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[null,"1.","Record Nr.",null,"UNINA9910451120003321"]
[null,null,"Titolo",null,"Aircraft propulsion systems technology and design [[electronic resource] /] / edited by Gordon C. Oates"]
[null,null,"Pubbl/distr/stampa",null,"Washington, D.C., : American Institute of Aeronautics and Astronautics, c1989"]
[null,null,"ISBN",null,"1-60086-149-0"]
[{"$nulls":4},"1-60086-021-4"]
[{"$nulls":4},"1-60119-206-1"]
[null,null,"Descrizione fisica",null,"1 online resource (535 p.)"]
[null,null,"Collana",null,"AIAA education series"]
[null,null,"Disciplina",null,"629.134/353"]
[null,null,"Soggetti",null,"Aircraft gas-turbines"]
[{"$nulls":4},"Electronic books."]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Note generali","The last of three texts on aircraft propulsion technology planned by Gordon C. Oates. Other titles: Aerothermodynamics of gas turbine and rocket propulsion (c1988); Aerothermodynamics of aircraft engine components (c1985)."]
[null,null,null,"Nota di bibliografia","Includes bibliographical references and index."]
[null,null,"Nota di contenuto",null,"\"\"Cover\"\"; \"\"Title\"\"; \"\"Copyright\"\"; \"\"Foreword\"\"; \"\"Table of Contents\"\"; \"\"Chapter 1. Design and Development of Aircraft Propulsion Systems\"\"; \"\"1.1 Introduction\"\"; \"\"1.2 Engine Design Objectives\"\"; \"\"1.3 Effect of Thermodynamic Variables on Engine Performance\"\"; \"\"1.4 Development of Thrust\"\"; \"\"1.5 Off-Design Performance of Gas Turbine Propulsion Engines\"\"; \"\"1.6 Losses in Available Energy\"\"; \"\"1.7 Interrelations Among Aerodynamic Components\"\"; \"\"1.8 Interaction with Other Specialties\"\"; \"\"1.9 Advanced Flow Calculations\"\"; \"\"1.10 Biography of a Typical Engine\"\""]
[{"$nulls":4},"\"\"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\"\""]
[{"$nulls":4},"\"\"4.2 Elements of a Successful Inlet/Engine Integration Program\"\"\"\"4.3 Definition of Subsonic Inlet/Engine Operational Requirements\"\"; \"\"4.4 "]
[{"$nulls":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\"\""]
[{"$nulls":4},"\"\"6.3 Stability Assessment\"\"\"\"6.4 Aerodynamic Interface Plane\"\"; \"\"6.5 Total Pressure Distortion\"\"; \"\"6.6 Total Temperature Distortion\"\"; \"\"6.7 Planar Waves\"\"; \"\"6.8 Recoverability\"\"; \"\"6.9 Analytical Techniques\"\"; \"\"6.10 Summary\"\"; \"\"Chapter 7. Aeroelasticity and Unsteady Aerodynamics\"\"; \"\"7.1 Introduction\"\"; \"\"7.2 Overview of Turbomachinery Flutter\"\"; \"\"7.3 Brief Survey of Turbomachinery Flutter Regimes\"\"; \"\"7.4 Elementary Considerations of Aircraft Wing Flutter\"\"; \"\"7.5 Fundamental Differences Between Turbomachinery Flutter and Wing Flutter\"\""]
[{"$nulls":4},"\"\"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\"\""]