%0 Journal Article
%T The Design Algorithm of the Optimum Structure from the Elasticity Module Point of View for Composite Materials
%A Vasile MOGA
%A Bogdan Vasile MOGA
%J INCAS Bulletin
%D 2012
%I National Institute for Aerospace Research ˇ°Elie Carafoliˇ± - INCAS
%R 10.13111/2066-8201.2012.4.3.2
%X Unlike other researches in the field, the simultaneous influence of all structural elements on the elasticity module is studied in this paper. The obtained physical ¨C mathematical model is in good accordance with the experimental results and it can be used in practice by calculating, prior to the production, the values the structural elements must have so that the composite has a certain elasticity module. The model gives the opportunity of quick and exact determination of the values for the structural elements without experimental determinations and successive difficult calculations.The method of establishing the optimum structure presented here can be also used for other composites and other mechanical properties.
%K laminate composite materials
%K elasticity module
%K mathematical model
%K response surface
%K design algorithm
%K optimum structure
%U http://bulletin.incas.ro/files/moga_v-b_v_moga__v4_iss_3_full.pdf