LEADER 04249nam  2200613 a 450 
001 9910783937603321
005 20230213211319.0
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(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$b[electronic resource] /$fedited by Gordon C. Oates
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   $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   $a""F""""G""; ""H""; ""I""; ""J""; ""K""; ""L""; ""M""; ""N""; ""O""; ""P""; ""R""; ""S""; ""T""; ""V""; ""W""
410  0$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   $a9910783937603321
996   $aAerothermodynamics of aircraft engine components$93779195
997   $aUNINA