1. Introduction Turbine Engines (Ch. 1) – The Atmosphere2. The Aerodynamics of the Aircraft (Ch. 2) – Specific Fuel Consumption3. The Creation of Thrust in a Jet Engine (Ch. 3) – Newton’s Second Law4. Gas Turbine Principles (Ch. 4) – Diagrams of Temperature – Entropy 5. The Gas Turbine Efficiency (Ch. 4) – Thermal and Cycle Efficiency 6. The Principle and Layout of Jet Engine (Ch. 5) – Turbine Inlet Temperature7. Fluid Mechanics of Compressible Gases (Ch. 6) – Energy Equation8. Fluid Mechanics of Compressible Gases (Ch. 6) – Mass Flow per Unit Area9. Selection of Bypass Ratio (Ch. 7) – Jet Velocity and the Fan Pressure Ratio10. Selection of Bypass Ratio (Ch. 7) – Bypass Ratio for Minimum Specific Fuel Consumption11. Dynamic Scaling and Dimensional Analysis (Ch. 8) – Nondimensional Treatment of Thrust12. Turbomachinery: Compressors and Turbines (Ch. 9) – Flow Coefficient and Work Coefficient13. Turbomachinery: Compressors and Turbines (Ch. 9) – Axial Turbine and Axial Compressor14. Overview of the Civil Engine Design (Ch. 10) 15. CFM56 Engines
Turbine Engines - Week 2: Động lực học hàng không máy bay - Động tua-bin khí Tuần – The Aerodynamics of the Aircraft (Chapter 2) Động lực học hàng không máy bay Large Aircraft Sizing the Wing Lift, Drag, Fuel Consumption and Range Breguet Range Equations - Specific Fuel Consumption Selecting the Engine Thrust Engine Weight and Fuel Consumption Tài liệu học tập [1] Nicholas Cumpsty, Jet Propulsion, Cambridge University Press, 1997 Chapters [2] Bài giảng điện tử [3] Tài liệu khác Nguyễn Thiện Tống – Mobile: 0933 321 877 – Email: nguyenthientong@gmail.com Các nội dung môn học (15 tuần theo textbook) Introduction - Turbine Engines (Ch 1) – The Atmosphere The Aerodynamics of the Aircraft (Ch 2) – Specific Fuel Consumption The Creation of Thrust in a Jet Engine (Ch 3) – Newton’s Second Law Gas Turbine Principles (Ch 4) – Diagrams of Temperature – Entropy The Gas Turbine Efficiency (Ch 4) – Thermal and Cycle Efficiency The Principle and Layout of Jet Engine (Ch 5) – Turbine Inlet Temperature Fluid Mechanics of Compressible Gases (Ch 6) – Energy Equation Fluid Mechanics of Compressible Gases (Ch 6) – Mass Flow per Unit Area Selection of Bypass Ratio (Ch 7) – Jet Velocity and the Fan Pressure Ratio 10 Selection of Bypass Ratio (Ch 7) – Bypass Ratio for Minimum Specific Fuel Consumption 11 Dynamic Scaling and Dimensional Analysis (Ch 8) – Non-dimensional Treatment of Thrust 12 Turbomachinery: Compressors and Turbines (Ch 9) – Flow Coefficient and Work Coefficient 13 Turbomachinery: Compressors and Turbines (Ch 9) – Axial Turbine and Axial Compressor 14 Overview of the Civil Engine Design (Ch 10) 15 CFM56 Engines Largest Jet Engine in the world (2017) is the General Electric’s GE90-115B which has a maximum diameter of 3.4 meters It generates 115,300 pounds of thrust and is currently the biggest and most powerful turbofan engine in the world These big engines can be found on Boeing 777 models JFK Airport, New York, 2017 Large Aircraft 10 28 29 30 31 Selecting the Engine Thrust 32 33 34 Engine Weight and Fuel Consumption 35 36 37 TURBOFAN ENGINES Engine Core 38 TURBOFAN ENGINES 39 Turbine Engines - Week 2: The Aerodynamics of the Aircraft – Động thiết bị đẩy Sinh viên * Xem giảng điện tử Lecture_Week * Đọc tài liệu [1] Nicholas Cumpsty, Jet Propulsion, Cambridge University Press, 1997 Chapters & [2] Tài liệu khác E-Learning * Làm tập • Next week The Creation of Thrust in a Jet Engine (Ch 3) – Newton’s Second Law Nguyên lý lực đẩy động phản lực Nguyễn Thiện Tống 40 • Làm tập - Exercises of Chapter 41 • Làm tập - Exercises of Chapter 42 ... nội dung mơn học (15 tuần theo textbook) Introduction - Turbine Engines (Ch 1) – The Atmosphere The Aerodynamics of the Aircraft (Ch 2) – Specific Fuel Consumption The Creation of Thrust in a... Selecting the Engine Thrust 32 33 34 Engine Weight and Fuel Consumption 35 36 37 TURBOFAN ENGINES Engine Core 38 TURBOFAN ENGINES 39 Turbine Engines - Week 2: The Aerodynamics of the Aircraft – Động. .. considered practical to make the wing much higher off the ground than current aircraft like the 747-400, since to so would raise the cabin and if the cabin were raised higher, the existing passenger