LP-RajalakshmiEngineeringCollege.docVIP

RAJALAKSHMI ENGINEERING COLLEGE DEPARTMENT OF AERONAUTICAL ENGINEERING LESSON PLAN LP Rev No: 00 Date: 20-06-2011 Sub Code Name: AE2304 PROPULSION-II Class: B.E - Aeronautical Engineering Semester: V Staff: Mr. Suresh Chandra Khandai Unit No Session No Topics to be covered Duration in Periods Teaching Method BB/PPT/Video 1 2 3 4 5 AIRCRAFT GAS TURBINES 1 Impulse and reaction blading of gas turbines 1 BB/PPT 2,3 Velocity triangles and power output 2 BB 4 Vortex theory 1 BB 5 Choice of blade profile, pitch and chord 1 BB 6 Estimation of stage performance 1 BB 7 Limiting factors in gas turbine design 1 BB 8 Methods of blade cooling 1 BB/PPT 9 Matching of turbine and compressor. 1 BB/PPT 10-12 Numerical problems 3 BB 13,14 University question paper solution 2 BB RAMJET PROPULSION 15 Operating principle of Ram jet engine 1 BB/PPT 16 Sub critical, critical and supercritical operation of Ramjet 1 BB/PPT 17 Combustion in Ramjet engine 1 BB/PPT 18,19 Ramjet performance 2 BB/PPT 20 Ramjet design calculations 1 BB/PPT 21 Introduction to scramjet. 1 BB/PPT 22,23 Numerical Problems 2 BB 24,25 University question paper solution 2 BB FUNDAMENTALS OF ROCKET PROPULSION 26 Operating principle 1 BB/PPT 27,28 Specific impulse of a rocket - Derivation 2 BB 29 Internal ballistics of rocket engines 1 BB/PPT 30 Rocket nozzle classification - Explanation 1 BB/PPT 31,32 Rocket performance considerations 2 BB/PPT 33,34 Numerical problems 2 BB 35,36 University question paper solution 2 BB CHEMICAL ROCKETS 37,38 Solid propellant rockets – Selection criteria of solid propellants 2 BB/PPT 39,40 Hardware components of solid rockets – Propellant grain design considerations 2 BB/PPT 41,42 Liquid propellant rockets – Selection of liquid propellants 2 BB/PPT 43 Cooling in liquid rockets 1 BB/PPT 44,45 Hybrid rockets 2 BB/PPT 46,47 Numerical problems 2 BB 48 University question p