nozzle Flow of a Reacting Gas
Solid-Propellant Rockets
Problems
Chapter
Nonchemical Rockets
Introduction
The Nuclear-Heated Rocket
Electrically Powered Rockets
Problems
Ideal Cycle Analysis
Introduction
Notation
Ideal Component Behaviors
The Ideal Thermodynamic Cycle
The Effect of Buing at Finite Mach Number
The Propulsive Efficiency, rip
Systems of Units
The Ideal Turbojet
Interpretation of the Behavior of the Specific Fuel
Consumption
The Maximum Thrust Turbojet
The Ideal Turbojet with Afterbuing
The Turbofan with Separate Exhaust Streams
The Ideal Turbofan with Mixed Exhaust Streams
The Ideal Constant-Pressure Mixer
The Ideal Turbofan with Afterbuing
Problems
Component Performance
Introduction
The Thrust Equation
Averages
The Inlet
The Compressor
The Buer
The Turbine
The Nozzle
Summary of Component Figures of Merit
Problems
Chapter
Nonideal Cycle Analysis
Introduction
The Turbojet
The Turbofan
The Turboprop or Prop Fan
The Effects of Nonconstant Specific Heats
Summary and Conclusions
Problems
Engine Off-Design Performance
Introduction
Off-Design Analysis of the Turbojet
Off-Design Analysis of the Turbofan
Off-Design Analysis of the Turboprop
The Use of Component Characteristics
Limitations on the Accuracy of Component Characteristics
Engine Acceleration
Problems
Elementary Theory of Blade Aerodynamics
Introduction
Two-Dimensional Incompressible Flow through
Blade Rows
Free Vortex Flow
Radial Equilibrium Flows
The Effects of Compressibility
Problems
Throughflow Theory
Introduction
The Throughflow Equations
The Actuator Disk
Integral Relationships
Example Solutions
Advanced Problems in Throughflow Theory
Problems
Chapter
Cascade Flows
Introduction
Cascade Losses
Cascade Notation
Calculation Methods
Problems
Appendix A. Standard Atmosphere
Appendix B. SAE Gas Turbine Engine Notation
Appendix C. Oates Companion Software
Subject Index