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Elements of Propulsion: Gas Turbines and Rockets Second Edition [Hardback]

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  • Formāts: Hardback, 976 pages
  • Sērija : AIAA Education Series
  • Izdošanas datums: 15-Sep-2016
  • Izdevniecība: American Institute of Aeronautics & Astronautics
  • ISBN-10: 1624103715
  • ISBN-13: 9781624103711
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  • Hardback
  • Cena: 136,64 €
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Elements of Propulsion: Gas Turbines and Rockets Second EditionPalielināt
  • Formāts: Hardback, 976 pages
  • Sērija : AIAA Education Series
  • Izdošanas datums: 15-Sep-2016
  • Izdevniecība: American Institute of Aeronautics & Astronautics
  • ISBN-10: 1624103715
  • ISBN-13: 9781624103711
Citas grāmatas par šo tēmu:
Permanent link: https://www.kriso.lv/db/9781624103711.html
Keywords:
Mattingly and Boyer present an undergraduate textbook introducing the fundamentals of gas turbine engines and jet propulsion, the basic elements that determine the behavior, design, and operation of the jet engines and chemical rocket motors used for propulsion. The text contains sufficient material for two sequential courses on propulsion: an introductory course on jet propulsion, and a course on gas turbine engine components. They retain from the first edition the historical foreword by Hans von Ohain, the German inventor of the jet engine. Annotation ©2016 Ringgold, Inc., Portland, OR (protoview.com)

Papildus informācija

Supporting Material for Chapter 5. Supporting Material for Chapter 7. Supporting Material for Chapter 8. lnlets, Nozzles, and Combustion Systems. Supplemental JANNAF Tables Software. Software User Guides.
Foreword to the Second Edition xiii
Foreword to the First Edition xxv
Preface lxiii
Acknowledgments lxvii
Nomenclature lxix
Chapter 1 Introduction
1(78)
1.1 Propulsion
1(1)
1.2 Units and Dimensions
2(1)
1.3 Operational Envelopes and Standard Atmosphere
3(3)
1.4 Airbreathing Engines
6(32)
1.5 Aircraft Performance
38(23)
1.6 Rocket Engines
61(18)
Problems
68(11)
Chapter 2 Review of Fundamentals
79(56)
2.1 Introductory Comments
79(1)
2.2 Thermodynamics Fundamentals
80(3)
2.3 Control Volume Approach to Governing Equations
83(19)
2.4 Perfect Gas
102(18)
2.5 Chemical Reactions
120(15)
Problems
128(7)
Chapter 3 Compressible Flow
135(110)
3.1 Introduction
135(1)
3.2 Compressible Flow Properties
135(16)
3.3 Velocity-Area Variation for Isentropic, Adiabatic Flow
151(4)
3.4 Two-Dimensional Small-Amplitude Wave Propagation
155(4)
3.5 Supersonic Compressions and Expansions
159(23)
3.6 Steady Flow, 1-D Gas Dynamics: Differential Control Volume Analysis
182(5)
3.7 Simple Flows
187(42)
3.8 Summary of Simple Flows
229(16)
Problems
232(13)
Chapter 4 Aircraft Gas Turbine Engine
245(36)
4.1 Introduction
245(1)
4.2 Generalized Thrust Equation
245(10)
4.3 Installed Thrust
255(5)
4.4 Gas Turbine Engine Components
260(10)
4.5 Brayton Cycle
270(6)
4.6 Aircraft Engine Design
276(5)
Problems
276(5)
Chapter 5 Parametric Cycle Analysis (PCA) of Ideal Engines
281(74)
5.1 Introduction
281(1)
5.2 Notation
282(3)
5.3 Design Inputs
285(1)
5.4 Steps of Engine Parametric Cycle Analysis
285(2)
5.5 Assumptions of Ideal Cycle Analysis
287(1)
5.6 Ideal Turbojet
287(7)
5.7 Ideal Turbojet with Afterburner
294(5)
5.8 Ideal Turbofan
299(12)
5.9 Ideal Turbofan with Optimum Bypass Ratio
311(4)
5.10 Ideal Turbofan with Optimum Fan Pressure Ratio
315(5)
5.11 Ideal Mixed-Flow Turbofan with Afterburning
320(6)
5.12 Ideal Turboprop Engines
326(11)
5.13 Ideal Pulse Detonation Engine
337(4)
5.14 Summary: PCA of Ideal Engines
341(14)
Problems
342(13)
Chapter 6 Component Performance
355(36)
6.1 Introduction
355(1)
6.2 Variation in Gas Properties
355(2)
6.3 Component Performance
357(1)
6.4 Inlet/Diffuser Pressure Recovery
357(2)
6.5 Compressor and Turbine Efficiencies
359(12)
6.6 Burner Efficiency and Pressure Loss
371(1)
6.7 Exhaust Nozzle Loss
372(1)
6.8 Mechanical Efficiency of a Power Shaft
372(1)
6.9 Mixer
372(5)
6.10 Gross Thrust
377(1)
6.11 Summary of Component Figures of Merit
378(2)
6.12 Component Performance with Variable cp
380(11)
Problems
387(4)
Chapter 7 Parametric Cycle Analysis (PCA) of Real Engines
391(74)
7.1 Introductory Comments and Assumptions
391(1)
7.2 Turbojet
392(14)
7.3 Turbojet with Afterburner
406(4)
7.4 Turbofan: Separate Exhaust Streams
410(21)
7.5 Turbofan with Afterburning: Mixed Exhaust Stream
431(9)
7.6 Turboprop Engine
440(8)
7.7 Variable Gas Properties
448(17)
Problems
453(12)
Chapter 8 Engine Performance Analysis (EPA)
465(110)
8.1 Introduction
465(12)
8.2 Gas Generator or Core
477(19)
8.3 Turbojet Engine
496(18)
8.4 Dual-Spool Turbojet Engine with Afterburning
514(8)
8.5 Dual-Spool Turbofan Engine: Separate Exhausts and Convergent Nozzles
522(16)
8.6 Dual-Spool Turbofan with Afterburning: Mixed Exhaust Stream
538(14)
8.7 Turboprop Engine
552(8)
8.8 Variable Gas Properties
560(15)
Problems
560(15)
Chapter 9 Turbomachinery
575(144)
9.1 Introduction
575(1)
9.2 Euler's Turbomachinery Equations
576(2)
9.3 Axial-Flow Compressor Analysis
578(65)
9.4 Centrifugal-Flow Compressor Analysis
643(8)
9.5 Axial-Flow Turbine Analysis
651(68)
Problems
704(15)
Chapter 10 Rocket Propulsion
719(78)
10.1 Introduction
719(6)
10.2 Rocket Propulsion Requirements and Capabilities
725(10)
10.3 Rocket Propulsion Engines
735(14)
10.4 Types of Rocket Nozzles
749(6)
10.5 Parameters for Chemical Rockets
755(42)
Problems
791(6)
Chapter 11 Inlets, Nozzles, and Combustion Systems online
Appendix A Altitude Tables 797(8)
Appendix B Gas Turbine Engine Data: Uninstalled Performance 805(10)
Appendix C Data for Some Liquid-Propellant Rocket Engines 815(2)
Appendix D Compressible Flow Functions 817(38)
Appendix E Normal Shock Functions 855(8)
Appendix F Two-Dimensional Oblique Shock Functions 863(12)
Appendix G Rayleigh Line Flow Functions 875(10)
Appendix H Fanno Line Flow Functions 885(10)
Appendix I Turbomachinery Stresses and Materials 895(16)
Appendix J About the Software 911(8)
Appendix K Answers to Selected Problems 919(4)
References 923(4)
About the Authors 927(2)
Index 929