Hello,
I have an area out question.
On my (hypothetical) airplane control surface, some corrosion was discovered and trimmed out.
To determine the area loss/capability, is it the thickness of the material times the length (or width) of the trimmed surface?
So if the material was .063 inches...
Hello!
Does anyone remember a software that was available for purchase a few years ago, called Cynapsis or Cynaptics? It was for sale, and marketed with capabilities of analyzing fastener loads, bending moments, and aircraft seat track loads.
Thanks.