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AKTU Aircraft Propulsion Lab (BAE651) Syllabus PDF – B.Tech 3rd Year
Aircraft Propulsion Lab BAE651
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- Semester 6
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Official AKTU syllabus of Aircraft Propulsion Lab (BAE651) for B.Tech 3rd Year – 1 credits, L-T-P 0-0-2. Read the unit-wise course content, course outcomes, evaluation pattern and recommended books online, or download the PDF.
Syllabus — Aircraft Propulsion Lab
Download PDFBAE651 · 1 credits · L-T-P 0-0-2
| The students will be able to | Blooms Taxonomy | |
| CO-1 | Understand the difference in constructional arrangement of turbojet, turbofan, turboprop and turbo-shaft engines. | K2 |
| CO-2 | Understand the operation of different types of propellers and engine starting system and firing order of multi cylinder spark ignition. | K2 |
| CO-3 | Apply the concept of thrust, work done and efficiencies of turbojet, turbofan, turboprop and turbo-shaft engines. | K3 |
| CO-4 | Apply the concept of Analyze performance estimation of aircraft for the purpose of evaluation. | K3 |
| CO-5 | Understand the difference in operation and working process of two stroke and four stroke engines. | K2 |
| CO-6 | Apply the concept of Formulate a system for estimation of flight performance and stability with lift drag and thrust characteristics. | K3 |
Minimum 10 out of following such experiments (or such experiments)
- To demonstrate the constructional arrangement and operation of turbojet and turbofan.
- To demonstrate the constructional arrangement and operation of turboprop and turbo- shaft.
- Recognition of visual defects of jet engines.
- To demonstrate the operating principal 2-stroke and 4-strokeCIengines.
- To demonstrate the operating principal 2-stroke and 4-strokeSIengines.
- To demonstrate the operating principle of air cooled and water cooled piston engines.
- To demonstrate the engine configuration and firing order.
- To demonstrate the working of engine starting systems.
- To demonstrate the installation and removal procedure of propellers.
- To demonstrate operation of fixed and variable pitch propellers.
- To demonstrate operation of turbine blades to turbine disc.
- To demonstrate the working of exhaust gas temperature measurement system.
- Calculate the cylinder area, sweep area and compression ratio for CI engine.
- Test a piston engine and determine: Specific fuel consumption, Break horsepower, and Indicated horse power for four stroke petrol engines.
- Test a piston engine and determine: Break thermal efficiency, Mechanical efficiency. Volumetric efficiency for four stroke petrol engine.
- To determine velocity and pressure measurements in co-axial jets.
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