FLD120 - Aeroelasticity using FlightLoads and Patran

Length:
5 days
Pre-requisites :
NAS101A and B (Linear Analysis using MSC Nastran), NAS102A and B (Dynamic Analysis Using MSC Nastran), PAT301 (Introduction to Patran)
Topics:
- Introduction to Aeroelasticity
- Introduction to FlightLoads and Dynamics
- Aerodynamic Theories
- Doublet Lattice
- Zona51
- Subsonic Slender Body Theory
- Surface Splines
- Linear Splines
- Theory of Static Aeroelastic Analysis
- Monitor Points
- Flutter Analysis
- Aeroelastic Response Analysis
- Basics of Patran and MSC Nastran
- Patran Graphical User Interface
- MSC Nastran Files
- Mapping CFD Data to a Structural FE Model
- Load Mapping