MTech Propulsion Lab syllabus for 1 Sem 2018 scheme 18MAPL16

Module-1 Experiments 56 hours

Experiments

1. Cascade testing of a model of turbine blade row and study of wake survey.

2. Estimation of propeller performance

3. Forced Convective heat transfer on a flat surface

4. Measurement of Burning Velocity of a Premixed Flame

5. Determination of heat of combustion of aviation fuels

6. Fuel - injection characteristics (spray cone geometry; spray speed etc. for various types of injectors)

7. Measurement of static overall pressure rise & rotor static pressure rise & fan overall efficiency through axial flow fan unit

8. Effect of inlet flow distortion on measurement of static overall pressure rise & rotor static pressure rise & fan overall efficiency through axial flow fan unit .

9. Investigation of relationship between flame speed and air-fuel ratio for a slow burning gaseous fuel.

10. Construction of flame stability diagram through flame lift up and flame fall back

11. Measurement of static overall pressure rise & rotor static pressure rise & fan overall efficiency through counter rotating axial flow fan unit

12. Effect of inlet flow distortion on measurement of static overall pressure rise & rotor static pressure rise & fan overall efficiency through contra rotating axial flow fan unit .