The course is intended to provide learning on the mathematics behind the computational analysis, Different methods of analysis, Mathematical modeling of the various phenomena related to vibration analysis, various failure criteria and theory related to elastic fracture.
- Understand vibrations and fluid dynamics behind the aerospace system
- Understand of different design aspects related to loading in aerospace system
- Do the system dynamic analysis using finite element methods
- Principles and methods of computational structural dynamics and vibration analysis
- Introduction to dynamic analysis using the finite element method, Calculation of modal parameters
- System dynamic response via mode superposition, frequency response, model reduction, and structural synthesis techniques, Fatigue analysis
- Introduction to aero-elasticity, Aerodynamic Loading, Bending Moment, Sectional properties of Aerofoil, V-n Diagra,
- Basic theory of linear elastic fracture mechanics; strain energy release rate
- Applications to delamination crack growth in polymer composite laminates, Damage tolerance issues in composites
