AEROELASTICITY

LDP Aerospace can handle aeroelastic problems. Four main analyses are available: one for static aeroelastic analyses, a second for modal flutter analyses by the K-, KE-, or PK-methods, a third for modal dynamic aeroelastic response analyses due to gusts or control surface deflections, and a fourth for design sensitivity and optimization including aeroelastic effects.

• Doublet-Lattice Theory
  • 2D Subsonic and supersonic
  • Slender body
• Mach Box Lifting Surface
• Strip Surface Theory
• Piston Surface Theory

• Static Aeroelastic Response (Divergence)
• Aerodynamic Flutter Velocity
• Aeroelastic Fluter Response