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Aerospace software engineering [[electronic resource] ] : a collection of concepts / / edited by Christine Anderson, Merlin Dorfman
| Aerospace software engineering [[electronic resource] ] : a collection of concepts / / edited by Christine Anderson, Merlin Dorfman |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1991 |
| Descrizione fisica | 1 online resource (636 p.) |
| Disciplina |
629.1 s
629.13/00285/53 |
| Altri autori (Persone) |
AndersonChristine <1947->
DorfmanM (Merlin) |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Aeronautics - Computer programs
Astronautics - Computer programs Software engineering |
| ISBN |
1-60086-609-3
1-60086-390-6 1-60119-253-3 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Preface""; ""Table of Contents""; ""Chapter 1 Introduction""; ""1.1 Current Problems""; ""1.2 Current Practice""; ""Chapter 2 Life Cycle Models""; ""2.1 The DOD Life Cycle Mode""; ""2.2 NASA Life Cycle Model""; ""2.3 Alternative Software Life Cycle Models""; ""Chapter 3 Development Methodologies""; ""3.1 Requirements""; ""3.2 Design""; ""3.3 Testing""; ""3.4 Mathematical Forecasting""; ""3.5 Cleanroom: An Alternative Software Development Process""; ""Chapter 4 Tools and Environments""; ""4.1 Software Development Environments""
""4.2 Tools and Environments""""Chapter 5 Software Engineering Management""; ""5.1 Management Principles""; ""5.2 Resource Estimation""; ""Chapter 6 Quality Assurance""; ""6.1 Reliability""; ""6.2 Safety""; ""6.3 Metrics""; ""Chapter 7 Programming Languages""; ""7.1 Programming Languages Overview""; ""7.2 Ada""; ""7.3 Artificial Intelligence Languages""; ""Chapter 8 Reuse""; ""8.1 Software Reuse: Definition and Overview""; ""8.2 Engineering and Application of Reusable Software Resources""; ""8.3 Reuse Tools""; ""Chapter 9 Legal Issues""; ""9.1 Legal Issues"" ""Chapter 10 Emerging Technologies""""10.1 Impact of Knowledge-Based Software Engineering on Aerospace Systems""; ""10.2 Impact of Innovative Architectures""; ""10.3 Symmetric Parallel Processing""; ""Chapter 11 Non-U.S. Aerospace Software Engineering""; ""11.1 Aerospace Software Engineering in France""; ""11.2 Aerospace Software Engineering in the United Kingdom""; ""11.3 Aerospace Software in Sweden""; ""11.4 Aerospace Software Engineering in Japan""; ""Chapter 12 Conclusion/Vision""; ""12.1 Software Engineering of Tomorrow""; ""12.2 Coping with the Crisis""; ""Author Index for Volume 136"" |
| Record Nr. | UNINA-9910783935003321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1991 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aerospace software engineering [[electronic resource] ] : a collection of concepts / / edited by Christine Anderson, Merlin Dorfman
| Aerospace software engineering [[electronic resource] ] : a collection of concepts / / edited by Christine Anderson, Merlin Dorfman |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1991 |
| Descrizione fisica | 1 online resource (636 p.) |
| Disciplina |
629.1 s
629.13/00285/53 |
| Altri autori (Persone) |
AndersonChristine <1947->
DorfmanM (Merlin) |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Aeronautics - Computer programs
Astronautics - Computer programs Software engineering |
| ISBN |
1-60086-609-3
1-60086-390-6 1-60119-253-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Preface""; ""Table of Contents""; ""Chapter 1 Introduction""; ""1.1 Current Problems""; ""1.2 Current Practice""; ""Chapter 2 Life Cycle Models""; ""2.1 The DOD Life Cycle Mode""; ""2.2 NASA Life Cycle Model""; ""2.3 Alternative Software Life Cycle Models""; ""Chapter 3 Development Methodologies""; ""3.1 Requirements""; ""3.2 Design""; ""3.3 Testing""; ""3.4 Mathematical Forecasting""; ""3.5 Cleanroom: An Alternative Software Development Process""; ""Chapter 4 Tools and Environments""; ""4.1 Software Development Environments""
""4.2 Tools and Environments""""Chapter 5 Software Engineering Management""; ""5.1 Management Principles""; ""5.2 Resource Estimation""; ""Chapter 6 Quality Assurance""; ""6.1 Reliability""; ""6.2 Safety""; ""6.3 Metrics""; ""Chapter 7 Programming Languages""; ""7.1 Programming Languages Overview""; ""7.2 Ada""; ""7.3 Artificial Intelligence Languages""; ""Chapter 8 Reuse""; ""8.1 Software Reuse: Definition and Overview""; ""8.2 Engineering and Application of Reusable Software Resources""; ""8.3 Reuse Tools""; ""Chapter 9 Legal Issues""; ""9.1 Legal Issues"" ""Chapter 10 Emerging Technologies""""10.1 Impact of Knowledge-Based Software Engineering on Aerospace Systems""; ""10.2 Impact of Innovative Architectures""; ""10.3 Symmetric Parallel Processing""; ""Chapter 11 Non-U.S. Aerospace Software Engineering""; ""11.1 Aerospace Software Engineering in France""; ""11.2 Aerospace Software Engineering in the United Kingdom""; ""11.3 Aerospace Software in Sweden""; ""11.4 Aerospace Software Engineering in Japan""; ""Chapter 12 Conclusion/Vision""; ""12.1 Software Engineering of Tomorrow""; ""12.2 Coping with the Crisis""; ""Author Index for Volume 136"" |
| Record Nr. | UNINA-9910816719103321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1991 | ||
| 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 |
| 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 [[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-9910812009403321 |
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Oates Gordon C
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| Reston, Va., : American Institute of Aeronautics and Astronautics, c1997 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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AIAA Dynamics specialists conference : a collection of technical papers / < general chair Dr. Thomas Strganac, technical program chair Dr. Michael Tinker> : April 18-19, 1996, Salt Lake City, UT
| AIAA Dynamics specialists conference : a collection of technical papers / < general chair Dr. Thomas Strganac, technical program chair Dr. Michael Tinker> : April 18-19, 1996, Salt Lake City, UT |
| Pubbl/distr/stampa | Reston, Va : American Institute of Aeronautics and Astronautics, c1996 |
| Descrizione fisica | V,449 p. : ill. ; 28 cm |
| ISBN | 1-56347-211-2 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-990008787220403321 |
| Reston, Va : American Institute of Aeronautics and Astronautics, c1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
AIAA journal : devoted to aerospace research and development / American Institute of Aeronautics and Astronautics
| AIAA journal : devoted to aerospace research and development / American Institute of Aeronautics and Astronautics |
| Pubbl/distr/stampa | New-York : American Institute of Aeronautics and Astronautics, 1963- |
| Descrizione fisica | fascicoli |
| Soggetto non controllato | Aerotecnica |
| ISSN | 0001-1452 |
| Formato | Materiale a stampa |
| Livello bibliografico | Periodico |
| Lingua di pubblicazione | eng |
| Note periodicità | Mensile |
| Record Nr. | UNIPARTHENOPE-000002090 |
| New-York : American Institute of Aeronautics and Astronautics, 1963- | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Parthenope | ||
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