Elements of Gas Turbine Propulsion
Table of Contents

• Foreword by Hans von Ohain
  
• Preface
  
• Symbols
  
• Chapter 1 - Introduction
  
• Chapter 2 - Thermodynamics Review
  
• Chapter 3 - Compressible Flow
  
• Chapter 4 - Aircraft Gas Turbine Engine
  
• Chapter 5 - Parametric Cycle Analysis of Ideal Engines
  
• Chapter 6 - Component Performance
  
• Chapter 7 - Parametric Cycle Analysis of Real Engines
  
• Chapter 8 - Engine Performance Analysis
  
• Chapter 9 - Turbomachinery
  
• Chapter 10 - Inlets, Nozzles, and Combustion Systems
  
  
• Appendixes
  
• A - U.S. Standard Atmosphere, 1976
  
• B - Gas Turbine Engine Data
  
• C - Data for Some Liquid Propellant Rocket Engines
  
• D - Air and (CH₂)_n Properties at Low Pressure
  
• E - Compressible Flow Functions (k = 1.4, 1.33, and 1.3)
  
• F - Normal Shock Functions (k = 1.4)
  
• G - Two-Dimensional Oblique Shock Functions (k = 1.4)
  
• H - Rayleigh Line Flow Functions (k = 1.4)
  
• I - Fanno Line Flow Functions (k = 1.4)
  
• J - Turbomachinery Stresses and Materials
  
• K - About the Software
  
• Reference
  
• Index