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  1. egalvan

    Fuselage skin door corners

    wktaylor, FYI, skin material is Al2024 T42 Clad sheet. Sorry for the annoying amateur omission...
  2. egalvan

    Fuselage skin door corners

    it looks to me that we still have a little bit of work to do to have this issue solved... Thank you for the tips rb1957.
  3. egalvan

    Fuselage skin door corners

    Thanks rb1957 for your answer. Although permanent deformation is expected according to the residual compressive strains in the strain gages after unloading, visual inspections in the skin corner after test did not reveal any damage or significative deformation in the area, and therefore rule...
  4. egalvan

    Fuselage skin door corners

    In a static test campaing, for some critical load cases we have found that the skin at the fuselage door corner reaches compressive stress values 30%-40% higher than the Fty of the skin material (Al 2024)at limit load, so we have started to think in the necessity of introducing additional...

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