The shape of a laminated composite structure is optimized using finite element analysis. The optimized shape minimizes the weight of the structure while satisfying minimum strength and stiffness requirements.
申请公布号
WO2010025413(A2)
申请公布日期
2010.03.04
申请号
WO2009US55433
申请日期
2009.08.28
申请人
THE BOEING COMPANY;HUNTER, ETHAN W.;FALASCO, THOMAS J.;SWANSON, KURT M.
发明人
HUNTER, ETHAN W.;FALASCO, THOMAS J.;SWANSON, KURT M.
