FLD120S - FlightLoads and Aeroelasticity - Static Analysis

Length:
3 days
Pre-requisites :
NAS101A (Linear Static and Normal Modes Analysis using MSC Nastran), NAS 101B (Advanced Linear Analysis using MSC Nastran), NAS120 (Linear Static Analysis Using MSC Nastran and Patran), or equivalent; NAS102A (Dynamic Analysis using MSC Nastran), NAS102B (Advanced Dynamic Analysis Using MSC Nastran), PAT301 (Introduction to Patran)
Topics:
- Introduction MSC Nastran Aerodynamics
- Introduction MSC Nastran Splining
- Introduction MSC Nastran Aeroelastic Solutions
- Static Aeroelasticity
- Introduction to FlightLoads
- Aerodynamic Theories
- Doublet Lattice
- CPM
- Zona51
- Slender Bodies
- Aeroelastic Overview
- Surface Splines
- Linear Splines
- Basics of Patran and MSC Nastran
- Patran GUI
- Nastran File Format
- Nastran Syntax
- Static Aeroelasticity
- Theory
- Case Study 1 and Workshop - FSW aircraft in longitudinal trim
- Case Study 2 and Workshop - Longitudinal Analysis of a straight wing aircraft
- Case Study 3 and Workshop - Aileron Effectiveness in Roll
- Case Study 4 and Workshop - Advanced fighter aircraft analysis
- Case Study 5 and Workshop - Advanced Wing and Canard Aero Workshop