Courseware

Under-Graduate Programmes

Courseware
Unit 1 - Why Aerodynamics
Unit 2 - Variation of Cl with the angle of attack and Reynolds
Unit 3 - The Aerodynamic Center
Unit 4 - Lift for a Finite Wing
Unit 5 - Swept Wings
Unit 6 - Wing-Body Combinations
Unit 7 - Different types of engines
Unit 8 - The Equations of Motion
Unit 9 - Analytical Approach
Unit 10 - Thrust available and the maximum Velocity of the airplane
Unit 11 - Power Required
Unit 12 - Rate Of Climb
Unit 13 - Gliding Flight
Unit 14 - Range
Unit 15 - Endurance
Unit 16 - Level Turn
Unit 17 - Takeoff Performance
Unit 18 - Landing Performance
Unit 19 - Seven Points For Conceptual Design
The Turbofan Engine
Turbojet
Dispersion Analysis of a rocket
Missile Classifiction
Dispersion Reduction For a Sounding Rocket Scramjet Flight Experiment
Rocket Performance
Analysis of Dispersion for Trajectories of Fire-extinguishing Rocket
L V optimisation
Air-Launched Giuded Missiles and Guided Missile Launchers
Launch vehicle staging
MONTE CARLO DISPERSION ANALYSIS OF A ROCKET
Rocket Rotational Dynamics IIMRI class notes
Rocket Tranlational Dynamics
LV Staging optimisation
BASICS OF LIQUID PROPELLANT ROCKET SYSTEM
DESIGN BASICS OF SOLID PROPELLANT ROCKETS
Design Of Prototype
ROCKETS AND MISSILES
Space Ordnance
CRYOGENIC PROPULSION SYSTEM
Materials for rockets and missiles
Liquid Propulsion System
Testing
AS0403 - Aircraft Systems & Instruments
Aircraft Control Systems
Aircraft Pressurisation Systems
Aircraft Instruments