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|a UAMI
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1 |
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|a Oates, Gordon C.
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1 |
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|a Aerothermodynamics of gas turbine and rocket propulsion /
|c Gordon C. Oates.
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| 250 |
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|a 3rd ed.
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| 260 |
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|a Reston, VA :
|b American Institute of Aeronautics and Astronautics,
|c ©1997.
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| 300 |
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|a 1 online resource (xii, 456 pages) :
|b illustrations
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| 336 |
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|a text
|b txt
|2 rdacontent
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| 337 |
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|a computer
|b c
|2 rdamedia
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| 338 |
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|a online resource
|b cr
|2 rdacarrier
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|a data file
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| 490 |
1 |
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|a AIAA education series
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| 504 |
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|a Includes bibliographical references and index.
|
| 588 |
0 |
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|a Print version record.
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| 506 |
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|3 Use copy
|f Restrictions unspecified
|2 star
|5 MiAaHDL
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| 533 |
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|a Electronic reproduction.
|b [Place of publication not identified] :
|c HathiTrust Digital Library,
|d 2010.
|5 MiAaHDL
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| 538 |
|
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|a Master and use copy. Digital master created according to Benchmark for Faithful Digital Reproductions of Monographs and Serials, Version 1. Digital Library Federation, December 2002.
|u http://purl.oclc.org/DLF/benchrepro0212
|5 MiAaHDL
|
| 583 |
1 |
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|a digitized
|c 2010
|h HathiTrust Digital Library
|l committed to preserve
|2 pda
|5 MiAaHDL
|
| 506 |
|
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|a Access restricted to Ryerson students, faculty and staff.
|5 CaOTR
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0 |
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|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
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| 505 |
8 |
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|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 System�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""
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| 505 |
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|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
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| 505 |
8 |
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|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""
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| 505 |
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|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
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| 546 |
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|a English.
|
| 590 |
|
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|a Knovel
|b ACADEMIC - Aerospace & Radar Technology
|
| 650 |
|
0 |
|a Aerothermodynamics.
|
| 650 |
|
0 |
|a Aircraft gas-turbines.
|
| 650 |
|
0 |
|a Rocket engines.
|
| 650 |
|
6 |
|a Aérothermodynamique.
|
| 650 |
|
6 |
|a Moteurs-fusées.
|
| 650 |
|
7 |
|a Aerothermodynamics
|2 fast
|
| 650 |
|
7 |
|a Aircraft gas-turbines
|2 fast
|
| 650 |
|
7 |
|a Rocket engines
|2 fast
|
| 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://appknovel.uam.elogim.com/kn/resources/kpAGTRPE01/toc
|z Texto completo
|
| 938 |
|
|
|a ebrary
|b EBRY
|n ebr10516704
|
| 938 |
|
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|a YBP Library Services
|b YANK
|n 7355835
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|a 92
|b IZTAP
|
