Fundamentals of propulsion / / V. Babu

• Autore: Babu V.
• Pubblicazione: Cham, Switzerland : , : Springer, , [2022]; ©2022
• Descrizione fisica: 1 online resource (164 pages)
• Disciplina: 629.13238
• Soggetto topico: Aerodynamics; Propulsion systems
• Note generali: Includes index.
• Nota di contenuto: 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-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. ; 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.
• Titolo autorizzato: Fundamentals of Propulsion
• ISBN: 3-030-79945-X
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910522972103321
• Lo trovi qui: Univ. Federico II