6th Sem, AERO

18AEL66: Aircraft Propulsion Lab AERO Syllabus for BE 6th Sem 2018 Scheme VTU

Aircraft Propulsion Lab detailed Syllabus for Aeronautical Engineering (AERO), 2018 scheme has been taken from the VTUs official website and presented for the VTU students. For Course Code, Subject Names, Teaching Department, Paper Setting Board, Theory Lectures, Tutorial, Practical/Drawing, Duration in Hours, CIE Marks, Total Marks, Credits and other information do visit full semester subjects post given below. The Syllabus PDF files can also be downloaded from the official website of the university.

For all other VTU AERO 6th Sem Syllabus for BE 2018 Scheme, do visit VTU AERO 6th Sem Syllabus for BE 2018 Scheme Subjects. The detailed Syllabus for aircraft propulsion lab is as follows.

Course Objectives:

For the complete Syllabus, results, class timetable, and many other features kindly download the iStudy App
It is a lightweight, easy to use, no images, and no pdfs platform to make students’s lives easier.
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List of Experiments:

  1. Study of an aircraft piston engine. (Includes study of assembly of sub systems, various components, their functions and operating principles.
  2. Study of an aircraft jet engine (Includes study of assembly of sub systems, various components, their functions and operating principles.
  3. Study of forced convective heat transfer over a flat plate.
  4. Cascade testing of a model of axial compressor blade row.
  5. Cascade testing of a model of axial Turbine blade row
  6. Study of performance of a propeller.
  7. Determination of heat of combustion of aviation fuel.
  8. Study of free and wall jet
  9. Measurement of burning velocity of a premixed flame.
  10. Study of the flame lift up and fall back phenomenon for varied Air/Fuel ratio.
  11. Measurement of nozzle flow.
  12. Performance studies on a scaled jet engine
  13. Investigation of pressure distribution and relationship between inlet pressure/outlet pressure and mass flow rate in a convergent-divergent nozzle when working over a variety of overall pressure ratios including under-expanding and over-expanding conditions.
  14. Investigation of pressure distribution and relationship between inlet pressure/outlet pressure and mass flow rate in a convergent-divergent nozzle under choked conditions.

Course Outcomes:

At the end of the course the student will be able to:

  1. Analyze the cascade testing of axial compressor and axial turbine blade row.
  2. Evaluate the performance of a jet engine.
  3. Perform the measurement of a flame and nozzle flow.

Conduct of Practical Examinations:

For the complete Syllabus, results, class timetable, and many other features kindly download the iStudy App
It is a lightweight, easy to use, no images, and no pdfs platform to make students’s lives easier.
Get it on Google Play.

For detail Syllabus of all other subjects of BE 6th Sem Aeronautical Engineering, visit (AERO) 6th Sem Syllabus Subjects.

For all (CBSE & Non-CBSC) BE results, visit VTU BE all semester results direct links.

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