Fig. 4From: Modelling of thermomechanical behaviour of fibrous polymeric composite materials subject to relaxation transition in the matrixErrors of stress calculation by (39) as a function of temperature (a) (notation is similar to that used in Fig. 3) and (b) of volume fraction of fibers. 1 – \( {E}_M^{(1)} \) = 0,001, \( {E}_M^{(2)} \) = 1; 2 – \( {E}_M^{(1)} \) = 10−4, \( {E}_M^{(2)} \) = 10−2; 1′,2′ – the same relations under heating conditionsBack to article page