Introduction to propulsion - Basic thermodynamics, Fundamental equations - Types of aircraft engines - Performance parameters - thrust equation, factors affecting thrust and efficiencies. Atomization and spray formation.
Ram effect, Internal flow and Stall in subsonic inlets – relation between minimum area ratio and eternal deceleration ratio – diffuser performance – modes of operation - supersonic inlets – starting problem on supersonic inlets – shock swallowing by area variation – real flow through nozzles and nozzle efficiency – losses in nozzles – thrust reversal.
Working principle of gas turbine engine - gas turbine cycle - turboprop - turbofan and turbojet engines -Thrust and efficiency - Methods of thrust augmentation - Engine performance characteristics.
History of rocket propulsion - types of rockets - Basic configurations and application -Types of missiles and their structure - Heat transfer and cooling system in rocket - classification of Chemical rocket propulsion system- MPD thrusters.
Static performance - vehicle acceleration - performance characteristics - nozzle, solid, liquid, and hybrid rocket, and their propellants- Electric propulsion for space applications - magnetic levitation propulsion.
Reference Book:
1. Mathur, M.L.and Sharma, R.P., Gas Turbine, Jet and Rocket Propulsion, 2nd Edition, Standard Publishers Distributors, Delhi, 2008. 2. Rolls Royce, "Jet Engine, 5th Edition, Rolls Royce Technical Publications, 2005 3. Klause Hunecke, Jet Engines - Fundamentals of theory, design, and operation, 1st Edition, the Cordwood Press Ltd, 2010 4. SM Yahya, Turbines, Compressors and Fans Tata McGraw Hill Education Pvt Ltd. 4th Edition, 2011. 5. Robert D.Zucker, Oscar Biblarz, Fundamentals of Gas Dynamics, 2nd Edition, John Wiley & Sons Inc, Print 2011
Text Book:
1. Hill, P.G. & Peterson, C.R. Mechanics & Thermodynamics of Propulsion, 2nd Edition, Pearson Publishers, 2008. 2. Cohen, H. Rogers, G.F.C. and Saravanamuttoo, H.I.H. Gas Turbine Theory, Prentice Hall; 6th Edition, 2008.