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Spacecraft Assembly - Panel
Spacecraft Assembly - Panel

Numerical Results

 

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Total Deformation

The following figure shows the total deformation at the end of the second load step. Note the separation between the mid and lower nozzles. Also inspect the total deformation after the 1st and 3rd load steps.
  

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Equivalent Stress

The following figure shows the equivalent or von Mises stress at the end of the second load step. The max value occurs in the bolt. It turns out these stress values change appreciably on refining/improving the mesh. 
 

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Go to Step 7: Verification & Validation

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