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[null,"1.","Record Nr.",null,"UNINA9910522972103321"]
[null,null,"Autore",null,"Babu V."]
[null,null,"Titolo",null,"Fundamentals of propulsion / / V. Babu"]
[null,null,"Pubbl/distr/stampa",null,"Cham, Switzerland : , : Springer, , [2022]"]
[{"$nulls":4},"©2022"]
[null,null,"ISBN",null,"3-030-79945-X"]
[null,null,"Descrizione fisica",null,"1 online resource (164 pages)"]
[null,null,"Disciplina",null,"629.13238"]
[null,null,"Soggetti",null,"Aerodynamics"]
[{"$nulls":4},"Propulsion systems"]
[null,null,"Lingua di pubblicazione",null,"Inglese"]
[null,null,"Formato",null,"Materiale a stampa"]
[null,null,null,"Livello bibliografico","Monografia"]
[null,null,null,"Note generali","Includes index."]
[null,null,"Nota di contenuto",null,"Intro -- Preface -- Contents -- About the Author -- 1 Introduction -- 1.1 Thrust -- 1.2 Modes of Thrust Generation -- 1.2.1 Propellers -- 1.2.2 Jet Engines -- 1.3 Types of Aircraft Engines -- 2 Basics of Compressible One-Dimensional Flows -- 2.1 Compressibility of Fluids -- 2.2 Compressible and Incompressible Flows -- 2.3 Perfect Gas Equation of State -- 2.4 Calorically Perfect Gas -- 2.5 Governing Equations -- 2.6 Acoustic Wave Propagation Speed -- 2.6.1 Mach Number -- 2.7 Reference States -- 2.7.1 Sonic State -- 2.7.2 Stagnation State -- 2.8 T-s Diagrams in Compressible Flows -- 3 Basics of Turbomachinery -- 3.1 Euler's Turbomachinery Equation -- 3.2 Relationship Between the Fluid Mechanics and Thermodynamics of Turbomachinery Process -- 3.3 Blade Design Parameters -- 3.3.1 Flow and Loading Coefficients -- 3.3.2 Degree of Reaction -- 3.4 Multi-stage Turbomachines -- 4 Basics of Combustion Thermodynamics -- 4.1 Enthalpy of Formation and Sensible Enthalpy -- 4.2 Properties of Ideal Gas Mixtures -- 4.3 Combustion Stoichiometry -- 4.4 Enthalpy of Combustion and Calorific Value -- 4.5 Adiabatic Flame Temperature -- 4.6 Fuels and Their Properties -- 4.6.1 Combustion Aspects of Fuels -- 5 The Turbojet Engine -- 5.1 Compressor -- 5.1.1 Nature of Compression Process -- 5.1.2 Design and Off-Design Operation -- 5.1.3 Tip Clearance Control -- 5.1.4 Materials -- 5.2 Combustor -- 5.2.1 Materials -- 5.2.2 Emissions -- 5.3 Turbine -- 5.3.1 Blade Cooling -- 5.3.2 Materials -- 5.4 Nozzle -- 5.4.1 Thrust Reversing -- 5.5 Afterburning Turbojet Engine -- 6 The Turbofan Engine -- 6.1 Concept of Bypass Engine -- 6.2 Transonic Fan Stage -- 6.2.1 Wide-"]
[{"$nulls":4},"Chord Fan Blade -- 6.2.2 Multi-spool Engine Technology -- 6.2.3 Fan Blade Material -- 6.3 Operation of a Turbofan Engine -- 6.3.1 Thrust Reversing -- 7 Thrust Calculations."]
[{"$nulls":4},"7.1 Derivation of Expression for Thrust and TSFC -- 7.1.1 Turbojet Engine -- 7.1.2 Turbofan Engine -- 7.2 Thermodynamics of an Ideal Turbojet Engine -- 7.3 Thermodynamics of an Ideal Turbojet Engine  with Afterburning -- 7.4 Component Efficiencies -- 7.4.1 Inlet -- 7.4.2 Compressor -- 7.4.3 Combustor -- 7.4.4 Turbine -- 7.4.5 Nozzle -- 7.5 Calculation of Specific Thrust and TSFC for a Turbojet Engine -- 7.5.1 Specific Thrust -- 7.5.2 TSFC -- 7.6 Thermodynamics of an Ideal Turbofan Engine -- 7.7 Component Efficiencies-Turbofan Engine -- 7.8 Calculation of Thrust and TSFC for a Twin Spool Turbofan Engine -- 7.8.1 Specific Thrust -- 7.8.2 TSFC -- 8 Ramjet and Scramjet Engine -- 8.1 Ramjet Engine -- 8.2 Supersonic Intakes -- 8.2.1 Internal Compression Intakes -- 8.2.2 External Compression Intakes -- 8.2.3 Intake Characteristic Curve -- 8.2.4 Mixed Compression Intake -- 8.2.5 Stability of Intake Operation -- 8.2.6 Axi-Symmetric (Conical) Intake -- 8.2.7 Thermodynamics of a Ramjet Engine -- 8.2.8 Thrust Calculation -- 8.3 Turboramjet Engine -- 8.4 Scramjet Engine -- 8.4.1 Operation of Scramjet Engine -- Appendix  Suggested Reading --  -- Index."]