AE31001: Thermodynamics And Aerospace Prop.System

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AE31001
Course name Thermodynamics And Aerospace Prop.System
Offered by Aerospace Engineering
Credits 4
L-T-P 3-1-0
Previous Year Grade Distribution
7
11
17
7
4
6
3
EX A B C D P F
Semester Autumn


Syllabus[edit | edit source]

Syllabus mentioned in ERP[edit | edit source]

Basic concepts of thermodynamics, first and second laws of thermodynamics and their corollaries, Engine cycles; Basic Principles of Propulsion, Classification and Characteristics of Aerospace Propulsive Devices, Thermodynamic and Real Cycle Analysis, Aviation Fuels, Theory of Propellers; Centrifugal Compressor and its performance; Nozzles, Subsonic and Supersonic Intakes, Combustion Chambers; Rocket propulsion.Books:J D Mattingly, Elements of Gas Turbine Propulsion, McGraw-HillJ D Mattingly, W H Heiser, D H Daley, Aircraft Engine Design, AIAAE L Houghton and A E Brock, Aerodynamics for Engineering Students, Edward ArnoldS L Dixon, Fluid Mechanics, Thermodynamics of Turbomachinery, Pergamon PressH Cohen, G F C Rogers, and H Saravanamutto, Gas Turbine Theory, Longman


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
Tuesday
Wednesday NC334
Thursday NC334
Friday NC334 NC334