BAE601

Aircraft Structure

L-T-P3-1-0 Credits4 Session2024-25 TypeTheory
Appears in 1 semester

B.Tech Aeronautical Engineering · Sem 6 (Core)

Syllabus

5 units · 42 lecture hours
Unit1

Unit 1

9 hrs
  • Introduction Different structural components of aircraft and their configuration, Types of loads acting on aircraft structure, V-n diagram and Gust envelope, Properties and selection of aircraft materials, Honeycomb structures, Use of thin-walled cross-sections in aircraft structural components.
  • Composite Materials Composition and Types of composite materials, Effective modulus of composite laminates, Applications of composites.
Unit2

Unit 2

8 hrs

Theory of Elasticity Stresses on inclined plane subjected to tri-axial loading, 3-D principal stresses and strains, Stress-displacement relations, Strain compatibility, Equilibrium equations, Generalized Hooke’s law, Types of materials based on elastic symmetry: anisotropic, orthotropic and isotropic materials. Plane stress and plane strain conditions, governing equations for plane elasticity, Compatibility relation in terms of stress components, Airy’s stress function, Solution of plane elasticity problems using Airy’s stress function.

Unit3

Unit 3

9 hrs
  • Torsion St.Venant’s torsion theory, Warping in shafts of circular and non-circular cross-sections, Difference between polar moment of inertia and torsional rigidity, Prandtl’s stress function, Torsion of open and closed thin-walled sections, Torsion of multi-cell closed sections, Torsional shear flow.
  • Unsymmetrical Bending Euler-Bernoulli beam equation for unidirectional and bidirectional bending, Timoshenko beam equation, Deflection of cantilever beam using Euler-Bernoulli and Timoshenko beam theory, Bending of unsymmetrical cross-sections, Structural idealization.
Unit4

Unit 4

8 hrs
  • Flexural Shear Stress Transverse shear stress in solid cross-sections, Transverse shear stress and shear flow in general symmetric and unsymmetrical thin-walled sections, Location of shear center in open and closed cross-sections, Shear flow in multi-cell thin-walled sections, Combined torsional and flexural shear flow.
  • Buckling of Columns and Plates Derivation of governing equation for column buckling, Euler’s and Rankine’s buckling load, Effect of end conditions on column buckling, buckling of thin plates.
Unit5

Unit 5

8 hrs
  • Vibration Basic concepts of vibration, Types of vibration, General governing equation for vibration, Un-damped and Damped free vibration, Forced vibration, Logarithmic decrement, Torsional vibrations, Vibration of Two Degree of Freedom System, Coordinate coupling, Semi-definite systems
  • Vibration of Continuous Systems Torsional vibration of shaft, longitudinal vibration of bars and lateral vibration of beams.
Course Outcomes (COs)6 outcomes

After completion of the course student will be able to:

  1. CO1K2 acting on them. Understand the common equations of solid mechanics using the theory
  2. CO2K2 of elasticity approach. Apply the suitable theories of failure while designing the aircraft structural
  3. CO3K3 components. Apply the basic concepts to design a new prototype of aircraft and able to
  4. CO4K3 present new layout or plan. Develop the ability to analyze bending, torsion and buckling problems to
  5. CO5K2 a practical level and not just rely on the simple approximations. Apply the vibration concepts to find out the mode shapes during vibration
  6. CO6K3 of muti-degree of freedom systems.

Books and References

  1. C. T. Sun, Mechanics of Aircraft Structures, John Wiley and Sons
  2. T.H.G. Megson, Aircraft Structures for Engineering Students, Butterworth-Heinemann
  3. S. Timoshenko and J.N. Goodier, Theory of Elasticity, McGraw Hill Education.
  4. V. P. Singh, Mechanical Vibrations,DhanpatRai and Co.
  5. Singiresu S. Rao, Mechanical Vibrations, Pearson Education

Official AKTU syllabus

This subject is on page 28, 29 of the original AKTU PDF.

Official AKTU syllabus PDF ↗