[request_ebook] Elements of Propulsion: Gas Turbines and Rockets
Author: Jack D. Mattingly
Date: 2006
ISBN: 1-56347-779-3
Pages: 867
Language: English
Publisher: AIAA
Category: Technical
Tag: Science/Engineering
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Description
- Author: Jack D. Mattingly
- Publisher: AIAA
- Publish Date: 2006
- Pages: 867
![Book Cover: [request_ebook] Elements of Propulsion: Gas Turbines and Rockets](http://www.nbcindia.com/Booksimages/1563477793.gif)
NOTE: This is an updated version of the book and contains additional support material for chapters 5, 7 & 8 which is different (more inclusive) than other versions found online so far.
Table of Contents
Foreword to the Second Edition.............................................................ix
Foreword to the First Edition.................................................................xv
Preface....................................................................................................li
Acknowledgments...................................................................................lv
Nomenclature........................................................................................lvii
Chapter 1. Introduction........................................................................1
1.1 Propulsion............................................................................1
1.2 Units and Dimensions..........................................................2
1.3 Operational Envelopes and Standard Atmosphere..............4
1.4 Airbreathing Engines...........................................................5
1.5 Aircraft Performance..........................................................29
1.6 Rocket Engines..................................................................49
Problems............................................................................56
Chapter 2. Review of Fundamentals.................................................65
2.1 Introduction.......................................................................65
2.2 Equations of State and Conservation of Mass...................65
2.3 Steady Flow Energy Equation............................................68
2.4 Steady Flow Entropy Equation...........................................75
2.5 Steady Flow Momentum Equation......................................76
2.6 Perfect Gas........................................................................82
2.7 Compressible Flow Properties............................................93
2.8 One-Dimensional Gas Dynamics—Finite Control Volume
Analysis and the H-K Diagram..........................................107
2.9 Nozzle Design and Nozzle Operating Characteristics.......121
2.10 One-Dimensional Gas Dynamics—Differential Control
Volume Analysis...............................................................134
2.11 Chemical Reactions..........................................................139
Problems..........................................................................147
Chapter 3. Rocket Propulsion...........................................................161
3.1 Introduction.....................................................................161
3.2 Rocket Propulsion Requirements and Capabilities............166
3.3 Rocket Propulsion Engines...............................................176
3.4 Types of Rocket Nozzles...................................................189
3.5 Parameters for Chemical Rockets.....................................194
Problems..........................................................................228
Chapter 4. Aircraft Gas Turbine Engine...........................................233
4.1 Introduction......................................................................233
4.2 Thrust Equation................................................................233
4.3 Note on Propulsive Efficiency............................................243
4.4 Gas Turbine Engine Components......................................244
4.5 Brayton Cycle....................................................................252
4.6 Aircraft Engine Design.......................................................257
Problems...........................................................................258
Chapter 5. Parametric Cycle Analysis of Ideal Engines...................261
5.1 Introduction......................................................................261
5.2 Notation............................................................................262
5.3 Design Inputs...................................................................264
5.4 Steps of Engine Parametric Cycle Analysis........................264
5.5 Assumptions of Ideal Cycle Analysis.................................266
5.6 Ideal Ramjet.....................................................................266
5.7 Ideal Turbojet...................................................................278
5.8 Ideal Turbojet with Afterburner........................................291
5.9 Ideal Turbofan..................................................................302
5.10 Ideal Turbofan with Optimum Bypass Ratio......................325
5.11 Ideal Turbofan with Optimum Fan Pressure Ratio.............332
5.12 Ideal Pulse Detonation Engine..........................................341
Problems...........................................................................344
Chapter 6. Component Performance.................................................355
6.1 Introduction.......................................................................355
6.2 Variation in Gas Properties................................................355
6.3 Component Performance....................................................357
6.4 Inlet and Diflfuser Pressure Recovery................................358
6.5 Compressor and Turbine Efficiencies.................................360
6.6 Burner Efficiency and Pressure Loss..................................370
6.7 Exhaust Nozzle Loss..........................................................371
6.8 Mechanical Efficiency of Power Shaft..................................371
6.9 Summary of Component Figures of Merit
(Constant cp Values)......................................................371
6.10 Component Performance with Variable cp.........................373
Problems............................................................................378
Chapter 7. Parametric Cycle Analysis of Real Engines......................381
7.1 Introduction........................................................................381
7.2 Turbojet..............................................................................381
7.3 Turbojet with Afterburner...................................................399
7.4 Turbofan—Separate Exhaust Streams................................404
Problems.............................................................................427
Chapter 8. Engine Performance Analysis............................................437
8.1 Introduction.........................................................................437
8.2 Gas Generator.....................................................................447
8.3 Turbojet Engine...................................................................464
8.4 Turbojet Engine with Afterburning.......................................486
8.5 Turbofan Engine—Separate Exhausts and
Convergent Nozzles........................................................499
Problems..............................................................................524
Chapter 9. Turbomachinery.................................................................537
9.1 Introduction.........................................................................537
9.2 Euler's Turbomachinery Equations.......................................537
9.3 Axial-Flow Compressor Analysis...........................................539
9.4 Centrifugal-Flow Compressor Analysis.................................600
9.5 Axial-Flow Turbine Analysis..................................................607
9.6 Centrifugal-Flow Turbine Analysis........................................668
Problems..............................................................................674
Chapter 10. Inlets, Nozzles, and Combustion Systems......................685
10.1 Introduction to Inlets and Nozzles.....................................685
10.2 Inlets..................................................................................685
10.3 Subsonic Inlets...................................................................686
10.4 Supersonic Inlets................................................................695
10.5 Exhaust Nozzles.................................................................726
10.6 Introduction to Combustion Systems.................................744
10.7 Main Burners......................................................................757
10.8 Afterburners.......................................................................769
Problems............................................................................779
Appendix A. Altitude Tables...................................................................785
Appendix B. Gas Turbine Engine Data...................................................793
Appendix C. Data for Some Liquid-Propellant Rocket Engines.............801
Appendix D. Air and (CH2)n Properties at Low Pressure....................803
Appendix E. Turbomachinery Stresses and Materials...........................821
Appendix F. About the Software............................................................835
Appendix G. Answers to Selected Problems..........................................841
References..............................................................................................845
Index.......................................................................................................851
Supporting Materials..............................................................................869
Supporting Material for Chapter 5: Parametric Cycle Analysis of
Ideal Engines
SM5.1 Ideal Mixed-Flow Turbofan with Afterburning
SM5.2 Ideal Turboprop Engines
SM5.3 Ideal Turboshaft Engine with Regeneration
Supporting Material for Chapter 7: Parametric Cycle Analysis for
Real Engines
SM7.1 Turbofan with Afterburning—Separate Exhaust Systems
SM7.2 Turbofan with Afterburning—Mixed Exhaust Stream
SM7.3 Turboprop Engine
SM7.4 Variable Gas Properties
Supporting Material for Chapter 8: Engine Performance Analysis
SM8.1 Turbofan with Afterburning—Mixed Exhaust Stream
SM8.2 Turboprop Engine
SM8.3 Variable Gas Properties
SM8.4 Performance Analysis—Dual-Spool Afterburning
Turbojet Engine
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