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Course Information
Course Unit Title : Jet and Rocket Engines
Course Unit Code : 01MAK5144
Type of Course Unit : Optional
Level of Course Unit : Second Cycle
Year of Study : 1
Semester : 1.Semester
Number of ECTS Credits Allocated : 6,00
Name of Lecturer(s) : ---
Course Assistants :
Learning Outcomes of The Course Unit : 1.Classifications and General Performance
2.Thermodynamic Cycles
3.Jet Propulsive System Analyses
4.Combustion
Mode of Delivery : Face-To-Face
Prerequisities and Co-requisities Courses : Unavailable
Recommended Optional Programme Components : Unavailable
Course Contents : Jet propulsion principles: fluid momentum and propulsion force, rockets, turbojets, turbofans and ramjets. Aircraft Engine Thermodynamics: propulsion and efficiency, ramjets, turbojet engines, turbofan engines, turboprop and turbo shaft engines, typical engine performance, engine-aircraft matching. Inlets, Combustion Chamber and Nozzle Aerothermodynamics: Subsonic air inlets, supersonic air inlets, Gas Turbine combustion chamber, afterburners and ramjet combustion chambers, supersonic combustion chambers, exhaust nozzles. Axial compressors. Centrifugal compressors. Rocket engine.
Languages of Instruction : Turkish
Course Goals : To learn the working principles, Propulsive System Analyses and Thermodynamic of Jet Engines and Rockets
Course Aims : Primary objective of this course is to teach the student the basic principles of jet engines and propulsion and also expand students? knowledge about the general performance analyses of the aircraft engines
WorkPlacement   Not Available
Recommended or Required Reading
Textbook : 1.Mechanics and Thermodynamics of Propulsion, Hill and Peterson, 2nd Edition (1992)
Additional Resources :
Material Sharing
Documents :
Assignments :
Exams :
Additional Material :
Planned Learning Activities and Teaching Methods
Lectures, Practical Courses, Presentation, Seminar, Project, Laboratory Applications (if necessary)
ECTS / Table Of Workload (Number of ECTS credits allocated)
Student workload surveys utilized to determine ECTS credits.
Activity :
Number Duration Total  
Course Duration (Excluding Exam Week) :
14 3 42  
Time Of Studying Out Of Class :
14 4 56  
Homeworks :
2 20 40  
Presentation :
0 0 0  
Project :
0 0 0  
Lab Study :
0 0 0  
Field Study :
0 0 0  
Visas :
1 20 20  
Finals :
1 25 25  
Workload Hour (30) :
30  
Total Work Charge / Hour :
183  
Course's ECTS Credit :
6      
Assessment Methods and Criteria
Studies During Halfterm :
Number Co-Effient
Visa :
1 100
Quiz :
0 0
Homework :
0 0
Attendance :
0 0
Application :
0 0
Lab :
0 0
Project :
0 0
Workshop :
0 0
Seminary :
0 0
Field study :
0 0
   
TOTAL :
100
The ratio of the term to success :
40
The ratio of final to success :
60
TOTAL :
100
Weekly Detailed Course Content
Week Topics  
1 Classifications and General Performance
1.Propulsion force and propulsive system performances
2.Propulsive system selection
 
2 Thermodynamic Cycles

 
3 Thermodynamic Cycles

 
4 Combustion

 
5 Combustion

 
6 Mid-term Exam
 
7 Combustion

 
8 Jet Propulsive System Analyses
 
9 a) Turbojet
b) Ramjets
c) Roket
d) Turboprop and Turbo shaft
 
10 e) Turbofan
f ) Typical engine performance
 
11 g) Engine-aircraft matching
 
12 Propulsive System Components
a) Air inlets (subsonic, supersonic)
b) Combustion Chamber
 
13 Propulsive System Components
c) Afterburner
d) Exhaust nozzles
 
14 Final Exam