Aerothermodynamics of gas turbine and rocket propulsion

Saved in:
Bibliographic Details
Main Author Oates, Gordon C.
Format Electronic eBook
LanguageEnglish
Published Reston, VA : American Institute of Aeronautics and Astronautics, ©1997.
Edition3rd ed.
SeriesAIAA education series.
Subjects
Aerothermodynamics.
Aircraft gas-turbines.
Rocket engines.
elektronické knihy
electronic books
Online AccessFull text
ISBN9781601192226
1601192223
1563472414
9781563472411
1600860060
9781600860065
Physical Description1 online resource (xii, 456 pages) : illustrations

Cover

Table of Contents:
  • 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 Systemâ€?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

Similar Items