tom787
Aerospace
- Oct 5, 2006
- 5
For metallic lugs design guidelines are available (eg. Niu). However, these can not be directly used in composite lugs.
Does anybody know of design guidelines or methods to analyze composite lug?
I am analyzing a 3D composite (carbon/epoxy) lug.
This thick laminated lug (17.5 mm) has a hole with a spherical bearing installed. The lug consists of 50 plies of SM_5H_Satin fabric. The lay-up is quasi isotropic.
The analyses were performed using finite element method (I am still looking for correct 3D material values see thread327-228660). Later, we will perform physical tests to correlate the results.
The papers that are referenced in thread181-27567 are interesting but do not give sufficient answer.
Regards, Tom.
Does anybody know of design guidelines or methods to analyze composite lug?
I am analyzing a 3D composite (carbon/epoxy) lug.
This thick laminated lug (17.5 mm) has a hole with a spherical bearing installed. The lug consists of 50 plies of SM_5H_Satin fabric. The lay-up is quasi isotropic.
The analyses were performed using finite element method (I am still looking for correct 3D material values see thread327-228660). Later, we will perform physical tests to correlate the results.
The papers that are referenced in thread181-27567 are interesting but do not give sufficient answer.
Regards, Tom.