04588nam 2200601 a 450 991045112000332120200520144314.01-60086-149-01-60086-021-41-60119-206-1(CKB)1000000000327136(EBL)3111570(SSID)ssj0000071411(PQKBManifestationID)12006380(PQKBTitleCode)TC0000071411(PQKBWorkID)10091545(PQKB)10347931(MiAaPQ)EBC3111570(Au-PeEL)EBL3111570(CaPaEBR)ebr10516674(OCoLC)922978802(EXLCZ)99100000000032713619890817d1989 uy 0engur|n|---|||||txtccrAircraft propulsion systems technology and design[electronic resource] /edited by Gordon C. OatesWashington, D.C. American Institute of Aeronautics and Astronauticsc19891 online resource (535 p.)AIAA education seriesThe 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).0-930403-24-X Includes bibliographical references and index.""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""AIAA education series.Aircraft gas-turbinesElectronic books.Aircraft gas-turbines.629.134/353Oates Gordon C314161MiAaPQMiAaPQMiAaPQBOOK9910451120003321Aircraft propulsion systems technology and design2167397UNINA