Aeroelasticity using MSC Nastran  

NAS111

Objective

This seminar is intended for engineers concerned with structural loads, flying qualities, and aeroelastic stability of flexible aircraft and missiles. The objective of the seminar is to familiarize the engineer with state-of-the-art MSC Nastran applications in aeroelastic analyses. An overview of the aeroelastic capability is followed by an in-depth discussion of the available aerodynamic theories and the three available aeroelastic solutions: static aeroelasticity, flutter, and dynamic aeroelasticity. Advanced topics include modeling aerodynamic bodies, active control systems, the specification of dynamic loads, sensitivity analysis, and aeroelastic optimization.


Content

  • Overview of MSC Nastran Aeroelastic Capabilities
  • Aerodynamic Theories
  • Surface and Linear Splines
  • Static Aeroelastic Analysis
  • Flutter Analysis
  • Preparation of Input/Sample Problems
  • Dynamic Aeroelasticity
  • Guidelines for Effective Response Analysis
  • Aeroelastic Design Sensitivities and Optimisation
  • Workshops


Prerequisites

NAS101/NAS120 and NAS102/NAS122 or equivalent experience. Experience with additional solution sequences and superelement analysis is helpful.


Dates

Instructor-led online:

21.02.2023-23.02.2023

26.09.2023-28.09.2023


Duration

3 days


Price

£1,350+VAT(Hexagon office)/£900+VAT(online)


Contact

Tel: +44 (0)1276 903120
Email: MI-MSC-info.uk@hexagon.com