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100   $a19971218d1997      uy             0
101 0 $aeng
135   $aur|n|---|||||
181   $ctxt
182   $cc
183   $acr
200 10$aAerothermodynamics of gas turbine and rocket propulsion$b[electronic resource] /$fGordon C. Oates
205   $a3rd ed.
210   $aReston, Va. $cAmerican Institute of Aeronautics and Astronautics$dc1997
215   $a1 online resource (469 p.)
225 1 $aAIAA education series
300   $aDescription based upon print version of record.
311   $a1-56347-241-4 
320   $aIncludes bibliographical references and index.
327   $a""Cover""; ""Title""; ""Copyright""; ""Foreword""; ""Acknowledgments""; ""Table of Contents""; ""Preface""; ""Chapter 1. Introduction""; ""1.1 Purpose""; ""1.2 Chemical Rockets""; ""1.3 Nonchemical Rockets""; ""1.4 Airbreathing Engines""; ""1.5 Summary""; ""Chapter 2. Thermodynamics and Quasi-One-Dimensional Fluid Flows""; ""2.1 Introduction""; ""2.2 Definitions""; ""2.3 The Laws of Thermodynamics""; ""2.4 The Zeroth Law of Thermodynamics""; ""2.5 The First Law of Thermodynamics""; ""2.6 The Reversible Process""; ""2.7 Derived Properties: Enthalpy and Specific Heats""
327   $a""2.8 The Second Law of Thermodynamics""""2.9 The Gibbs Equation""; ""2.10 The Gibbs Function and the Helmholtz Function""; ""2.11 Maxwell's Relations""; ""2.12 General Relationships between Properties""; ""2.13 The Perfect Gas""; ""2.14 Quasi-One-Dimensional Fluid Flows""; ""2.15 The First Law for a Flowing Systema???The Control Volume""; ""2.16 The Channel Flow Equations""; ""2.17 Stagnation Properties""; ""2.18 Property Variations in Channels""; ""2.19 The Nozzle Flow Equations""; ""2.20 Numerical Solutions of Equations""; ""Problems""; ""Chapter 3. Chemical Rockets""; ""3.1 Introduction""
327   $a""3.2 Expression for the Thrust""""3.3 Acceleration of a Rocket""; ""3.4 Rocket Nozzle Performance""; ""3.5 Elementary Chemistry""; ""3.6 Determination of Chamber Conditions""; ""3.7 Nozzle Flow of a Reacting Gas""; ""3.8 Solid-Propellant Rockets""; ""Problems""; ""Chapter 4. Nonchemical Rockets""; ""4.1 Introduction""; ""4.2 The Nuclear-Heated Rocket""; ""4.3 Electrically Powered Rockets""; ""Problems""; ""Chapter 5. Ideal Cycle Analysis""; ""5.1 Introduction""; ""5.2 Notation""; ""5.3 Ideal Component Behaviors""; ""5.4 The Ideal Thermodynamic Cycle""
327   $a""5.5 The Effect of Burning at Finite Mach Number""""5.6 The Propulsive Efficiency, I?·[sub(p)]""; ""5.7 Systems of Units""; ""5.8 The Ideal Turbojet""; ""5.9 Interpretation of the Behavior of the Specific Fuel Consumption""; ""5.10 The Maximum Thrust Turbojet""; ""5.11 The Ideal Turbojet with Afterburning""; ""5.12 The Turbofan with Separate Exhaust Streams""; ""5.13 The Ideal Turbofan with Mixed Exhaust Streams""; ""5.14 The Ideal Constant-Pressure Mixer""; ""5.15 The Ideal Turbofan with Afterburning""; ""Problems""; ""Chapter 6. Component Performance""; ""6.1 Introduction""
327   $a""6.2 The Thrust Equation""""6.3 Averages""; ""6.4 The Inlet""; ""6.5 The Compressor""; ""6.6 The Burner""; ""6.7 The Turbine""; ""6.8 The Nozzle""; ""6.9 Summary of Component Figures of Merit""; ""Problems""; ""Chapter 7. Nonideal Cycle Analysis""; ""7.1 Introduction""; ""7.2 The Turbojet""; ""7.3 The Turbofan""; ""7.4 The Turboprop or Prop Fan""; ""7.5 The Effects of Nonconstant Specific Heats""; ""7.6 Summary and Conclusions""; ""Problems""; ""Chapter 8. Engine Off-Design Performance""; ""8.1 Introduction""; ""8.2 Off-Design Analysis of the Turbojet""
327   $a""8.3 Off-Design Analysis of the Turbofan""
410  0$aAIAA education series.
606   $aAerothermodynamics
606   $aAircraft gas-turbines
606   $aRocket engines
615  0$aAerothermodynamics.
615  0$aAircraft gas-turbines.
615  0$aRocket engines.
676   $a629.134/353
700   $aOates$b Gordon C$0314161
801  0$bMiAaPQ
801  1$bMiAaPQ
801  2$bMiAaPQ
906   $aBOOK
912   $a9910783934603321
996   $aAerothermodynamics of gas turbine and rocket propulsion$91422986
997   $aUNINA