O. Orlova
DOI Number: N/A
Conference number: IFASD-2015-053
Designing of an elastically scaled model of a high aspect ratio wing, which made using of digital technologies is considered. Model is made on the basis of rigid core and polymeric material with low modulus of elasticity. It is possible to use numerical control (NC) machines or 3D – printers during manufacturing. The search of required construction is carried out on the basis of finite element method (FEM) with the aid of optimization through influence coefficient matrix.