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  1. matavia

    Deformable Contact Body, Fuselage - Wing connection, non-linear sol 400 NASTRAN

    I made as u said and: This is my bulk data entry: $ Complex Eigenvalue Analysis, Direct Formulation, Database SOL 400 CEND $ Direct Text Input for Global Case Control Data TITLE = MSC.Nastran job created on 05-Feb-15 at 18:12:01 SUBCASE 1 STEP 1 SUBTITLE=Default ANALYSIS = NLSTATIC...
  2. matavia

    Deformable Contact Body, Fuselage - Wing connection, non-linear sol 400 NASTRAN

    Nlgyro, thanks for clue!
  3. matavia

    Deformable Contact Body, Fuselage - Wing connection, non-linear sol 400 NASTRAN

    I forgot to say that i put several types of force (i try with pressure, nodal/point force, total load) nothing is working) My vector force is in (x,y) plane.
  4. matavia

    Deformable Contact Body, Fuselage - Wing connection, non-linear sol 400 NASTRAN

    Hey everybody, Thanks for attencion. I have specific issue, which I am not able to solve. If u would help me i will be gratefull. It is my first post so, please to be lenient. one part of my engineer thesis is to symulate contact condition. To make it i use Patran 2012 with Nastran solver. (I...
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