Course syllabus

010023408-65 การขับดันทางการบินและอวกาศ (Aerospace Propulsions)

Course Syllabus

Data entry : Asst.Prof. Dr.Thada Suksila
1. Course number and name

010023408-65 การขับดันทางการบินและอวกาศ (Aerospace Propulsions)

2. Credits and contact hours

3(3-0-6)

3. Instructor’s or course coordinator’s name

Asst.Prof. Dr.Thada Suksila

4. Text book, title, author, and year

5. Specific course information

  1. brief description of the content of the course (catalog description)
  2. prerequisites or co-requisites
    010013321-65 Thermodynamics
    010013322-65 Fluid Mechanics
  3. indicate whether a required, elective, or selected elective (as per Table 5-1) course in the program
    Required :

6. Specific goals for the course

  1. specific outcomes of instruction (e.g. The student will be able to explain the significance of current research about a particular topic.)
  2. explicitly indicate which of the student outcomes listed in Criterion 3 or any other outcomes are addressed by the course.
    ABET Student Outcome (SO) Listed in Criterion 3 Performance indicator
    SO1 an ability to identify, formulate, and solve complex engineering problems by applying principles of engineering, science, and mathematics.
    • PI-1.1 Identifies problem and states assumptions (20%)
    • PI-1.2 Chooses an appropriate mathematical model of a system or process (20%)
    • PI-1.3 Shows solution procedure and methods (50%)
    • PI-1.4 Interprets and/or verifies the problem solution (10%)

7. Brief list of topics to be covered
Week Topic Details Activities
1 Engine types; alternatives to Air-breathing combustion engines
2 Fuels, chemical thermodynamics
3 Chemical thermodynamics
4 Basics of combustion, Pollutant formation and remediation
5 Basic operating principles, design and performance parameters Using P-V and T-s diagrams
6-8 Unsteady-flow Ideal cycle analysis (con’t) Unsteady-flow Non-ideal cycle analysis
9 Thrust and aircraft range
10-12 1D compressible flow Compressible Flow with Friction and Heat
13 Ideal performance of turbojets and turbofans (turboshaft) propellers
14 Non-ideal performance of air breathing propulsion devices
8. Course Assessment
Course assessment Weight score (%) Assessment tools Date
Quiz1 10 quiz
Quiz2 10 quiz
Midterm Exam 30 midterm examination
Final Exam 30 final examination
Project 10 Final Project
Attendance 5 Attendance
Weekly quiz 5 Weekly quiz

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