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Aerothermodynamics of aircraft engine components [[electronic resource] /] / edited by Gordon C. Oates
| Aerothermodynamics of aircraft engine components [[electronic resource] /] / edited by Gordon C. Oates |
| Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, c1985 |
| Descrizione fisica | 1 online resource (559 p.) |
| Disciplina | 629.134/353 |
| Altri autori (Persone) | OatesGordon C |
| Collana | AIAA education series |
| Soggetto topico |
Aerothermodynamics
Aircraft gas-turbines |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-133-4
1-60086-005-2 1-60119-204-5 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Preface""; ""Chapter 1. Fundamentals of Combustion""; ""1.1 Introduction""; ""1.2 Chemistry""; ""1.3 Thermodynamics""; ""1.4 Gasdynamics and Diffusion Processes""; ""1.5 Combustion Parameters""; ""1.6 Jet Fuels""; ""1.7 Summary""; ""Chapter 2. Afterburners""; ""2.1 Introduction""; ""2.2 Diffuser""; ""2.3 Fuel Injection, Atomization, and Vaporization""; ""2.4 Ignition""; ""2.5 Stabilization Process""; ""2.6 Flame Spread in Premixed and Homogeneous Fuel-Air Mixtures""; ""2.7 Nozzle and Fuel Control Systems""
""2.8 Complete Afterburner Systems""""2.9 Combustion Instabilities""; ""Chapter 3. Axial Flow Compressor Aerodynamics""; ""3.1 Introduction""; ""3.2 Axial Flow Compressor Nomenclature and Terminology""; ""3.3 Characteristics of the Flow in Axial Flow Compressor Configurations""; ""3.4 Aerodynamic Design Objectives for Axial Flow Compressor Units""; ""3.5 Elements of a Compressor Design System�Technical Requirements""; ""3.6 Content of Current and Developing Design Systems� The Technology Base""; ""3.7 Component and Configuration Experimental Development"" ""3.8 Axial Flow Compressor Performance Trends""""Chapter 4. Turbine Aerodynamics""; ""4.1 Introduction""; ""4.2 Turbine Airfoil Characteristics""; ""4.3 Design Considerations""; ""4.4 Performance""; ""4.5 Profile Aerodynamics""; ""4.6 End Wall Aerodynamics""; ""4.7 Parasitic Loss""; ""4.8 Structural Excitation""; ""4.9 Stage Performance""; ""4.10 Looking Ahead""; ""4.11 Looking Back�Developments Since 1977""; ""Chapter 5. Turbine Cooling""; ""5.1 Introduction""; ""5.2 Cooling Design Problem""; ""5.3 Airfoil Cooling""; ""5.4 End Wall Cooling""; ""5.5 Conclusions""; ""5.6 Recent Advances"" ""Chapter 6. Computation of Turbomachinery Boundary Layers""""6.1 Introduction""; ""6.2 Two-Dimensional or Axisymmetric Boundary Layers""; ""6.3 Three-Dimensional Boundary Layers""; ""6.4 Boundary-Layer Separation""; ""6.5 Turbulence Models""; ""6.6 Conclusion""; ""Chapter 7. Engine Noise""; ""7.1 Introduction""; ""7.2 Scales and Ratings for Noise""; ""7.3 Introduction to Acoustics of Ducts""; ""7.4 Compressor and Fan Noise""; ""7.5 Turbine Noise""; ""7.6 Core Noise""; ""7.7 Acoustic Treatment""; ""7.8 Conclusions and Future Prospects""; ""Subject Index""; ""A""; ""B""; ""C""; ""D""; ""E"" ""F""""G""; ""H""; ""I""; ""J""; ""K""; ""L""; ""M""; ""N""; ""O""; ""P""; ""R""; ""S""; ""T""; ""V""; ""W"" |
| Record Nr. | UNINA-9910451071403321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, c1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerothermodynamics of aircraft engine components [[electronic resource] /] / edited by Gordon C. Oates
| Aerothermodynamics of aircraft engine components [[electronic resource] /] / edited by Gordon C. Oates |
| Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, c1985 |
| Descrizione fisica | 1 online resource (559 p.) |
| Disciplina | 629.134/353 |
| Altri autori (Persone) | OatesGordon C |
| Collana | AIAA education series |
| Soggetto topico |
Aerothermodynamics
Aircraft gas-turbines |
| ISBN |
1-60086-133-4
1-60086-005-2 1-60119-204-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Preface""; ""Chapter 1. Fundamentals of Combustion""; ""1.1 Introduction""; ""1.2 Chemistry""; ""1.3 Thermodynamics""; ""1.4 Gasdynamics and Diffusion Processes""; ""1.5 Combustion Parameters""; ""1.6 Jet Fuels""; ""1.7 Summary""; ""Chapter 2. Afterburners""; ""2.1 Introduction""; ""2.2 Diffuser""; ""2.3 Fuel Injection, Atomization, and Vaporization""; ""2.4 Ignition""; ""2.5 Stabilization Process""; ""2.6 Flame Spread in Premixed and Homogeneous Fuel-Air Mixtures""; ""2.7 Nozzle and Fuel Control Systems""
""2.8 Complete Afterburner Systems""""2.9 Combustion Instabilities""; ""Chapter 3. Axial Flow Compressor Aerodynamics""; ""3.1 Introduction""; ""3.2 Axial Flow Compressor Nomenclature and Terminology""; ""3.3 Characteristics of the Flow in Axial Flow Compressor Configurations""; ""3.4 Aerodynamic Design Objectives for Axial Flow Compressor Units""; ""3.5 Elements of a Compressor Design System�Technical Requirements""; ""3.6 Content of Current and Developing Design Systems� The Technology Base""; ""3.7 Component and Configuration Experimental Development"" ""3.8 Axial Flow Compressor Performance Trends""""Chapter 4. Turbine Aerodynamics""; ""4.1 Introduction""; ""4.2 Turbine Airfoil Characteristics""; ""4.3 Design Considerations""; ""4.4 Performance""; ""4.5 Profile Aerodynamics""; ""4.6 End Wall Aerodynamics""; ""4.7 Parasitic Loss""; ""4.8 Structural Excitation""; ""4.9 Stage Performance""; ""4.10 Looking Ahead""; ""4.11 Looking Back�Developments Since 1977""; ""Chapter 5. Turbine Cooling""; ""5.1 Introduction""; ""5.2 Cooling Design Problem""; ""5.3 Airfoil Cooling""; ""5.4 End Wall Cooling""; ""5.5 Conclusions""; ""5.6 Recent Advances"" ""Chapter 6. Computation of Turbomachinery Boundary Layers""""6.1 Introduction""; ""6.2 Two-Dimensional or Axisymmetric Boundary Layers""; ""6.3 Three-Dimensional Boundary Layers""; ""6.4 Boundary-Layer Separation""; ""6.5 Turbulence Models""; ""6.6 Conclusion""; ""Chapter 7. Engine Noise""; ""7.1 Introduction""; ""7.2 Scales and Ratings for Noise""; ""7.3 Introduction to Acoustics of Ducts""; ""7.4 Compressor and Fan Noise""; ""7.5 Turbine Noise""; ""7.6 Core Noise""; ""7.7 Acoustic Treatment""; ""7.8 Conclusions and Future Prospects""; ""Subject Index""; ""A""; ""B""; ""C""; ""D""; ""E"" ""F""""G""; ""H""; ""I""; ""J""; ""K""; ""L""; ""M""; ""N""; ""O""; ""P""; ""R""; ""S""; ""T""; ""V""; ""W"" |
| Record Nr. | UNINA-9910783937603321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, c1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerothermodynamics of aircraft engine components [[electronic resource] /] / edited by Gordon C. Oates
| Aerothermodynamics of aircraft engine components [[electronic resource] /] / edited by Gordon C. Oates |
| Pubbl/distr/stampa | New York, N.Y., : American Institute of Aeronautics and Astronautics, c1985 |
| Descrizione fisica | 1 online resource (559 p.) |
| Disciplina | 629.134/353 |
| Altri autori (Persone) | OatesGordon C |
| Collana | AIAA education series |
| Soggetto topico |
Aerothermodynamics
Aircraft gas-turbines |
| ISBN |
1-60086-133-4
1-60086-005-2 1-60119-204-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Preface""; ""Chapter 1. Fundamentals of Combustion""; ""1.1 Introduction""; ""1.2 Chemistry""; ""1.3 Thermodynamics""; ""1.4 Gasdynamics and Diffusion Processes""; ""1.5 Combustion Parameters""; ""1.6 Jet Fuels""; ""1.7 Summary""; ""Chapter 2. Afterburners""; ""2.1 Introduction""; ""2.2 Diffuser""; ""2.3 Fuel Injection, Atomization, and Vaporization""; ""2.4 Ignition""; ""2.5 Stabilization Process""; ""2.6 Flame Spread in Premixed and Homogeneous Fuel-Air Mixtures""; ""2.7 Nozzle and Fuel Control Systems""
""2.8 Complete Afterburner Systems""""2.9 Combustion Instabilities""; ""Chapter 3. Axial Flow Compressor Aerodynamics""; ""3.1 Introduction""; ""3.2 Axial Flow Compressor Nomenclature and Terminology""; ""3.3 Characteristics of the Flow in Axial Flow Compressor Configurations""; ""3.4 Aerodynamic Design Objectives for Axial Flow Compressor Units""; ""3.5 Elements of a Compressor Design System�Technical Requirements""; ""3.6 Content of Current and Developing Design Systems� The Technology Base""; ""3.7 Component and Configuration Experimental Development"" ""3.8 Axial Flow Compressor Performance Trends""""Chapter 4. Turbine Aerodynamics""; ""4.1 Introduction""; ""4.2 Turbine Airfoil Characteristics""; ""4.3 Design Considerations""; ""4.4 Performance""; ""4.5 Profile Aerodynamics""; ""4.6 End Wall Aerodynamics""; ""4.7 Parasitic Loss""; ""4.8 Structural Excitation""; ""4.9 Stage Performance""; ""4.10 Looking Ahead""; ""4.11 Looking Back�Developments Since 1977""; ""Chapter 5. Turbine Cooling""; ""5.1 Introduction""; ""5.2 Cooling Design Problem""; ""5.3 Airfoil Cooling""; ""5.4 End Wall Cooling""; ""5.5 Conclusions""; ""5.6 Recent Advances"" ""Chapter 6. Computation of Turbomachinery Boundary Layers""""6.1 Introduction""; ""6.2 Two-Dimensional or Axisymmetric Boundary Layers""; ""6.3 Three-Dimensional Boundary Layers""; ""6.4 Boundary-Layer Separation""; ""6.5 Turbulence Models""; ""6.6 Conclusion""; ""Chapter 7. Engine Noise""; ""7.1 Introduction""; ""7.2 Scales and Ratings for Noise""; ""7.3 Introduction to Acoustics of Ducts""; ""7.4 Compressor and Fan Noise""; ""7.5 Turbine Noise""; ""7.6 Core Noise""; ""7.7 Acoustic Treatment""; ""7.8 Conclusions and Future Prospects""; ""Subject Index""; ""A""; ""B""; ""C""; ""D""; ""E"" ""F""""G""; ""H""; ""I""; ""J""; ""K""; ""L""; ""M""; ""N""; ""O""; ""P""; ""R""; ""S""; ""T""; ""V""; ""W"" |
| Record Nr. | UNINA-9910817542403321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, c1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerothermodynamics of gas turbine and rocket propulsion [[electronic resource] /] / Gordon C. Oates
| Aerothermodynamics of gas turbine and rocket propulsion [[electronic resource] /] / Gordon C. Oates |
| Autore | Oates Gordon C |
| Edizione | [3rd ed.] |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c1997 |
| Descrizione fisica | 1 online resource (469 p.) |
| Disciplina | 629.134/353 |
| Collana | AIAA education series |
| Soggetto topico |
Aerothermodynamics
Aircraft gas-turbines Rocket engines |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-134-2
1-60086-006-0 1-60119-222-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""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""
""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"" ""3.2 Expression for the Thrust""""3.3 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"" ""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"" ""6.2 The Thrust Equation""""6.3 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"" ""8.3 Off-Design Analysis of the Turbofan"" |
| Record Nr. | UNINA-9910451105603321 |
Oates Gordon C
|
||
| Reston, Va., : American Institute of Aeronautics and Astronautics, c1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerothermodynamics of gas turbine and rocket propulsion [[electronic resource] /] / Gordon C. Oates
| Aerothermodynamics of gas turbine and rocket propulsion [[electronic resource] /] / Gordon C. Oates |
| Autore | Oates Gordon C |
| Edizione | [3rd ed.] |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c1997 |
| Descrizione fisica | 1 online resource (469 p.) |
| Disciplina | 629.134/353 |
| Collana | AIAA education series |
| Soggetto topico |
Aerothermodynamics
Aircraft gas-turbines Rocket engines |
| ISBN |
1-60086-134-2
1-60086-006-0 1-60119-222-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""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""
""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"" ""3.2 Expression for the Thrust""""3.3 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"" ""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"" ""6.2 The Thrust Equation""""6.3 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"" ""8.3 Off-Design Analysis of the Turbofan"" |
| Record Nr. | UNINA-9910783934603321 |
|
Oates Gordon C
|
||
| Reston, Va., : American Institute of Aeronautics and Astronautics, c1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerothermodynamics of gas turbine and rocket propulsion / / Gordon C. Oates
| Aerothermodynamics of gas turbine and rocket propulsion / / Gordon C. Oates |
| Autore | Oates Gordon C |
| Edizione | [3rd ed.] |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, c1997 |
| Descrizione fisica | 1 online resource (469 p.) |
| Disciplina | 629.134/353 |
| Collana | AIAA education series |
| Soggetto topico |
Aerothermodynamics
Aircraft gas-turbines Rocket engines |
| ISBN |
1-60086-134-2
1-60086-006-0 1-60119-222-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""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""
""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"" ""3.2 Expression for the Thrust""""3.3 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"" ""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"" ""6.2 The Thrust Equation""""6.3 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"" ""8.3 Off-Design Analysis of the Turbofan"" |
| Record Nr. | UNINA-9910812009403321 |
|
Oates Gordon C
|
||
| Reston, Va., : American Institute of Aeronautics and Astronautics, c1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft engines and gas turbines [[electronic resource] /] / Jack L. Kerrebrock
| Aircraft engines and gas turbines [[electronic resource] /] / Jack L. Kerrebrock |
| Autore | Kerrebrock Jack L |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | [Cambridge, Mass.], : MIT Press, 1992 |
| Descrizione fisica | 1 online resource (xv, 478 p.) |
| Soggetto topico | Aircraft gas-turbines |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910260641503321 |
|
Kerrebrock Jack L
|
||
| [Cambridge, Mass.], : MIT Press, 1992 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft gas turbine engine technology / Irwin E. Treager
| Aircraft gas turbine engine technology / Irwin E. Treager |
| Autore | Treager, Irwin E. |
| Edizione | [3rd ed.] |
| Pubbl/distr/stampa | New York, N.Y. : Glencoe, c1996 |
| Descrizione fisica | x, 677 p. : ill. ; 28 cm |
| Disciplina | 629.134 |
| Collana |
Aviation technology series.
Glencoe aviation technology series |
| Soggetto topico | Aircraft gas-turbines |
| ISBN | 0028018281 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNISALENTO-991001145429707536 |
|
Treager, Irwin E.
|
||
| New York, N.Y. : Glencoe, c1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. del Salento | ||
| ||
Aircraft propulsion and gas turbine engines / / by Ahmed F. El-Sayed
| Aircraft propulsion and gas turbine engines / / by Ahmed F. El-Sayed |
| Autore | El-Sayed Ahmed F. |
| Edizione | [Second edition.] |
| Pubbl/distr/stampa | Boca Raton, FL : , : CRC Press, an imprint of Taylor and Francis, , [2017] |
| Descrizione fisica | 1 online resource (xxvii, 1,447 pages) : illustrations |
| Disciplina | 629.134/353 |
| Soggetto topico |
Avions - Motors turboreactors
Airplanes - Turbojet engines Aircraft gas-turbines |
| Soggetto genere / forma | Electronic books. |
| ISBN |
9781315156743
1-315-15674-1 1-5231-1396-0 1-4665-9517-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | History and classifications of aero-engine -- Performance parameters of jet engines -- Pulsejet and ramjet engines -- Turbojet engine -- Turbofan engines -- Shaft engines -- High speed supersonic and hypersonic engines -- Industrial gas turbines -- Power plant installation and intakes -- Combustion systems -- Exhaust system -- Centrifugal compressors -- Axial flow compressors and fans -- Axial turbines -- Radial inflow turbines -- Module matching -- Selected topics -- Introduction to rocketry -- Rocket engines. |
| Record Nr. | UNINA-9910466775303321 |
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El-Sayed Ahmed F.
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| Boca Raton, FL : , : CRC Press, an imprint of Taylor and Francis, , [2017] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft propulsion and gas turbine engines / / Ahmed F. El-Sayed
| Aircraft propulsion and gas turbine engines / / Ahmed F. El-Sayed |
| Autore | El-Sayed Ahmed F |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Boca Raton, Fla., : CRC P., 2017 |
| Descrizione fisica | 1 online resource (xxvii, 1447 p.) : ill |
| Disciplina | 629.134353 |
| Soggetto topico |
Airplanes - Turbojet engines
Aircraft gas-turbines |
| ISBN |
9781315156743 (e-book)
9781466595163 (hbk.) 1-4665-9518-3 1-315-15674-1 1-5231-1396-0 1-4665-9517-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Section I Aero engines and gas turbines -- 1. History and classifications of aero-engine -- 2. Performance parameters of jet engines -- 3. Pulsejet and ramjet engines -- 4. Turbojet engine -- 5. Turbofan engines -- 6. Shaft engines: internal combustion, turboprop, turboshaft, and propfan engines -- 7. High speed supersonic and hypersonic engines -- 8. Industrial gas turbines -- Section II Component design -- 9. Powerplant installation and intakes -- 10. Combustion systems -- 11. Exhaust system -- 12. Centrifugal compressors -- 13. Axial flow compressors and fans -- 14. Axial turbines -- 15. Radial inflow turbines -- 16. Module matching -- 17. Selected topics -- Section III Rocket propulsion -- 18. Introduction to rocketry -- 19. Rocket engines -- Appendix A: Glossary -- Appendix B: Turbofan -- Appendix C: Samples of gas turbines (representative manufacturers) -- Index. |
| Record Nr. | UNINA-9910793188103321 |
|
El-Sayed Ahmed F
|
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| Boca Raton, Fla., : CRC P., 2017 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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