AE40030: Advanced Gas Turbine Theory

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AE40030
Course name Advanced Gas Turbine Theory
Offered by Aerospace Engineering
Credits 3
L-T-P 3-0-0
Previous Year Grade Distribution
1
3
4
2
3



EX A B C D P F
Semester Spring


Syllabus[edit | edit source]

Syllabus mentioned in ERP[edit | edit source]

Prerequisites: AE31001, AE31008 3 - 0 - 0: 3 CreditsGeneral propulsion systems, Theory of intakes and exhaust systems, thrust reversal, jet engine noise and methods of noise reduction, Cycle analysis of one and two spool engines, Equilibrium running of gas turbine engines, Component matching, Transient behavior, Design consideration of axial flow multistage machines, stream line curvature method, radial equilibrium equation, Design and off-design performance.


Concepts taught in class[edit | edit source]

Student Opinion[edit | edit source]

How to Crack the Paper[edit | edit source]

Classroom resources[edit | edit source]

Additional Resources[edit | edit source]


Time Table[edit | edit source]

Day 8:00-8:55 am 9:00-9:55 am 10:00-10:55 am 11:00-11:55 am 12:00-12:55 pm 2:00-2:55 pm 3:00-3:55 pm 4:00-4:55 pm 5:00-5:55 pm
Monday 2nd Year Class Room
Tuesday 2nd Year Class Room 2nd Year Class Room
Wednesday
Thursday
Friday