Project “Future Projects Office”: High-aspect-ratio Wing Nonlinear Aeroelastic Modeling and Validation

• Project objectives:
  • Develop, implement, and experimentally validate a method that extends the
    classical modal approach towards large wing deformations while keeping the
    modal approach simplicity.
• Nonlinear modes
  • Direct identification of the 3-D built-up FEM model
     Only need a static nonlinear FEM solver for model ID and create of dynamic
    model