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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 / / edited by Gordon C. Oates
| Aerothermodynamics of aircraft engine components / / edited by Gordon C. Oates |
| Edizione | [1st ed.] |
| 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-9910972342603321 |
| New York, N.Y., : American Institute of Aeronautics and Astronautics, c1985 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft propulsion systems technology and design [[electronic resource] /] / edited by Gordon C. Oates
| Aircraft propulsion systems technology and design [[electronic resource] /] / edited by Gordon C. Oates |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1989 |
| Descrizione fisica | 1 online resource (535 p.) |
| Disciplina | 629.134/353 |
| Altri autori (Persone) | OatesGordon C |
| Collana | AIAA education series |
| Soggetto topico | Aircraft gas-turbines |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-60086-149-0
1-60086-021-4 1-60119-206-1 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Chapter 1. Design and Development of Aircraft Propulsion Systems""; ""1.1 Introduction""; ""1.2 Engine Design Objectives""; ""1.3 Effect of Thermodynamic Variables on Engine Performance""; ""1.4 Development of Thrust""; ""1.5 Off-Design Performance of Gas Turbine Propulsion Engines""; ""1.6 Losses in Available Energy""; ""1.7 Interrelations Among Aerodynamic Components""; ""1.8 Interaction with Other Specialties""; ""1.9 Advanced Flow Calculations""; ""1.10 Biography of a Typical Engine""
""Chapter 2. Turbopropulsion Combustion Technology""""2.1 Introduction""; ""2.2 Combustion System Description/Definitions""; ""2.3 Component Considerations""; ""2.4 Design Tools""; ""2.5 Future Requirements""; ""2.6 Conclusions""; ""Chapter 3. Engine/Airframe Performance Matching""; ""3.1 Introduction""; ""3.2 Mission Analysis""; ""3.3 Optimization of Engine/Airplane Match""; ""3.4 Sensitivity and Influence Coefficients""; ""3.5 Computer Simulation of Gas Turbine Engines""; ""Chapter 4. Inlets and Inlet/Engine Integration""; ""4.1 Introduction"" ""4.2 Elements of a Successful Inlet/Engine Integration Program""""4.3 Definition of Subsonic Inlet/Engine Operational Requirements""; ""4.4 Definition of Supersonic Inlet/Engine Operational Requirements""; ""4.5 Engine Impact on Inlet Design""; ""4.6 Inlet Impact on Engine Design""; ""4.7 Validation of Inlet/Engine System""; ""Chapter 5. Variable Convergent-Divergent Exhaust Nozzle Aerodynamics""; ""5.1 Introduction""; ""5.2 Nozzle Concept""; ""5.3 Performance Predictions""; ""5.4 Aerodynamic Load Predictions""; ""Chapter 6. Engine Operability""; ""6.1 Introduction""; ""6.2 Definitions"" ""6.3 Stability Assessment""""6.4 Aerodynamic Interface Plane""; ""6.5 Total Pressure Distortion""; ""6.6 Total Temperature Distortion""; ""6.7 Planar Waves""; ""6.8 Recoverability""; ""6.9 Analytical Techniques""; ""6.10 Summary""; ""Chapter 7. Aeroelasticity and Unsteady Aerodynamics""; ""7.1 Introduction""; ""7.2 Overview of Turbomachinery Flutter""; ""7.3 Brief Survey of Turbomachinery Flutter Regimes""; ""7.4 Elementary Considerations of Aircraft Wing Flutter""; ""7.5 Fundamental Differences Between Turbomachinery Flutter and Wing Flutter"" ""7.6 Fundamental of Unsteady Aerodynamic Theory for Isolated Airfoils""""7.7 Unsteady Aerodynamic Theory for Cascaded Airfoils""; ""7.8 Dynamic Stall-Empiricism and Experiment""; ""7.9 Coupled Blade-Disk-Shroud Stability Theory""; ""Subject Index""; ""A""; ""B""; ""C""; ""D""; ""E""; ""F""; ""G""; ""H""; ""I""; ""K""; ""L""; ""M""; ""N""; ""O""; ""P""; ""R""; ""S""; ""T""; ""U""; ""V""; ""W"" |
| Record Nr. | UNINA-9910451120003321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1989 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft propulsion systems technology and design [[electronic resource] /] / edited by Gordon C. Oates
| Aircraft propulsion systems technology and design [[electronic resource] /] / edited by Gordon C. Oates |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1989 |
| Descrizione fisica | 1 online resource (535 p.) |
| Disciplina | 629.134/353 |
| Altri autori (Persone) | OatesGordon C |
| Collana | AIAA education series |
| Soggetto topico | Aircraft gas-turbines |
| ISBN |
1-60086-149-0
1-60086-021-4 1-60119-206-1 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Chapter 1. Design and Development of Aircraft Propulsion Systems""; ""1.1 Introduction""; ""1.2 Engine Design Objectives""; ""1.3 Effect of Thermodynamic Variables on Engine Performance""; ""1.4 Development of Thrust""; ""1.5 Off-Design Performance of Gas Turbine Propulsion Engines""; ""1.6 Losses in Available Energy""; ""1.7 Interrelations Among Aerodynamic Components""; ""1.8 Interaction with Other Specialties""; ""1.9 Advanced Flow Calculations""; ""1.10 Biography of a Typical Engine""
""Chapter 2. Turbopropulsion Combustion Technology""""2.1 Introduction""; ""2.2 Combustion System Description/Definitions""; ""2.3 Component Considerations""; ""2.4 Design Tools""; ""2.5 Future Requirements""; ""2.6 Conclusions""; ""Chapter 3. Engine/Airframe Performance Matching""; ""3.1 Introduction""; ""3.2 Mission Analysis""; ""3.3 Optimization of Engine/Airplane Match""; ""3.4 Sensitivity and Influence Coefficients""; ""3.5 Computer Simulation of Gas Turbine Engines""; ""Chapter 4. Inlets and Inlet/Engine Integration""; ""4.1 Introduction"" ""4.2 Elements of a Successful Inlet/Engine Integration Program""""4.3 Definition of Subsonic Inlet/Engine Operational Requirements""; ""4.4 Definition of Supersonic Inlet/Engine Operational Requirements""; ""4.5 Engine Impact on Inlet Design""; ""4.6 Inlet Impact on Engine Design""; ""4.7 Validation of Inlet/Engine System""; ""Chapter 5. Variable Convergent-Divergent Exhaust Nozzle Aerodynamics""; ""5.1 Introduction""; ""5.2 Nozzle Concept""; ""5.3 Performance Predictions""; ""5.4 Aerodynamic Load Predictions""; ""Chapter 6. Engine Operability""; ""6.1 Introduction""; ""6.2 Definitions"" ""6.3 Stability Assessment""""6.4 Aerodynamic Interface Plane""; ""6.5 Total Pressure Distortion""; ""6.6 Total Temperature Distortion""; ""6.7 Planar Waves""; ""6.8 Recoverability""; ""6.9 Analytical Techniques""; ""6.10 Summary""; ""Chapter 7. Aeroelasticity and Unsteady Aerodynamics""; ""7.1 Introduction""; ""7.2 Overview of Turbomachinery Flutter""; ""7.3 Brief Survey of Turbomachinery Flutter Regimes""; ""7.4 Elementary Considerations of Aircraft Wing Flutter""; ""7.5 Fundamental Differences Between Turbomachinery Flutter and Wing Flutter"" ""7.6 Fundamental of Unsteady Aerodynamic Theory for Isolated Airfoils""""7.7 Unsteady Aerodynamic Theory for Cascaded Airfoils""; ""7.8 Dynamic Stall-Empiricism and Experiment""; ""7.9 Coupled Blade-Disk-Shroud Stability Theory""; ""Subject Index""; ""A""; ""B""; ""C""; ""D""; ""E""; ""F""; ""G""; ""H""; ""I""; ""K""; ""L""; ""M""; ""N""; ""O""; ""P""; ""R""; ""S""; ""T""; ""U""; ""V""; ""W"" |
| Record Nr. | UNINA-9910783936003321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1989 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft propulsion systems technology and design / / edited by Gordon C. Oates
| Aircraft propulsion systems technology and design / / edited by Gordon C. Oates |
| Edizione | [1st ed.] |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1989 |
| Descrizione fisica | 1 online resource (535 p.) |
| Disciplina | 629.134/353 |
| Altri autori (Persone) | OatesGordon C |
| Collana | AIAA education series |
| Soggetto topico | Aircraft gas-turbines |
| ISBN |
1-60086-149-0
1-60086-021-4 1-60119-206-1 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Table of Contents""; ""Chapter 1. Design and Development of Aircraft Propulsion Systems""; ""1.1 Introduction""; ""1.2 Engine Design Objectives""; ""1.3 Effect of Thermodynamic Variables on Engine Performance""; ""1.4 Development of Thrust""; ""1.5 Off-Design Performance of Gas Turbine Propulsion Engines""; ""1.6 Losses in Available Energy""; ""1.7 Interrelations Among Aerodynamic Components""; ""1.8 Interaction with Other Specialties""; ""1.9 Advanced Flow Calculations""; ""1.10 Biography of a Typical Engine""
""Chapter 2. Turbopropulsion Combustion Technology""""2.1 Introduction""; ""2.2 Combustion System Description/Definitions""; ""2.3 Component Considerations""; ""2.4 Design Tools""; ""2.5 Future Requirements""; ""2.6 Conclusions""; ""Chapter 3. Engine/Airframe Performance Matching""; ""3.1 Introduction""; ""3.2 Mission Analysis""; ""3.3 Optimization of Engine/Airplane Match""; ""3.4 Sensitivity and Influence Coefficients""; ""3.5 Computer Simulation of Gas Turbine Engines""; ""Chapter 4. Inlets and Inlet/Engine Integration""; ""4.1 Introduction"" ""4.2 Elements of a Successful Inlet/Engine Integration Program""""4.3 Definition of Subsonic Inlet/Engine Operational Requirements""; ""4.4 Definition of Supersonic Inlet/Engine Operational Requirements""; ""4.5 Engine Impact on Inlet Design""; ""4.6 Inlet Impact on Engine Design""; ""4.7 Validation of Inlet/Engine System""; ""Chapter 5. Variable Convergent-Divergent Exhaust Nozzle Aerodynamics""; ""5.1 Introduction""; ""5.2 Nozzle Concept""; ""5.3 Performance Predictions""; ""5.4 Aerodynamic Load Predictions""; ""Chapter 6. Engine Operability""; ""6.1 Introduction""; ""6.2 Definitions"" ""6.3 Stability Assessment""""6.4 Aerodynamic Interface Plane""; ""6.5 Total Pressure Distortion""; ""6.6 Total Temperature Distortion""; ""6.7 Planar Waves""; ""6.8 Recoverability""; ""6.9 Analytical Techniques""; ""6.10 Summary""; ""Chapter 7. Aeroelasticity and Unsteady Aerodynamics""; ""7.1 Introduction""; ""7.2 Overview of Turbomachinery Flutter""; ""7.3 Brief Survey of Turbomachinery Flutter Regimes""; ""7.4 Elementary Considerations of Aircraft Wing Flutter""; ""7.5 Fundamental Differences Between Turbomachinery Flutter and Wing Flutter"" ""7.6 Fundamental of Unsteady Aerodynamic Theory for Isolated Airfoils""""7.7 Unsteady Aerodynamic Theory for Cascaded Airfoils""; ""7.8 Dynamic Stall-Empiricism and Experiment""; ""7.9 Coupled Blade-Disk-Shroud Stability Theory""; ""Subject Index""; ""A""; ""B""; ""C""; ""D""; ""E""; ""F""; ""G""; ""H""; ""I""; ""K""; ""L""; ""M""; ""N""; ""O""; ""P""; ""R""; ""S""; ""T""; ""U""; ""V""; ""W"" |
| Record Nr. | UNINA-9910958783603321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1989 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||