Online course on Turbomachinery I (3:0)
Last day to apply: 27 July 2025
Objectives
To introduce Turbomachinery fundamentals in a rational framework so as to bolster the Aerothermodynamics of turbomachinery in general and Aeroengines in particular. This is expected to be followed up by a second course in Aeroengine turbomachinery.
Syllabus
Introduction
Dimensional Anlaysis and Simillitude
Cascade flows
Axial Flow Turbines
Axial Flow Compressors
Centifugal pumps and compressors
Aerothermodynamics of Jet propulsion
Course Plan
Week 1 – 2
Introduction
Dimensional Anlaysis and Simillitude
Cascade flows
Weeks 3-6
Axial Flow Turbines
Weeks 7-10
Axial Flow Compressors
Weeks 11-14
Centifugal pumps and compressors
Weeks 15-18
Aerothermodynamics of Jet propulsion
Number of credits – 3:0
Mode of Instruction
Online Classes
Duration
AUG-DEC 2025
Class start date
5th August 2025
Timings of the class
Tuesday and Thursday (6.30PM to 8.00PM)
Course Fee
₹ 15000 (Excluding 18% GST)
Particulars | Amount (in ₹) |
Course Fee | 15,000 |
Application Fee | 300 |
GST@18% | 2,754 |
Total | 18,054 |
Who Can apply?
B E Mechanical or Aerospace Engineering
Pre-requisites:
Basic courses in Fluid Mechanics Gas Dynamics and Thermodynamics
Who will benefit
Gas Turbine and Turbomachinery design Engineers and Academics