Question

Answer at the bottom

4.3 A laminate of 0.015 in. thickness under a complex load gives the following midplane strains and curvatures: 2x10-6 4x10-6 κ, | | 1.2×10-4 к, | | 1.5 x10-41 1/in. 2.6x10 ry aylor & Francis Group, LLC Macromechanical Analysis of Laminates 365 Find the global strains at the top, middle and bottom surface of the laminate. 4.3 Given for a laminate under a complex load Global strains at top surface of laminate 1.100 106 60 1.875-106 2.050-106 in Global strains at middle surface of laminate 6 2-10 1 3.10 4-10 6in in Global strains at bottom surface of laminate 2.9x 106 4.125 x 106 in in 5.950 x 10

Answer 1

nSun사 ueu n)を huen mid lau Stans au kx Is qven land uita lb on a (a o bal Stalw g

0.0035 , 2 6 X 10 5:95 X to Y, axID Ex