Cargando…
Aircraft propulsion /
"Aircraft Propulsion, Second Edition is a comprehensive textbook covering aircraft gas turbine engine and rocket propulsion from the basic principles to more advanced treatments in engine components"--
| Clasificación: | Libro Electrónico |
|---|---|
| Autor principal: | |
| Formato: | Electrónico eBook |
| Idioma: | Inglés |
| Publicado: |
Chichester, West Sussex, United Kingdom :
Wiley,
2014.
|
| Edición: | Second edition. |
| Temas: | |
| Acceso en línea: | Texto completo (Requiere registro previo con correo institucional) |
MARC
| LEADER | 00000cam a2200000 i 4500 | ||
|---|---|---|---|
| 001 | OR_ocn869066578 | ||
| 003 | OCoLC | ||
| 005 | 20231017213018.0 | ||
| 006 | m o d | ||
| 007 | cr ||||||||||| | ||
| 008 | 140123s2014 enk ob 001 0 eng | ||
| 010 | |a 2014002860 | ||
| 040 | |a DLC |b eng |e rda |e pn |c DLC |d YDX |d N$T |d IDEBK |d CDX |d E7B |d COO |d YDXCP |d OCLCF |d TEFOD |d RECBK |d UMI |d DEBBG |d DEBSZ |d TEFOD |d EBLCP |d UAB |d MERER |d OCLCQ |d STF |d OCLCQ |d CEF |d RRP |d ZCU |d INT |d VT2 |d AU@ |d OCLCQ |d WYU |d OCLCQ |d UWW |d OCLCQ |d UKAHL |d CNCEN |d BWN |d S2H |d OCLCQ |d MM9 |d OCLCO |d OCLCQ |d OCLCO |d OCLCQ |d OCLCO | ||
| 066 | |c (S | ||
| 019 | |a 883319798 |a 906040857 |a 927508948 |a 961593123 |a 962633683 |a 1007238458 |a 1087284519 |a 1105798922 |a 1117097723 |a 1148156300 | ||
| 020 | |a 9781118806760 |q (ePub) | ||
| 020 | |a 111880676X |q (ePub) | ||
| 020 | |a 9781118806753 |q (Adobe PDF) | ||
| 020 | |a 1118806751 |q (Adobe PDF) | ||
| 020 | |z 9781118806777 |q (hardback) | ||
| 020 | |z 1118806778 | ||
| 020 | |z 9781306550673 | ||
| 020 | |z 130655067X | ||
| 020 | |a 9781523109951 |q (electronic) | ||
| 020 | |a 1523109955 | ||
| 024 | 8 | |a 9781118806760 | |
| 028 | 0 | 1 | |a EB00316113 |b Recorded Books |
| 029 | 1 | |a DEBBG |b BV042682942 | |
| 029 | 1 | |a DEBSZ |b 443427291 | |
| 029 | 1 | |a DEBSZ |b 446581437 | |
| 029 | 1 | |a AU@ |b 000052441605 | |
| 029 | 1 | |a AU@ |b 000067100950 | |
| 035 | |a (OCoLC)869066578 |z (OCoLC)883319798 |z (OCoLC)906040857 |z (OCoLC)927508948 |z (OCoLC)961593123 |z (OCoLC)962633683 |z (OCoLC)1007238458 |z (OCoLC)1087284519 |z (OCoLC)1105798922 |z (OCoLC)1117097723 |z (OCoLC)1148156300 | ||
| 037 | |a 77C2D20D-4BE9-407A-9489-A3E149C57867 |b OverDrive, Inc. |n http://www.overdrive.com | ||
| 042 | |a pcc | ||
| 050 | 0 | 0 | |a TL709 |
| 072 | 7 | |a TEC |x 009000 |2 bisacsh | |
| 082 | 0 | 0 | |a 629.134/35 |2 23 |
| 084 | |a TEC002000 |2 bisacsh | ||
| 049 | |a UAMI | ||
| 100 | 1 | |a Farokhi, Saeed. | |
| 245 | 1 | 0 | |a Aircraft propulsion / |c Saeed Farokhi. |
| 250 | |a Second edition. | ||
| 264 | 1 | |a Chichester, West Sussex, United Kingdom : |b Wiley, |c 2014. | |
| 300 | |a 1 online resource | ||
| 336 | |a text |b txt |2 rdacontent | ||
| 337 | |a computer |b c |2 rdamedia | ||
| 338 | |a online resource |b cr |2 rdacarrier | ||
| 347 | |a text file | ||
| 520 | |a "Aircraft Propulsion, Second Edition is a comprehensive textbook covering aircraft gas turbine engine and rocket propulsion from the basic principles to more advanced treatments in engine components"-- |c Provided by publisher | ||
| 504 | |a Includes bibliographical references and index. | ||
| 588 | 0 | |a Print version record and CIP data provided by publisher. | |
| 505 | 0 | |6 880-01 |a Aircraft Propulsion; Table of Contents; Preface to the Second Edition; Acknowledgments; Preface; Intended Audience; Motivation; Mathematical Level; Chapter Organization and Topical Coverage; Instructor Resources; Acknowledgments; Nomenclature; 1 Introduction; 1.1 History of the Airbreathing Jet Engine, a Twentieth-Century Invention-The Beginning; 1.2 Innovations in Aircraft Gas Turbine Engines; 1.2.1 Multispool Configuration; 1.2.2 Variable Stator; 1.2.3 Transonic Compressor; 1.2.4 Low-Emission Combustor; 1.2.5 Turbine Cooling; 1.2.6 Exhaust Nozzles. | |
| 505 | 8 | |a 1.2.7 Modern Materials and Manufacturing Techniques1.3 New Engine Concepts; 1.3.1 Advanced Turboprop (ATP) and Geared Turbofan (GTF); 1.3.2 Advanced Airbreathing Rocket Technology; 1.3.3 Wave Rotor Topping Cycle; 1.3.4 Pulse Detonation Engine (PDE); 1.3.5 Millimeter-Scale Gas Turbine Engines: Triumph of MEMS and Digital Fabrication; 1.3.6 Combined Cycle Propulsion: Engines from Takeoff to Space; 1.4 New Vehicles; 1.5 Summary; 1.6 Roadmap for the Second Edition; References; Problems; 2 Compressible Flow with Friction and Heat: A Review; 2.1 Introduction; 2.2 A Brief Review of Thermodynamics. | |
| 505 | 8 | |a 2.3 Isentropic Process and Isentropic Flow2.4 Conservation Principles for Systems and Control Volumes; 2.5 Speed of Sound & Mach Number; 2.6 Stagnation State; 2.7 Quasi-One-Dimensional Flow; 2.8 Area-Mach Number Relationship; 2.9 Sonic Throat; 2.10 Waves in Supersonic Flow; 2.11 Normal Shocks; 2.12 Oblique Shocks; 2.13 Conical Shocks; 2.14 Expansion Waves; 2.15 Frictionless, Constant-Area Duct Flow with Heat Transfer; 2.16 Adiabatic Flow of a Calorically Perfect Gas in a Constant-Area Duct with Friction; 2.17 Friction (Drag) Coefficient Cf and D'Arcy Friction Factor fD. | |
| 505 | 8 | |a 2.18 Dimensionless Parameters2.19 Fluid Impulse; 2.20 Summary of Fluid Impulse; References; Problems; 3 Engine Thrust and Performance Parameters; 3.1 Introduction; 3.1.1 Takeoff Thrust; 3.2 Installed Thrust-Some Bookkeeping Issues on Thrust and Drag; 3.3 Engine Thrust Based on the Sum of Component Impulse; 3.4 Rocket Thrust; 3.5 Airbreathing Engine Performance Parameters; 3.5.1 Specific Thrust; 3.5.2 Specific Fuel Consumption and Specific Impulse; 3.5.3 Thermal Efficiency; 3.5.4 Propulsive Efficiency; 3.5.5 Engine Overall Efficiency and Its Impact on Aircraft Range and Endurance. | |
| 505 | 8 | |a 3.6 Modern Engines, Their Architecture and Some Performance Characteristics3.7 Summary; References; Problems; 4 Gas Turbine Engine Cycle Analysis; 4.1 Introduction; 4.2 The Gas Generator; 4.3 Aircraft Gas Turbine Engines; 4.3.1 The Turbojet Engine; 4.3.2 The Turbojet Engine with an Afterburner; 4.3.3 The Turbofan Engine; 4.3.4 Ultra-High Bypass (UHB) Turbofan Engines; 4.4 Analysis of a Mixed-Exhaust Turbofan Engine with an Afterburner; 4.4.1 Mixer; 4.4.2 Cycle Analysis; 4.5 The Turboprop Engine; 4.5.1 Introduction; 4.5.2 Propeller Theory; 4.5.3 Turboprop Cycle Analysis; 4.6 Summary. | |
| 542 | |f Copyright © John Wiley & Sons | ||
| 590 | |a O'Reilly |b O'Reilly Online Learning: Academic/Public Library Edition | ||
| 650 | 0 | |a Airplanes |x Jet propulsion. | |
| 650 | 0 | |a Airplanes |x Motors |x Design and construction. | |
| 650 | 6 | |a Avions |x Propulsion par réaction. | |
| 650 | 7 | |a TECHNOLOGY & ENGINEERING |x Aeronautics & Astronautics. |2 bisacsh | |
| 650 | 7 | |a Airplanes |x Jet propulsion |2 fast | |
| 650 | 7 | |a Airplanes |x Motors |x Design and construction |2 fast | |
| 776 | 0 | 8 | |i Print version: |a Farokhi, Saeed. |t Aircraft propulsion. |b Second edition. |d Chichester, West Sussex, United Kingdom : Wiley, 2014 |z 9781118806777 |w (DLC) 2014001461 |
| 856 | 4 | 0 | |u https://learning.oreilly.com/library/view/~/9781118806760/?ar |z Texto completo (Requiere registro previo con correo institucional) |
| 880 | 0 | 0 | |6 505-00/(S |g Machine generated contents note: |g 1. |t Introduction -- |g 1.1. |t History of the Airbreathing Jet Engine, a Twentieth-Century Invention---The Beginning -- |g 1.2. |t Innovations in Aircraft Gas Turbine Engines -- |g 1.2.1. |t Multispool Configuration -- |g 1.2.2. |t Variable Stator -- |g 1.2.3. |t Transonic Compressor -- |g 1.2.4. |t Low-Emission Combustor -- |g 1.2.5. |t Turbine Cooling -- |g 1.2.6. |t Exhaust Nozzles -- |g 1.2.7. |t Modern Materials and Manufacturing Techniques -- |g 1.3. |t New Engine Concepts -- |g 1.3.1. |t Advanced Turboprop (ATP) and Geared Turbofan (GTF) -- |g 1.3.2. |t Advanced Airbreathing Rocket Technology -- |g 1.3.3. |t Wave Rotor Topping Cycle -- |g 1.3.3.1. |t Humphrey Cycle versus Brayton Cycle -- |g 1.3.4. |t Pulse Detonation Engine (PDE) -- |g 1.3.5. |t Millimeter-Scale Gas Turbine Engines: Triumph of MEMS and Digital Fabrication -- |g 1.3.6. |t Combined Cycle Propulsion: Engines from Takeoff to Space -- |g 1.4. |t New Vehicles -- |g 1.5. |t Summary -- |g 1.6. |t Roadmap for the Second Edition -- |t References -- |t Problems -- |g 2. |t Compressible Flow with Friction and Heat: A Review -- |g 2.1. |t Introduction -- |g 2.2. |t Brief Review of Thermodynamics -- |g 2.3. |t Isentropic Process and Isentropic Flow -- |g 2.4. |t Conservation Principles for Systems and Control Volumes -- |g 2.5. |t Speed of Sound & Mach Number -- |g 2.6. |t Stagnation State -- |g 2.7. |t Quasi-One-Dimensional Flow -- |g 2.8. |t Area--Mach Number Relationship -- |g 2.9. |t Sonic Throat -- |g 2.10. |t Waves in Supersonic Flow -- |g 2.11. |t Normal Shocks -- |g 2.12. |t Oblique Shocks -- |g 2.13. |t Conical Shocks -- |g 2.14. |t Expansion Waves -- |g 2.15. |t Frictionless, Constant-Area Duct Flow with Heat Transfer -- |g 2.16. |t Adiabatic Flow of a Calorically Perfect Gas in a Constant-Area Duct with Friction -- |g 2.17. |t Friction (Drag) Coefficient Cf and D'Arcy Friction Factor fD -- |g 2.18. |t Dimensionless Parameters -- |g 2.19. |t Fluid Impulse -- |g 2.20. |t Summary of Fluid Impulse -- |t References -- |t Problems -- |g 3. |t Engine Thrust and Performance Parameters -- |g 3.1. |t Introduction -- |g 3.1.1. |t Takeoff Thrust -- |g 3.2. |t Installed Thrust---Some Bookkeeping Issues on Thrust and Drag -- |g 3.3. |t Engine Thrust Based on the Sum of Component Impulse -- |g 3.4. |t Rocket Thrust -- |g 3.5. |t Airbreathing Engine Performance Parameters -- |g 3.5.1. |t Specific Thrust -- |g 3.5.2. |t Specific Fuel Consumption and Specific Impulse -- |g 3.5.3. |t Thermal Efficiency -- |g 3.5.4. |t Propulsive Efficiency -- |g 3.5.5. |t Engine Overall Efficiency and Its Impact on Aircraft Range and Endurance -- |g 3.6. |t Modern Engines, Their Architecture and Some Performance Characteristics -- |g 3.7. |t Summary -- |t References -- |t Problems -- |g 4. |t Gas Turbine Engine Cycle Analysis -- |g 4.1. |t Introduction -- |g 4.2. |t Gas Generator -- |g 4.3. |t Aircraft Gas Turbine Engines -- |g 4.3.1. |t Turbojet Engine -- |g 4.3.1.1. |t Inlet -- |g 4.3.1.2. |t Compressor -- |g 4.3.1.3. |t Burner -- |g 4.3.1.4. |t Turbine -- |g 4.3.1.5. |t Nozzle -- |g 4.3.1.6. |t Thermal Efficiency of a Turbojet Engine -- |g 4.3.1.7. |t Propulsive Efficiency of a Turbojet Engine -- |g 4.3.1.8. |t Overall Efficiency of a Turbojet Engine -- |g 4.3.1.9. |t Performance Evaluation of a Turbojet Engine -- |g 4.3.2. |t Turbojet Engine with an Afterburner -- |g 4.3.2.1. |t Introduction -- |g 4.3.2.2. |t Analysis -- |g 4.3.2.3. |t Optimum Compressor Pressure Ratio for Maximum (Ideal) Thrust Turbojet Engine with Afterburner -- |g 4.3.3. |t Turbofan Engine -- |g 4.3.3.1. |t Introduction -- |g 4.3.3.2. |t Analysis of a Separate-Exhaust Turbofan Engine -- |g 4.3.3.3. |t Thermal Efficiency of a Turbofan Engine -- |g 4.3.3.4. |t Propulsive Efficiency of a Turbofan Engine -- |g 4.3.4. |t Ultra-High Bypass (UHB) Turbofan Engines -- |g 4.4. |t Analysis of a Mixed-Exhaust Turbofan Engine with an Afterburner -- |g 4.4.1. |t Mixer -- |g 4.4.2. |t Cycle Analysis -- |g 4.4.2.1. |t Solution Procedure -- |g 4.5. |t Turboprop Engine -- |g 4.5.1. |t Introduction -- |g 4.5.2. |t Propeller Theory -- |g 4.5.2.1. |t Momentum Theory -- |g 4.5.2.2. |t Blade Element Theory -- |g 4.5.3. |t Turboprop Cycle Analysis -- |g 4.5.3.1. |t New Parameters -- |g 4.5.3.2. |t Design Point Analysis -- |g 4.5.3.3. |t Optimum Power Split Between the Propeller and the Jet -- |g 4.6. |t Summary -- |t References -- |t Problems -- |g 5. |t General Aviation and Uninhabited Aerial Vehicle Propulsion System -- |g 5.1. |t Introduction -- |g 5.2. |t Cycle Analysis -- |g 5.2.1. |t Otto Cycle -- |g 5.2.2. |t Real Engine Cycles -- |g 5.2.2.1. |t Four-Stroke Cycle Engines -- |g 5.2.2.2. |t Diesel Engines -- |g 5.2.2.3. |t Two-Stroke Cycle Engines -- |g 5.2.2.4. |t Rotary (Wankel) Engines -- |g 5.3. |t Power and Efficiency -- |g 5.4. |t Engine Components and Classifications -- |g 5.4.1. |t Engine Components -- |g 5.4.2. |t Reciprocating Engine Classifications -- |g 5.4.2.1. |t Classification by Cylinder Arrangement -- |g 5.4.2.2. |t Classification by Cooling Arrangement -- |g 5.4.2.3. |t Classification by Operating Cycle -- |g 5.4.2.4. |t Classification by Ignition Type -- |g 5.5. |t Scaling of Aircraft Reciprocating Engines -- |g 5.5.1. |t Scaling of Aircraft Diesel Engines -- |g 5.6. |t Aircraft Engine Systems -- |g 5.6.1. |t Aviation Fuels and Engine Knock -- |g 5.6.2. |t Carburetion and Fuel Injection Systems -- |g 5.6.2.1. |t Float-Type Carburetors -- |g 5.6.2.2. |t Pressure Injection Carburetors -- |g 5.6.2.3. |t Fuel Injection Systems -- |g 5.6.2.4. |t Full Authority Digital Engine Control (FADEC) -- |g 5.6.3. |t Ignition Systems -- |g 5.6.3.1. |t Battery Ignition Systems -- |g 5.6.3.2. |t High Tension Ignition System -- |g 5.6.3.3. |t Low Tension Ignition System -- |g 5.6.3.4. |t Full Authority Digital Engine Control (FADEC) -- |g 5.6.3.5. |t Ignition Boosters -- |g 5.6.3.6. |t Spark Plugs -- |g 5.6.4. |t Lubrication Systems -- |g 5.6.5. |t Supercharging -- |g 5.7. |t Electric Engines -- |g 5.7.1. |t Electric Motors -- |g 5.7.2. |t Solar cells -- |g 5.7.3. |t Advanced Batteries -- |g 5.7.4. |t Fuel cells -- |g 5.7.5. |t State of the Art for Electric Propulsion -- Future Technology -- |g 5.8. |t Propellers and Reduction Gears -- |t References -- |t Problems -- |g 6. |t Aircraft Engine Inlets and Nozzles -- |g 6.1. |t Introduction -- |g 6.2. |t Flight Mach Number and Its Impact on Inlet Duct Geometry -- |g 6.3. |t Diffusers -- |g 6.4. |t Ideal Diffuser -- |g 6.5. |t Real Diffusers and Their Stall Characteristics -- |g 6.6. |t Subsonic Diffuser Performance -- |g 6.7. |t Subsonic Cruise Inlet -- |g 6.8. |t Transition Ducts -- |g 6.9. |t Interim Summary for Subsonic Inlets -- |g 6.10. |t Supersonic Inlets -- |g 6.10.1. |t Isentropic Convergent--Divergent Inlets -- |g 6.10.2. |t Methods to Start a Supersonic Convergent--Divergent Inlet -- |g 6.10.2.1. |t Overspeeding -- |g 6.10.2.2. |t Kantrowitz--Donaldson Inlet -- |g 6.10.2.3. |t Variable-Throat Isentropic C--D Inlet -- |g 6.11. |t Normal Shock Inlets -- |g 6.12. |t External Compression Inlets -- |g 6.12.1. |t Optimum Ramp Angles -- |g 6.12.2. |t Design and Off-Design Operation -- |g 6.13. |t Variable Geometry---External Compression Inlets -- |g 6.13.1. |t Variable Ramps -- |g 6.14. |t Mixed-Compression Inlets -- |g 6.15. |t Supersonic Inlet Types and Their Performance---A Review -- |g 6.16. |t Standards for Supersonic Inlet Recovery -- |g 6.17. |t Exhaust Nozzle -- |g 6.18. |t Gross Thrust -- |g 6.19. |t Nozzle Adiabatic Efficiency -- |g 6.20. |t Nozzle Total Pressure Ratio -- |g 6.21. |t Nozzle Pressure Ratio (NPR) and Critical Nozzle Pressure Ratio (NPRcrit.) -- |g 6.22. |t Relation Between Nozzle Figures of Merit, ηn and πn -- |g 6.23. |t Convergent Nozzle or a De Laval-- |g 6.24. |t Effect of Boundary Layer Formation on Nozzle Internal Performance -- |g 6.25. |t Nozzle Exit Flow Velocity Coefficient -- |g 6.26. |t Effect of Flow Angularity on Gross Thrust -- |g 6.27. |t Nozzle Gross Thrust Coefficient Cfg -- |g 6.28. |t Overexpanded Nozzle Flow---Shock Losses -- |g 6.29. |t Nozzle Area Scheduling, A8 and A9/A8 -- |g 6.30. |t Nozzle Exit Area Scheduling, A9/A8 -- |g 6.31. |t Nozzle Cooling -- |g 6.32. |t Thrust Reverser and Thrust Vectoring -- |g 6.33. |t Hypersonic Nozzle -- |g 6.34. |t Exhaust Mixer and Gross Thrust Gain in a Mixed-Flow Turbofan Engine -- |g 6.35. |t Noise -- |g 6.35.1. |t Jet Noise -- |g 6.35.2. |t Chevron Nozzle -- |g 6.36. |t Nozzle-Turbine (Structural) Integration -- |g 6.37. |t Summary of Exhaust Systems -- |t References -- |t Problems -- |g 7. |t Combustion Chambers and Afterburners -- |g 7.1. |t Introduction -- |g 7.2. |t Laws Governing Mixture of Gases -- |g 7.3. |t Chemical Reaction and Flame Temperature -- |g 7.4. |t Chemical Equilibrium and Chemical Composition -- |g 7.4.1. |t Law of Mass Action -- |g 7.4.2. |t Equilibrium Constant KP -- |g 7.5. |t Chemical Kinetics -- |g 7.5.1. |t Ignition and Relight Envelope -- |g 7.5.2. |t Reaction Timescale -- |g 7.5.3. |t Flammability Limits -- |g 7.5.4. |t Flame Speed -- |g 7.5.5. |t Flame Stability -- |g 7.5.6. |t Spontaneous Ignition Delay Time -- |g 7.5.7. |t Combustion-Generated Pollutants -- |g 7.6. |t Combustion Chamber |
| 880 | 0 | 0 | |t -- |g 7.6.1. |t Combustion Chamber Total Pressure Loss -- |g 7.6.2. |t Combustor Flow Pattern and Temperature Profile -- |g 7.6.3. |t Combustor Liner and Its Cooling Methods -- |g 7.6.4. |t Combustion Efficiency -- |g 7.6.5. |t Some Combustor Sizing and Scaling Laws -- |g 7.6.6. |t Afterburner -- |g 7.7. |t Combustion-Generated Pollutants -- |g 7.7.1. |t Greenhouse Gases, CO2 and H2O -- |g 7.7.2. |t Carbon Monoxide, CO, and Unburned Hydrocarbons, UHC -- |g 7.7.3. |t Oxides of Nitrogen, NO and NO2 -- |g 7.7.4. |t Smoke -- |g 7.7.5. |t Engine Emission Standards -- |g 7.7.6. |t Low-Emission Combustors -- |g 7.7.7. |t Impact of NO on the Ozone Layer -- |g 7.8. |t Aviation Fuels -- |g 7.9. |t Alternative "Drop-In" Jet Fuels (AJFs) -- |g 7.10. |t Combustion Instability: Screech and Rumble -- |g 7.10.1. |t Screech Damper -- |g 7.11. |t Summary -- |t References -- |t Problems -- |g 8. |t Axial Compressor Aerodynamics -- |g 8.1. |t Introduction -- |g 8.2. |t Geometry -- |g 8.3. |t Rotor and Stator Frames of Reference -- |g 8.4. |t Euler Turbine Equation -- |g 8.5. |t Axial-Flow Versus Radial-Flow Machines -- |g 8.6. |t Axial-Flow Compressors and Fans -- |g 8.6.1. |t Definition of Flow Angles -- |g 8.6.2. |t Stage Parameters -- |g 8.6.3. |t Cascade Aerodynamics -- |g 8.6.4. |t Aerodynamic Forces on Compressor Blades -- |g 8.6.5. |t Three-Dimensional Flow -- |g 8.6.5.1. |t Blade Vortex Design. |
| 880 | 0 | 0 | |6 505-01/(S |g Contents note continued: |g 8.6.5.2. |t Three-Dimensional Losses -- |g 8.6.5.3. |t Reynolds Number Effect -- |g 8.7. |t Compressor Performance Map -- |g 8.8. |t Compressor Instability -- Stall and Surge -- |g 8.9. |t Multistage Compressors and Their Operating Line -- |g 8.10. |t Multistage Compressor Stalling Pressure Rise and Stall Margin -- |g 8.11. |t Multistage Compressor Starting Problem -- |g 8.12. |t Effect of Inlet Flow Condition on Compressor Performance -- |g 8.13. |t Isometric and Cutaway Views of Axial-Flow Compressor Hardware -- |g 8.14. |t Compressor Design Parameters and Principles -- |g 8.14.1. |t Blade Design -- Blade Selection -- |g 8.14.2. |t Compressor Annulus Design -- |g 8.14.3. |t Compressor Stall Margin -- |g 8.15. |t Summary -- |t References -- |t Problems -- |g 9. |t Centrifugal Compressor Aerodynamics -- |g 9.1. |t Introduction -- |g 9.2. |t Centrifugal Compressors -- |g 9.3. |t Radial Diffuser -- |g 9.4. |t Inducer -- |g 9.5. |t Inlet Guide Vanes (IGVs) and Inducer-Less Impellers -- |g 9.6. |t Impeller Exit Flow and Blockage Effects -- |g 9.7. |t Efficiency and Performance -- |g 9.8. |t Summary -- |t References -- |t Problems -- |g 10. |t Aerothermo-dynamics of Gas Turbines -- |g 10.1. |t Introduction -- |g 10.2. |t Axial-Flow Turbines -- |g 10.2.1. |t Optimal Nozzle Exit Swirl Mach Number Mθ2 -- |g 10.2.2. |t Turbine Blade Losses -- |g 10.2.2.1. |t Blade Profile Loss -- |g 10.2.2.2. |t Secondary Flow Losses -- |g 10.2.2.3. |t Annulus Losses -- |g 10.2.3. |t Optimum Solidity -- |g 10.2.4. |t Turbine Cooling -- |g 10.2.4.1. |t Convective Cooling -- |g 10.2.4.2. |t Impingement Cooling -- |g 10.2.4.3. |t Film Cooling -- |g 10.2.4.4. |t Transpiration Cooling -- |g 10.3. |t Turbine Performance Map -- |g 10.4. |t Effect of Cooling on Turbine Efficiency -- |g 10.5. |t Turbine Blade Profile Design -- |g 10.5.1. |t Angles -- |g 10.5.2. |t Other Blade Geometrical Parameters -- |g 10.5.3. |t Throat Sizing -- |g 10.5.4. |t Throat Reynolds Number Reo -- |g 10.5.5. |t Turbine Blade Profile Design -- |g 10.5.6. |t Blade Vibration and Campbell Diagram -- |g 10.5.7. |t Turbine Blade and Disk Material Selection and Design Criteria -- |g 10.6. |t Stresses in Turbine Blades and Disks and Useful Life Estimation -- |g 10.7. |t Axial-Flow Turbine Design and Practices -- |g 10.8. |t Gas Turbine Design Summary -- |g 10.9. |t Summary -- |t References -- |t Problems -- |g 11. |t Aircraft Engine Component Matching and Off-Design Analysis -- |g 11.1. |t Introduction -- |g 11.2. |t Engine (Steady-State) Component Matching -- |g 11.2.1. |t Engine Corrected Parameters -- |g 11.2.2. |t Inlet-Compressor Matching -- |g 11.2.3. |t Compressor--Combustor Matching -- |g 11.2.4. |t Combustor--Turbine Matching -- |g 11.2.5. |t Compressor--Turbine Matching and Gas Generator Pumping Characteristics -- |g 11.2.5.1. |t Gas Generator Pumping Characteristics -- |g 11.2.6. |t Turbine--Afterburner--(Variable-Geometry) Nozzle Matching -- |g 11.2.6.1. |t Fixed-Geometry Convergent Nozzle Matching -- |g 11.3. |t Engine Off-Design Analysis -- |g 11.3.1. |t Off-Design Analysis of a Turbojet Engine -- |g 11.3.2. |t Off-Design Analysis of an Afterburning Turbojet Engine -- |g 11.3.3. |t Off-Design Analysis of a Separate-Flow Turbofan (Two-Spool) Engine -- |g 11.4. |t Unchoked Nozzles and Other Off-Design Iteration Strategies -- |g 11.4.1. |t Unchoked Exhaust Nozzle -- |g 11.4.2. |t Unchoked Turbine Nozzle -- |g 11.4.3. |t Turbine Efficiency at Off-Design -- |g 11.4.4. |t Variable Gas Properties -- |g 11.5. |t Principles of Engine Performance Testing -- |g 11.5.1. |t Force of Inlet Bellmouth on Engine Thrust Stand -- |g 11.5.1.1. |t Bellmouth Instrumentation -- |g 11.5.1.2. |t Effect of Fluid Viscosity -- |g 11.5.1.3. |t Force of Inlet Bellmouth on Engine Thrust Stand -- |g 11.6. |t Summary -- |t References -- |t Problems -- |g 12. |t Chemical Rocket and Hypersonic Propulsion -- |g 12.1. |t Introduction -- |g 12.2. |t From Takeoff to Earth Orbit -- |g 12.3. |t Chemical Rockets -- |g 12.4. |t Chemical Rocket Applications -- |g 12.4.1. |t Launch Engines -- |g 12.4.2. |t Boost Engines -- |g 12.4.3. |t Space Maneuver Engines -- |g 12.4.4. |t Attitude Control Rockets -- |g 12.5. |t New Parameters in Rocket Propulsion -- |g 12.6. |t Thrust Coefficient, CF -- |g 12.7. |t Characteristic Velocity -- |g 12.8. |t Flight Performance -- |g 12.9. |t Multistage Rockets -- |g 12.10. |t Propulsive and Overall Efficiencies -- |g 12.11. |t Chemical Rocket Combustion Chamber -- |g 12.11.1. |t Liquid Propellant Combustion Chambers -- |g 12.11.1.1. |t Some Design Guidelines for Injector Plate -- |g 12.11.1.2. |t Combustion Instabilities -- |g 12.11.2. |t Solid Propellant Combustion Chambers -- |g 12.12. |t Thrust Chamber Cooling -- |g 12.12.1. |t Liquid Propellant Thrust Chambers -- |g 12.12.2. |t Cooling of Solid Propellant Thrust Chambers -- |g 12.13. |t Combustor Volume and Shape -- |g 12.14. |t Rocket Nozzles -- |g 12.14.1. |t Multiphase Flow in Rocket Nozzles -- |g 12.14.2. |t Flow Expansion in Rocket Nozzles -- |g 12.14.3. |t Thrust Vectoring Nozzles -- |g 12.15. |t High-Speed Airbreathing Engines -- |g 12.15.1. |t Supersonic Combustion Ramjet -- |g 12.15.1.1. |t Inlet Analysis -- |g 12.15.1.2. |t Scramjet Combustor -- |g 12.15.1.3. |t Scramjet Nozzle -- |g 12.16. |t Rocket-Based Airbreathing Propulsion -- |g 12.17. |t Summary -- |t References -- |t Problems. |
| 938 | |a Askews and Holts Library Services |b ASKH |n AH26311672 | ||
| 938 | |a Askews and Holts Library Services |b ASKH |n AH26311668 | ||
| 938 | |a Coutts Information Services |b COUT |n 27950580 | ||
| 938 | |a ProQuest Ebook Central |b EBLB |n EBL4038818 | ||
| 938 | |a ebrary |b EBRY |n ebr10855747 | ||
| 938 | |a EBSCOhost |b EBSC |n 746952 | ||
| 938 | |a ProQuest MyiLibrary Digital eBook Collection |b IDEB |n cis27950580 | ||
| 938 | |a Recorded Books, LLC |b RECE |n rbeEB00316113 | ||
| 938 | |a YBP Library Services |b YANK |n 12673375 | ||
| 938 | |a YBP Library Services |b YANK |n 11723965 | ||
| 994 | |a 92 |b IZTAP | ||