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Opticom

Opticom

For normally loaded optimized composite aero structural part, in comparison with the existing metallic structure for the same loads and boundary condition, OPTICOM would provide:

  • Reduced number of layers
  • All together new set of stack up sequence
  • Comparable deflection and strains as output
  • Comparable deflection fringe patterns in Nastran Solver
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MAX CHARACTERS: 10,000

We will treat any information you submit with us as confidential. Please read our privacy statement for additional information.

We will treat any information you submit with us as confidential. Please read our privacy statement for additional information.