Aerothermodynamics of gas turbine and rocket propulsion

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Bibliographic Details
Main Author: Oates, Gordon C.
Format: eBook
Language: English
Published: Reston, VA : American Institute of Aeronautics and Astronautics, ©1997.
Edition: 3rd ed.
Series: AIAA education series.
Subjects:
Aerothermodynamics.
Aircraft gas-turbines.
Rocket engines.
elektronické knihy
electronic books
ISBN: 9781601192226
1601192223
1563472414
9781563472411
1600860060
9781600860065
Physical Description: 1 online resource (xii, 456 pages) : illustrations

Cover

Table of contents

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042 |a dlr 
100 1 |a Oates, Gordon C. 
245 1 0 |a Aerothermodynamics of gas turbine and rocket propulsion /  |c Gordon C. Oates. 
250 |a 3rd ed. 
260 |a Reston, VA :  |b American Institute of Aeronautics and Astronautics,  |c ©1997. 
300 |a 1 online resource (xii, 456 pages) :  |b illustrations 
336 |a text  |b txt  |2 rdacontent 
337 |a computer  |b c  |2 rdamedia 
338 |a online resource  |b cr  |2 rdacarrier 
490 1 |a AIAA education series 
504 |a Includes bibliographical references and index. 
505 0 |a 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 
505 8 |a ""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"" 
505 8 |a 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 
505 8 |a ""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"" 
505 8 |a 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 
506 |a Plný text je dostupný pouze z IP adres počítačů Univerzity Tomáše Bati ve Zlíně nebo vzdáleným přístupem pro zaměstnance a studenty 
590 |a Knovel  |b Knovel (All titles) 
650 0 |a Aerothermodynamics. 
650 0 |a Aircraft gas-turbines. 
650 0 |a Rocket engines. 
655 7 |a elektronické knihy  |7 fd186907  |2 czenas 
655 9 |a electronic books  |2 eczenas 
776 0 8 |i Print version:  |a Oates, Gordon C.  |t Aerothermodynamics of gas turbine and rocket propulsion.  |b 3rd ed.  |d Reston, VA : American Institute of Aeronautics and Astronautics, ©1997  |z 1563472414  |w (DLC) 97051303  |w (OCoLC)38132650 
830 0 |a AIAA education series. 
856 4 0 |u https://proxy.k.utb.cz/login?url=https://app.knovel.com/hotlink/toc/id:kpAGTRPE01/aerothermodynamics-of-gas?kpromoter=marc  |y Full text 

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