Composite Wing Midplane FEM
Composite Wing Midplane FEM
(OP)
Hi, im wondering how to make a model of a complete composite wing, with "C" spar, and their skin by midplane analysis. To be more precise, the distance between the spar and skin midplane was 1cm (first aproximate), and i cant figure how to transfer loads/displacements from one to another.
Should i neglect that distance as an aproximation?
The chord is 0,80m and max tickness 13cm (0,13m)
I have access to Femap/Nastran.
Thanks in advance
Rick
Should i neglect that distance as an aproximation?
The chord is 0,80m and max tickness 13cm (0,13m)
I have access to Femap/Nastran.
Thanks in advance
Rick





RE: Composite Wing Midplane FEM
Cheers
Greg Locock
Please see FAQ731-376 for tips on how to make the best use of Eng-Tips.
RE: Composite Wing Midplane FEM
to much wondering.
Thanks Greg for rapid response.
Rick
RE: Composite Wing Midplane FEM
Rick
RE: Composite Wing Midplane FEM
Cheers
Greg Locock
Please see FAQ731-376 for tips on how to make the best use of Eng-Tips.
RE: Composite Wing Midplane FEM
Garland E. Borowski, PE
Borowski Engineering & Analytical Services, Inc.
www.borowskiengineering.com
RE: Composite Wing Midplane FEM
Thanks to GregLocock an GBor for the asistance.