PME 5150-0

Brief

介紹渦輪機之理論、熱力學與流體力學之相關理論、航空器噴射引擎、進氣道、燃燒室與噴嘴。本課程之教學目標在建立渦輪機 之基本解晰能力及解決實際問題之素養，即經由基本原理之了解，建立吸氣式推進系統之分析能力，以創造工程之價值。教學內 容包括渦輪機基本原理，採用理想氣體穩態一維流體理論探討流體之動力與熱力循環分析, 進氣道,壓縮機,燃燒室,渦輪機,噴 嘴之基本原理及噴射推進基本裝置原理等。

Description

Course keywords: gas turbine, propulsion, jet engine, turbomachinery, rocket 一、課程說明(Course Description) Chapter 1. Jet Propulsion review Chapter 8. Axial Compressor Aerodynamics Chapter 9. Centrifugal Compressor Aerodynamics Chapter 10. Aerothermo-dynamics of Gas Turbines Chapter 12. Conclusion 二、指定用書(Text Books) "Aircraft Propulsion" 3rd edition, Wiley, 2020  三、參考書籍(References) 1. Zucrow, Aircraft & Missile Propulsion, J W & Sons, 1976 2. Hoffman, Gas Dynamics, J W & Sons, 1983 3. Mattingly, Elements of Gas Turbine Propulsion, McGraw-Hill, 1996 四、教學方式(Teaching Method) Lectures & Demonstrations Projects & Discussions Interactive Teaching & Learning New Technology Update 五、教學進度(Syllabus) Chapter 1. Jet Propulsion review Chapter 8. Axial Compressor Aerodynamics Chapter 9. Centrifugal Compressor Aerodynamics Chapter 10. Aerothermo-dynamics of Gas Turbines Chapter 12. Conclusion 六、成績考核(Evaluation) Homework(30%) + MidTerm(30%) + Final(40%) + Presence(5%)

Timetable

Scores

Average Percentage 84.31

Std. Deviation 9.21

Remarks

Restrictions

Compulsory

Elective

Cross Discipline

First Specialization

Second Specialization