LEADER 04575nam 2200649 a 450 001 9910972342603321 005 20240416073304.0 010 $a1-60086-133-4 010 $a1-60086-005-2 010 $a1-60119-204-5 035 $a(CKB)1000000000327104 035 $a(EBL)3111573 035 $a(SSID)ssj0000071395 035 $a(PQKBManifestationID)12006448 035 $a(PQKBTitleCode)TC0000071395 035 $a(PQKBWorkID)10090142 035 $a(PQKB)11730538 035 $a(MiAaPQ)EBC3111573 035 $a(Au-PeEL)EBL3111573 035 $a(CaPaEBR)ebr10516677 035 $a(OCoLC)922978789 035 $a(BIP)23267 035 $a(EXLCZ)991000000000327104 100 $a19850523d1985 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 00$aAerothermodynamics of aircraft engine components /$fedited by Gordon C. Oates 205 $a1st ed. 210 $aNew York, N.Y. $cAmerican Institute of Aeronautics and Astronautics$dc1985 215 $a1 online resource (559 p.) 225 1 $aAIAA education series 300 $aDescription based upon print version of record. 311 08$a0-915928-97-3 320 $aIncludes bibliographical references and index. 327 $a""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"" 327 $a""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 Systema???Technical Requirements""; ""3.6 Content of Current and Developing Design Systemsa??? The Technology Base""; ""3.7 Component and Configuration Experimental Development"" 327 $a""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 Backa???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"" 327 $a""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"" 327 $a""F""""G""; ""H""; ""I""; ""J""; ""K""; ""L""; ""M""; ""N""; ""O""; ""P""; ""R""; ""S""; ""T""; ""V""; ""W"" 330 $aBeginning with the basic principles and concepts of aeropropulsion combustion, this text goes on to explore specific processes, limitations and analytical methods as they bear on component design. The text features invited work of prominent specialists in aircraft gas turbine engines. 410 0$aAIAA education series. 606 $aAerothermodynamics 606 $aAircraft gas-turbines 615 0$aAerothermodynamics. 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 $a9910972342603321 996 $aAerothermodynamics of aircraft engine components$94472697 997 $aUNINA