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To work as part of a team, often deployed to a multi-disciplinary project, that ensures structural integrity of a major sub-assembly of a product.
Ideal candidates should have had a minimum of two years working as an aircraft stress engineer involved in the static and fatigue analysis of
metallic structures using a broad range of hand and computer
methods. Should have a working knowledge of one or more
of the following packages:- Nastran, Patran, Matlab, Fortran
or Ansys. Disciplines
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