jokerbenj
New member
- Oct 13, 2010
- 10
Dear engineers,
I trying to define guidelines for a stress engineer in aeronautic. We are making composite monuments for aircrafts/rotorcrafts. They are made with honeycomb panels (from Euro-Composite EC-PA-235G).
For the margin of safety calculation, what would you recommend to use: A-basis allowable strength values or B-basis?
By the way, does anyone have a clear datasheet of that panel?
Thanks for your coming answers!
Ben
I trying to define guidelines for a stress engineer in aeronautic. We are making composite monuments for aircrafts/rotorcrafts. They are made with honeycomb panels (from Euro-Composite EC-PA-235G).
For the margin of safety calculation, what would you recommend to use: A-basis allowable strength values or B-basis?
By the way, does anyone have a clear datasheet of that panel?
Thanks for your coming answers!
Ben