Elements of Gas Turbine Propulsion – Jack Mattingly

Elements of Gas Turbine Propulsion – Jack Mattingly
اسم المؤلف
Jack Mattingly
التاريخ
1 أبريل 2015
المشاهدات
التقييم
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Elements of Gas Turbine Propulsion – Jack Mattingly
Table of Contents
Foreword to the First Edition ix
Preface xlix
Acknowledgments liii
Nomenclature lv
Chapter Introduction
Propulsion
Units and Dimensions
Operational Envelopes and Standard Atmosphere
Airbreathing Engines
Aircraft Performance
Rocket Engines
Problems
Chapter Review of Fundamentals
Introduction
Equations of State and Conservation of Mass
Steady Flow Energy Equation
Steady Flow Entropy Equation
Steady Flow Momentum Equation
Perfect Gas
Compressible Flow Properties
One-Dimensional Gas Dynamics Finite Control Volume
Analysis and the H-K Diagram
Nozzle Design and Nozzle Operating Characteristics
One-Dimensional Gas Dynamics Differential Control
Volume Analysis
Chemical Reactions
Problems
Chapter Rocket Propulsion
Introduction
Rocket Propulsion Requirements and Capabilities
Rocket Propulsion Engines
Types of Rocket Nozzles
Parameters for Chemical Rockets
Problems
Chapter Aircraft Gas Turbine Engine
Introduction
Thrust Equation
Note on Propulsive Efficiency
Gas Turbine Engine Components
Brayton Cycle
Aircraft Engine Design
Problems
Chapter Parametric Cycle Analysis of Ideal Engines
Introduction
Notation
Design Inputs
Steps of Engine Parametric Cycle Analysis
Assumptions of Ideal Cycle Analysis
Ideal Ramjet
Ideal Turbojet
Ideal Turbojet with Afterburner
Ideal Turbofan
Ideal Turbofan with Optimum Bypass Ratio
Ideal Turbofan with Optimum Fan Pressure Ratio
Ideal Mixed-Flow Turbofan with Afterburning
Supporting Material
Ideal Turboprop Engines Supporting Material
Ideal Turboshaft Engine with Regeneration
Supporting Material
Ideal Pulse Detonation Engine
Problems
Chapter Component Performance
Introduction
Variation in Gas Properties
Component Performance
Inlet and Diffuser Pressure Recovery
Compressor and Turbine Efficiencies
Burner Efficiency and Pressure Loss
Exhaust Nozzle Loss
Mechanical Efficiency of Power Shaft
Summary of Component Figures of Merit
(Constant cp Values)
Component Performance with Variable cp
Problems
Chapter Parametric Cycle Analysis of Real Engines
Introduction
Turbojet
Turbojet with Afterburner
Turbofan Separate Exhaust Streams
Turbofan with Afterburning Separate Exhaust Streams
Turbofan with Afterburning Mixed Exhaust
Stream Supporting Material
Turboprop Engine Supporting Material
Variable Gas Properties
Problems
Chapter Engine Performance Analysis
Introduction
Gas Generator
Turbojet Engine
Turbojet Engine with Afterburning
Turbofan Engine Separate Exhausts and
Convergent Nozzles
Turbofan with Afterburning Mixed Exhaust
Stream Supporting Material
Turboprop Engine Supporting Material
Variable Gas Properties Supporting Material
Performance Analysis Dual-Spool Afterburning
Turbojet Engine
Problems
Chapter Turbomachinery
Introduction
Euler’s Turbomachinery Equations
Axial-Flow Compressor Analysis
Centrifugal-Flow Compressor Analysis
Axial-Flow Turbine Analysis
Centrifugal-Flow Turbine Analysis
Problems
Chapter Inlets, Nozzles, and Combustion Systems
Introduction to Inlets and Nozzles
Inlets
Subsonic Inlets
Supersonic Inlets
Exhaust Nozzles
Introduction to Combustion Systems
Main Burners
Afterburners
Problems
Appendix A Altitude Tables
Appendix B Gas Turbine Engine Data
Appendix C Data for Some Liquid-Propellant Rocket Engines
Appendix D Air and (CH )n Properties at Low Pressure
Appendix E Turbomachinery Stresses and Materials
E Introduction
E Turbomachinery Stresses
E Engine Materials
Appendix F About the Software
F Getting Started
F The Software
Appendix G Answers to Selected Problems
References
Index
Supporting Materials
Library of Congress Subject Headings for this publication:
Aircraft gas-turbines
Airplanes — Jet propulsion
Jet engines
Rocket engines
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