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001442182 001__ 1442182
001442182 003__ OCoLC
001442182 005__ 20230310003316.0
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001442182 019__ $$a1265460581
001442182 020__ $$a9783030799458$$q(electronic bk.)
001442182 020__ $$a303079945X$$q(electronic bk.)
001442182 020__ $$z3030799441
001442182 020__ $$z9783030799441
001442182 0247_ $$a10.1007/978-3-030-79945-8$$2doi
001442182 035__ $$aSP(OCoLC)1265457309
001442182 040__ $$aYDX$$beng$$epn$$cYDX$$dGW5XE$$dEBLCP$$dOCLCO$$dOCLCF$$dN$T$$dOCLCQ$$dOCLCO$$dOCLCQ
001442182 049__ $$aISEA
001442182 050_4 $$aTL573
001442182 08204 $$a629.132/38$$223
001442182 1001_ $$aBabu, V.
001442182 24510 $$aFundamentals of propulsion /$$cV. Babu.
001442182 260__ $$aCham, Switzerland :$$bSpringer,$$c2022.
001442182 300__ $$a1 online resource
001442182 336__ $$atext$$btxt$$2rdacontent
001442182 337__ $$acomputer$$bc$$2rdamedia
001442182 338__ $$aonline resource$$bcr$$2rdacarrier
001442182 504__ $$aIncludes bibliographical references and index.
001442182 5050_ $$aIntro -- 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
001442182 5058_ $$a3 Basics of Turbomachinery -- 3.1 Euler's Turbomachinery Equation -- 3.2 Relationship Between the Fluid Mechanics and Thermodynamics of Turbomachinery Process -- 3.3 Blade Design Parameters -- 3.3.1 Flow and Loading Coefficients -- 3.3.2 Degree of Reaction -- 3.4 Multi-stage Turbomachines -- 4 Basics of Combustion Thermodynamics -- 4.1 Enthalpy of Formation and Sensible Enthalpy -- 4.2 Properties of Ideal Gas Mixtures -- 4.3 Combustion Stoichiometry -- 4.4 Enthalpy of Combustion and Calorific Value -- 4.5 Adiabatic Flame Temperature -- 4.6 Fuels and Their Properties
001442182 5058_ $$a4.6.1 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
001442182 5058_ $$a6.3 Operation of a Turbofan Engine -- 6.3.1 Thrust Reversing -- 7 Thrust Calculations -- 7.1 Derivation of Expression for Thrust and TSFC -- 7.1.1 Turbojet Engine -- 7.1.2 Turbofan Engine -- 7.2 Thermodynamics of an Ideal Turbojet Engine -- 7.3 Thermodynamics of an Ideal Turbojet Engine with Afterburning -- 7.4 Component Efficiencies -- 7.4.1 Inlet -- 7.4.2 Compressor -- 7.4.3 Combustor -- 7.4.4 Turbine -- 7.4.5 Nozzle -- 7.5 Calculation of Specific Thrust and TSFC for a Turbojet Engine -- 7.5.1 Specific Thrust -- 7.5.2 TSFC -- 7.6 Thermodynamics of an Ideal Turbofan Engine
001442182 5058_ $$a7.7 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
001442182 506__ $$aAccess limited to authorized users.
001442182 520__ $$aThis highly informative book offers a comprehensive overview of the fundamentals of propulsion. The book focuses on foundational topics in propulsion, namely gas dynamics, turbomachinery, and combustion to more complex subjects such as practical design aspects of aircraft engines and thermodynamic aspects and analysis. It also includes pedagogical aspects such as end-of-chapter problems and worked examples to augment learning and self-testing. This book is a useful reference for students in the area of mechanical and aerospace engineering. Also, scientists and engineers working in the areas of aerospace propulsion and gas dynamics find this book a valuable addition.
001442182 588__ $$aOnline resource; title from PDF title page (SpringerLink, viewed September 14, 2021).
001442182 650_0 $$aAerodynamics.
001442182 650_0 $$aPropulsion systems.
001442182 650_6 $$aAérodynamique.
001442182 650_6 $$aSystèmes de propulsion.
001442182 655_0 $$aElectronic books.
001442182 77608 $$iPrint version:$$z3030799441$$z9783030799441$$w(OCoLC)1253477804
001442182 852__ $$bebk
001442182 85640 $$3Springer Nature$$uhttps://univsouthin.idm.oclc.org/login?url=https://link.springer.com/10.1007/978-3-030-79945-8$$zOnline Access$$91397441.1
001442182 909CO $$ooai:library.usi.edu:1442182$$pGLOBAL_SET
001442182 980__ $$aBIB
001442182 980__ $$aEBOOK
001442182 982__ $$aEbook
001442182 983__ $$aOnline
001442182 994__ $$a92$$bISE