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Aircraft landing gear design [[electronic resource] ] : principles and practices / / Norman S. Currey
| Aircraft landing gear design [[electronic resource] ] : principles and practices / / Norman S. Currey |
| Autore | Currey Norman S |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1988 |
| Descrizione fisica | x, 373 p. : ill |
| Disciplina | 629.134/381 |
| Collana | AIAA education series |
| Soggetto topico | Airplanes - Landing gear - Design and construction |
| ISBN |
1-60086-018-4
1-60119-210-X |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910783936203321 |
Currey Norman S
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| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1988 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft landing gear design [[electronic resource] ] : principles and practices / / Norman S. Currey
| Aircraft landing gear design [[electronic resource] ] : principles and practices / / Norman S. Currey |
| Autore | Currey Norman S |
| Pubbl/distr/stampa | Washington, D.C., : American Institute of Aeronautics and Astronautics, c1988 |
| Descrizione fisica | x, 373 p. : ill |
| Disciplina | 629.134/381 |
| Collana | AIAA education series |
| Soggetto topico | Airplanes - Landing gear - Design and construction |
| ISBN |
1-60086-018-4
1-60119-210-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910817541603321 |
|
Currey Norman S
|
||
| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1988 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft landing gear design: principles and practices / Norman S. Currey
| Aircraft landing gear design: principles and practices / Norman S. Currey |
| Autore | Currey, Norman S. |
| Pubbl/distr/stampa | Washington : American Institute of Aeronautics and Astronautics, 1988 |
| Descrizione fisica | X, 373 p. : ill. ; 24 cm |
| Disciplina | 629.134381 |
| Collana | AIAA Education series |
| Soggetto non controllato | Aeroplani - Atterraggio - Sistemi |
| ISBN | 0-930403-41-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-990008813650403321 |
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Currey, Norman S.
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| Washington : American Institute of Aeronautics and Astronautics, 1988 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Aircraft propulsion systems technology and design / edited by Gordon C. Oates
| Aircraft propulsion systems technology and design / edited by Gordon C. Oates |
| Pubbl/distr/stampa | Washington : American Institute of Aeronautics and Astronautics, 1989 |
| Descrizione fisica | 528 p. : ill. ; 24 cm. |
| ISBN | 09-304-0324-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNICAMPANIA-SUN0035381 |
| Washington : American Institute of Aeronautics and Astronautics, 1989 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Vanvitelli | ||
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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 / edited by Gordon C. Oates
| Aircraft propulsion systems technology and design / edited by Gordon C. Oates |
| Pubbl/distr/stampa | Washington, : American Institute of Aeronautics and Astronautics, 1989 |
| Descrizione fisica | 528 p. : ill. ; 24 cm |
| ISBN | 09-304-0324-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Titolo uniforme | |
| Record Nr. | UNICAMPANIA-VAN0035381 |
| Washington, : American Institute of Aeronautics and Astronautics, 1989 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Vanvitelli | ||
| ||
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 [[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-9910825637503321 |
| Washington, D.C., : American Institute of Aeronautics and Astronautics, c1989 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft systems : mechanical, electrical, and avionics subsystems integration / Ian Moir, Allan Seabridge
| Aircraft systems : mechanical, electrical, and avionics subsystems integration / Ian Moir, Allan Seabridge |
| Autore | Moir, I. (Ian) |
| Edizione | [3rd ed.] |
| Pubbl/distr/stampa | Reston, VA : American Institute of Aeronautics and Astronautics |
| Descrizione fisica | xxxix, 504 p. : ill. ; 26 cm. |
| Disciplina | 629.135 |
| Altri autori (Persone) | Seabridge, A. G. (Allan G.)author |
| Collana | AIAA education series |
| Soggetto topico |
Aeronautics - Systems engineering
Airplanes, Military - Design and construction Airplanes - Equipment and supplies |
| ISBN |
9781563479526 (alk. paper)
1563479524 (alk. paper) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNISALENTO-991001979109707536 |
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Moir, I. (Ian)
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| Reston, VA : American Institute of Aeronautics and Astronautics | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. del Salento | ||
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An introduction to the mathematics and methods of astrodynamics / Richard H. Battin
| An introduction to the mathematics and methods of astrodynamics / Richard H. Battin |
| Autore | Battin, Richard H. |
| Pubbl/distr/stampa | New York : American Institute of Aeronautics and Astronautics, c1987 |
| Descrizione fisica | XXXII, 796 p. ; 24 cm |
| Disciplina | 629.411 |
| Collana | AIAA Education series |
| ISBN | 0-930403-25-8 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-990008782800403321 |
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Battin, Richard H.
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| New York : American Institute of Aeronautics and Astronautics, c1987 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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