Aluminum Alloy NL

Geometry is thanks to Oleksandr Babenko from grabcad.

Aspect ratio = 2

Chord = 1 m

The geometry and setup consider the general pressure loads upon the external wing without the internal structural components. The whole wing is made of the selected material.

After this first case general analysis would be to consider the internal structural components of the wing and to cut as much mass as possible while maintaining the stress profile of the wing to be within the limits of a set of requirements.

Author’s notes

This is my first time making inferences from the data that I have created from ANSYS.

So from the analysis what I am observing based off the material properties of the wing is that the full volume of the geometry of the wing can handle direct wind loads at top speeds of 593 miles per hour. In order to meet predefined weight requirements I would then further take structurally redundant mass out of the wing to develop its architecture.

I would like to add an engine mount as well as the inner architecture to the wing

This is just from the mid-span to the wing-lets, not the full wing.