Helicopter UAV fuselage bulkhead modelling

This article deals with the design of helicopter UAV airframe components. There is a description of UAV airframe design modelling involving already existing components in three-dimensional (3D) form. The modelling methodology focuses in detail on proposed bulkheads by using “top-downbottom-up” methodology. In conclusion, there is a brief description of all proposed bulkheads and an outline of possible solutions for how to design airframe stringers.


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  • Accession Number: 01631529
  • Record Type: Publication
  • Files: TRIS
  • Created Date: Mar 31 2017 9:24AM