8th Sem, AERO

Theory of Elasticity Aero 8th Sem Syllabus for BE 2017 Regulation Anna Univ (Professional Elective V)

Theory of Elasticity Aero 8th Sem Syllabus for BE 2017 Regulation Anna Univ (Professional Elective V) detail syllabus for Aeronautical Engineering (Aero), 2017 regulation is collected from the Anna Univ official website and presented for students of Anna University. The details of the course are: course code (AE8017), Category (PE), Contact Periods/week (3), Teaching hours/week (3), Practical Hours/week (0). The total course credits are given in combined syllabus.

For all other aero 8th sem syllabus for be 2017 regulation anna univ you can visit Aero 8th Sem syllabus for BE 2017 regulation Anna Univ Subjects. For all other Professional Elective V subjects do refer to Professional Elective V. The detail syllabus for theory of elasticity is as follows.

Course Objective:

  • To make the student understand the elastic behavior of different structural components under various loadings and boundary conditions.

Unit I

For complete syllabus and results, class timetable and more pls download iStudy. Its a light weight, easy to use, no images, no pdfs platform to make students life easier.

Unit II

Plane Stress and Plane Strain Problems
Airys stress function, Bi-harmonic equations, Polynomial solutions, Simple two dimensional problems in Cartesian coordinates like bending of cantilever and simply supported beams.

Unit III

Polar Coordinates
Equations of equilibrium, Strain – displacement relations, Stress – strain relations, Airys stress function, Axi – symmetric problems, Introduction to Dunders table, Curved beam analysis, Lames, Kirsch, Michells and Boussinesque problems – Rotating discs.

Unit IV

For complete syllabus and results, class timetable and more pls download iStudy. Its a light weight, easy to use, no images, no pdfs platform to make students life easier.

Unit V

Introduction To Theory of Plates and Shells
Classical plate theory – Assumptions – Governing equations – Boundary conditions – Naviers method of solution for simply supported rectangular plates – Levys method of solution for rectangular plates under different boundary conditions.

Course Outcome:

  • Ability to use mathematical knowledge to solve problem related to structural elasticity.
  • Identify stress-strain relation in 3D, principal stress and principal strain.
  • Analyze a structure using Elasticity concepts.
  • Use analytical techniques to predict deformation, internal force and failure of simple solids and structural components.
  • Solve aerospace-relevant problems in plane strain and plane stress in Cartesian and polar coordinates.

Text Books:

  1. Ansel C Ugural and Saul K Fenster, “Advanced Strength and Applied Elasticity”, 4th Edition, Prentice Hall, New Jersey, 2003.
  2. Bhaskar, K., and Varadan, T. K., “Theory of Isotropic/Orthotropic Elasticity”, CRC Press USA, 2009.
  3. Timoshenko, S., and Goodier, T.N., “Theory of Elasticity”, McGraw – Hill Ltd., Tokyo, 1990.

References:

  1. Barber, J. R., “Elasticity”, Kluwer Academic Publishers, 2004
  2. Sokolnikoff, I. S., “Mathematical Theory of Elasticity”, McGraw – Hill, New York, 1978.
  3. Volterra and J.H. Caines, “Advanced Strength of Materials”, Prentice Hall, New Jersey, 1991
  4. Wang, C. T., “Applied Elasticity”, McGraw – Hill Co., New York, 1993.

For detail syllabus of all other subjects of BE Aero, 2017 regulation do visit Aero 8th Sem syllabus for 2017 Regulation.

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