Thermodynamics for Aeronautical Engineering (3130109)  

5
Credit
4 + 1 + 0
Lect + Tuto + Pract
Teaching Scheme
70 + 30 + 0
ESE + PA + ALA
Theory Marks
30 + 0 + 20
ESE + OEP + PA
Practical Marks
ESE - End Semester Examination, PA - Progress Assessment, ALA - Active Learning Assignments, OEP -Open Ended Problem


Prerequisite
Basics of Mechanical Engineering
Rationale
This subject provides an in depth understanding of various thermodynamic processes involved and concepts of energy transfer and conversion in aircraft engine components and other heat exchange applications.
Course Outcome
 Sr.   No.  CO statement  Marks %   weightage
 CO-1 To identify the unique vocabulary associated with thermodynamics and explain the basic concepts of thermodynamics  5
 CO-2 To state and apply first law of thermodynamics for closed and open systems undergoing different thermodynamic processes and evaluate the feasibility of thermodynamic cycles and processes using second law of thermodynamics and concept of entropy 25
 CO-3  To analyze different gas power and vapour power cycles 20
 CO-4  To analyze utility of Brayton cycle and its modifications in gas turbine engines 25
 CO-5 To understand the concept of heat exchange in a process  10 
 CO-6 To apply fundamentals of thermodynamic to an aircraft engine component design/performance calculations  15 

Active Learning
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