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01-13-2017
02:26 AM
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Hello,
At the moment I am considering a simplified aircraft fuselage.
Dimensions:
Diameter: 3500 mm
Thickness skin: 1 mm
Thickness floor beam: 9.6 mm
Length: 31420 mm
After applying a pressure of 0.064 MPa, it takes an enormous amount of time to solve.
After waiting for more than 1 hour, it still has not provided a solution.
We suspect it has something to do with the mesh settings or the quite large length size.
Our last resort would be to shorten the length of the fuselage, but eventually we want to
analyse bending as well, which will be affected by a different length.
Help would be greatly appreciated!
With kind regards,
AJ
Solved! Go to Solution.