Composite Material and Structure detail syllabus for Aeronautical Engineering (Aero), 2019-20 scheme is taken from AKTU official website and presented for AKTU students. The course code (RAE062), and for exam duration, Teaching Hr/Week, Practical Hr/Week, Total Marks, internal marks, theory marks, and credits do visit complete sem subjects post given below.
For all other aero 6th sem syllabus for b.tech 2019-20 scheme aktu you can visit Aero 6th Sem syllabus for B.Tech 2019-20 Scheme AKTU Subjects. For all other Departmental Elective-2 subjects do refer to Departmental Elective-2. The detail syllabus for composite material and structure is as follows.
Unit 1
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Unit 2
Equilibrium Equations. Constitutive Equations, 3D Constitutive Equations. Constitutive Relations: Generally Anisotropy to Orthotropic. Constitutive Relations: Transverse Isotropy and Isotropy. Constitutive Relations for Orthotropic Materials and Stress-Strain Transformations. Stiffness, Compliance Transformation and Hygro-thermo-elastic Constitutive Relation. Plane Stress Constitutive Equations. 2-Dimensional Lamina Analysis. Lamina Engineering Constants. Laminate Theory.
Unit 3
Introduction to Classical Plate Theory. Laminate Constitutive Relations. Laminate Engineering Constants. Hygro -thermal Laminate Theory. Failure and Damage. Damage Mechanisms in Unidirectional Composites. Macroscopic Failure Theories.
Unit 4
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Unit 5
Effective Plane Strain Bulk Modulus. Effective Axial Shear Modulus. Effective Transverse Shear Modulus. Tanaka and Halpin -Tsai Models. Background to Mechanical Testing. Quality Assessment and Physical Properties. Tensile and Compressive Testing. Design Considerations in Laminated Composites. Design Considerations in Laminated Composites. Poisson’s Ratio.
Books and References:
- Rivello, R.M., Theory and Analysis of Flight Structures, McGraw Hill, 1993.
- Peery, D.J., and Azar, J.J., Aircraft Structures, 2nd edition, McGraw – Hill, N.Y., 1999.
- D.J.Perry, Aircraft Structures, Mc Graw Hill 1950
- E.E. Sechler& L,G, Dunn, Airplane Structural Analysis & Design , Wiley & Sons Ltd,
- F.E. Bruhn Analysis & Design of ?Flight Vehicle Structures , Tristate offset Co, 1965
- A.S. Niles & J,S, Newel , Airplane Structural Analysis and Design, Vol & II Wiley & Sons ltd,
- F.R. Shanley , Weight Strength Analysis of Aircraft Structures , Dover Publication, 1960
- S. Timoshenko and J,N, Goodier , Theory of Elasticity , Mc Graw Hill , 1951
- J.P. Den Hartog, Advanced Strength of materials, McGraw Hill , 1952
- S. Timoshenko and J,M, Gere , Theory of Elasti Stability , Mc Graw Hill 1961
- S. Timoshenko and K,S, Woenowsky , Theory of Plates & Shells , Mc, Graw Hill , 1959
- M.F. Rubinstein , Matrix computer Analysis of Structures , Prentice Hall 1966
- B. Venkatraman and S, A. Patel , Structural Mechanics with Introduction to Elasticity and Plasticity , Mc Graw Hill 1965.
For detail syllabus of all other subjects of B.Tech Aero, 2019-20 regulation do visit Aero 6th Sem syllabus for 2019-20 Regulation.
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