6th Sem, AERO

18AEL67: Aircraft Structures Lab AERO Syllabus for BE 6th Sem 2018 Scheme VTU

Aircraft Structures 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 structures lab is as follows.

Course Objectives:

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List of Experiments:

  1. Deflection of a Simply Supported Beam.
  2. Deflection of a cantilever Beam
  3. Beam with combined loading by using superposition theorem
  4. Verification of Maxwell’s Reciprocal Theorem for beam with
    1. Constant cross section
    2. Varying Cross section
  5. Determination of Young’s Modulus using strain gages.
  6. Poisson Ratio Determination
  7. Buckling load of slender Eccentric Columns and Construction of Southwell Plot
  8. Shear Failure of Bolted and Riveted Joints
  9. Bending Modulus of sandwich Beam
  10. Tensile, Compressive and Flexural testing of a composite material plate.
  11. Determination of natural frequency and mode shapes of a cantilever beam for the following cases.
    1. Constant cross section
    2. Varying cross section
    3. Constant cross section and varying stiffness
  12. Determination of shear centre for following cases through deflection measurements.
    1. Close section-Symmetrical bending
    2. Open section-Unsymmetrical bending
  13. Determination of shear flow for following cases.
    1. Close section-Symmetrical bending
    2. Open section-Unsymmetrical bending
  14. Determining of Shear centre through shear flow measurement for following cases.
    1. Close section-Symmetrical bending
    2. Open section-Unsymmetrical bending

Course Outcomes:

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

  1. Compute the deflection of simply supported beam and cantilever beam.
  2. Verify the Maxwell’s theorem.
  3. Determine the buckling load, shear failure and shear centre.

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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