18ASL67: Aircraft Structures Lab AS Syllabus for BE 6th Sem 2018 Scheme VTU

Aircraft Structures Lab detailed Syllabus for Aerospace Engineering (AS), 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 AS 6th Sem Syllabus for BE 2018 Scheme, do visit VTU AS 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 beams with.
   1. Constant cross section
   2. Varying cross section
5. Determination of Young’s Modulus using strain gages.
6. Determination of natural frequency, 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.
7. Buckling load of slender Eccentric Columns and Construction of Southwell Plot
8. Shear Failure of Bolted and Riveted Joints
9. Determination of damping coefficient of a cantilever beam for the following cases.
10. Determination of shear flow and shear centre through shear flow for the case of close section beam -Symmetrical bending.
11. Tensile, Compressive and Flexural testing of a composite material plate.
12. Estimation of natural frequency and mode shapes of a two rotor system.
13. Determining of Shear centre location for closed and open section beams through deflection measurements.
14. Determination of shear flow and shear centre through shear flow for the case of beam of 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.
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For detail Syllabus of all other subjects of BE 6th Sem Aerospace Engineering, visit (AS) 6th Sem Syllabus Subjects.

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