Aircraft Structure detail syllabus for Aeronautical Engineering (Aero), 2019-20 scheme is taken from AKTU official website and presented for AKTU students. The course code (RAE601), and for exam duration, Teaching Hr/Week, Practical Hr/Week, Total Marks, internal marks, theory marks, duration, 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. The detail syllabus for aircraft structure is as follows.
Unit 1
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Unit 2
Analysis of Fuselage or Structural idealization. Arrystress function. Fatigue loads, Fluctuating stress and theories of failure.2-D and 3-D stress and strain relations. Principal stresses. 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.Equilibrium Equations. Constitutive Equations, 3D Constitutive Equations. Constitutive Relations: Generally Anisotropy to Orthotropic. Constitutive Relations: Transverse Isotropy and Isotropy.
Unit 3
Deflection of Beams-Types of beams. Various methods of slope-deflection for beams. Principle of virtual work.Application to deflection problems on fixed and cantilever beams.Deflection of open and close section beams. Shear force and bending moment distribution for semi-cantilever and other types of (wings and fuselage,) beam.Pure bending and Torsion Equation and their applications.Bending of thin plates, plate subjected to bending and twisting.Bending stresses in beams of unsymmetrical sections-and symmetric sections with skew loads. Combined bending and twisting on plate and beams.
Unit 4
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Unit 5
Bucking in Beam & Plates-Euler buckling of columns and beams inelastic stability of columns, effect of initial imperfections, energy method for the calculation of buckling loads in columns and thin plates. Flexural and tensional buckling in the thin walled columns.Buckling stress of thin walled sections, crippling strength estimation.Buckling in stiffened rectangular sheets under compression.
Books and References:
- Megson T M G, Aircraft Structures for Engineering Students’, Edward Arnold,1995.
- Bruhn. E.H., Analysis and Design of Flight Vehicles Structures’, Tri-state offset company, USA, 1985.
- Howard D Curtis, Fundamentals of Aircraft Structural Analysis’, WC BMcGraw Hill, 1997.
- 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
- J. W Dallyand , W,F Riley Experimental Stress Analysis, Mc Graw Hill 1965
- F.R. Shanley, Weight Strength Analysis of Aircraft Structures, Dover Publications, 1960
For detail syllabus of all other subjects of B.Tech Aero, 2019-20 scheme do visit Aero 6th Sem syllabus for 2019-20 scheme.
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