LEADER 04554nam 2200589 a 450 001 9910825637503321 005 20230331005320.0 010 $a1-60086-149-0 010 $a1-60086-021-4 010 $a1-60119-206-1 035 $a(CKB)1000000000327136 035 $a(EBL)3111570 035 $a(SSID)ssj0000071411 035 $a(PQKBManifestationID)12006380 035 $a(PQKBTitleCode)TC0000071411 035 $a(PQKBWorkID)10091545 035 $a(PQKB)10347931 035 $a(MiAaPQ)EBC3111570 035 $a(Au-PeEL)EBL3111570 035 $a(CaPaEBR)ebr10516674 035 $a(OCoLC)922978802 035 $a(EXLCZ)991000000000327136 100 $a19890817d1989 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 00$aAircraft propulsion systems technology and design$b[electronic resource] /$fedited by Gordon C. Oates 210 $aWashington, D.C. $cAmerican Institute of Aeronautics and Astronautics$dc1989 215 $a1 online resource (535 p.) 225 1 $aAIAA education series 300 $aThe 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). 311 $a0-930403-24-X 320 $aIncludes bibliographical references and index. 327 $a""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"" 327 $a""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"" 327 $a""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"" 327 $a""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"" 327 $a""7.6 Fundamental of Unsteady Aerodynamic Theory for Isolated Airfoils""""7.7 Unsteady Aerodynamic Theory for Cascaded Airfoils""; ""7.8 Dynamic Stall-Empiricism and Experiment""; ""7.9 Coupled Blade-Disk-Shroud Stability Theory""; ""Subject Index""; ""A""; ""B""; ""C""; ""D""; ""E""; ""F""; ""G""; ""H""; ""I""; ""K""; ""L""; ""M""; ""N""; ""O""; ""P""; ""R""; ""S""; ""T""; ""U""; ""V""; ""W"" 410 0$aAIAA education series. 606 $aAircraft gas-turbines 615 0$aAircraft gas-turbines. 676 $a629.134/353 701 $aOates$b Gordon C$0314161 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910825637503321 996 $aAircraft propulsion systems technology and design$94124253 997 $aUNINA