1. Aero-Science B.Sc. Aero Science-I Total Mark: 100 Appendix A (Outlines of Tests) Aero-Engines : 100 Marks
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1 1. Aero-Science B.Sc. Aero Science-I Total Mark: 100 Appendix A (Outlines of Tests) Aero-Engines : 100 Marks Note:- The questions will be set in each paper. Candidates are to attempt any five except in Paper B in which the question on Computer will be compulsory. Appendix B (Syllabi and Courses of Reading) Aero-Engine 100 Marks Note: The depth and treatment of the topics given below will conform to the relevant material specially published by the P.A.F. College, Sargodha. The Material is referred to below: S.No. Topic Reference Material Training Notes and Precis. 1. GAS Dynamics: AENG-B-I (a) Continuity Equation Derivation. (b) Momentum Equation Derivation. (c) Energy Equation Derivation. (d) Thrust of a Static Jet Engine Derivation (e) Thrust of a Moving Jet Engine Derivation. (f) Thrust of a Turbofan Engine. (g)engine Performance Parameters Definition of: (i) Propulsion Efficiency. (ii) Thermal Efficiency. (iii) Propeller Efficiency. (iv) Over-all Efficiency. (h) Derivation of Brequet s Range formula and its analysis. (i) Take-Off Thrust. (j) Specific Fuel Consumption. (k) Effective exhaust Velocity. (l) Gross Thrust. (m) Net Thrust.
2 (n) T-S diagram of actual and ideal, Turb-jet, Efficiencies of Diffuser,Compressor. Turbine and Nozzle, Pressure Ratios of Diffuser compressor. Combustor. (o) Characteristics of subsonic and supersonic flow in venturi tube. (Review). (p)shock wave formation (Review). 2. Ramjet and Pulsejet: AENG-B-II (a) Thermodynamic limitations of Turbojet Engine. (b) Operation Principle of Ramjet. (c) Subsonic Combustion Ramjet. (d) Supersonic Combustion Ramjet (Scram Jet). (e) Application of Ramjet. (f) Operating Principle of Pulsejet. (g) Advantages and disadvantages of Pulsejet. 3. Intakes: AENG-B-III (b) Ideal Intake Conditions. (c) Flow speed and pressure behind Shockwaves. (d) Intake design. (e) Intake Shape. (f) Types of Intake for Supersonic Flight. (g) Problems of Supersonic Intake Design. 4. Compressors: AENG-B-IV (b) Requirements of a Compressor. (c) Centrifugal Compressor : (i) Introduction. (ii) Principles of Operation. (iii) Impellers. (iv) Diffuser. (d) Axtal Blow Compressor. (i)introduction. (ii) Construction (iii) Principles of Operation. (iv) Compressor Stall and surge (only introduction).
3 (e) Comparison of Axtal Flow and Centrifugal Flow Compressor Engine (i) Factors. (ii) Material. (f) Antistall devices. (g) Effects of Stall and Surge. 5. Combustion Chamber: 6. Turbines: (b) Combustion system requirements. (c) Flow through typical Combustion Chamber (d) Combustion System layout. (e) Combustion Chamber Material and Defects. (f) Burners. (b) Turbine Blading. (c) Energy transfer from Gas Flow to Turbine. (d) Vane and Blade profile. (e) Turbines operating Conditions. (f) Turbine installations. (g) Balancing and Testing of Turbines. (h) Turbine Faults. 7. Exhaust System: (b) The Exhaust Unit (c) The Jet Pipe. (d) The Nozzle. (e) Variable Geometry Nozzle. 8. Thrust Augmentation: (b) Water injection. (c) Re-heat. AENG-B-V AENG-B-VI AENG-B-VII AENG-B-VIII
4 (d) Principles of Re-heat: (i) Thrust Production. (ii) Variation of Nozzle area. (iii) Specific Fuel Consumption. (e) After Burner Components. (f) Re-heat ignition System. (g) Re-heat Control. 9. Thrust Reversal: (h) Choice of ignition and Control System. (a) Requirements of Thrust Reversal. (b) Layout and Operation of Typical Thrust Reversing System. (c) Safety Features. 10. Turboprop and Turbofan Engines: Operating principles and general characteristics. 11. V/Stol Engines: 12. Gas Turbine Fuels: 13. Rocket Motors: (a) PowerplantArrangements : (i) Composite Power Plant. (ii) Vactored Thrust. (b)engine Types: (i) Lifting Engines. (ii) Vectored Thrust Engines. (c) Advantages of Lift Thrust Turbofan. (d)large aircraft requirements and Supersonic aircraft requirements. (a) General Characteristics. (b)vapour pressure. (c) Methods of reducing or eleminating fuel losses. (d) Aviation turbine fuels, AVTUR-AVTAG-AVCAT. (a) Rocket performance. (b) Solid propellant Rocket Motors. (i) Main Components. (ii) Nozzles and nozzle cooling. AENG-B-IX AENG-B-X AENG-B-X1 AENG-B-XII AENG-B-XIII
5 (iii) Thrust vector control. (c) Liquid propeilant Rocket Motor: (i) Liquid propellant feed systems. (ii) Combustion chamber and nozzle. (iii) Liquid Rocket injectors. (d) Introduction to other propulsion system like Nuclear Rockets and Electrical propulsion Units. 14. Specific Engine System: (a) Fuel system of MFI 17 Aircraft. (b) Fuel system of T 37 Aircraft. (c) Hydraulic system of T 37 Aircraft. AENG-B-XIV
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