Q4. (a) Calculate the ply reduced stiffness matrix, [Q], for a specially orthotropic ply having the...
2.15 The reduced stiffness matrix [Q] is given for a unidirectional lamina is given as follows: by Taylor & Francis Group, LLC Mechanics of Composite Materials, Second Edition 170 5,681 0.3164 0 Msi Q]= 0.3164 1.217 0 0 0 0.6006 What are the four engineering constants, E E, v12, and G12, of the lamina? 2.15 The reduced stiffness matrix [Q] is given for a unidirectional lamina is given as follows: by Taylor & Francis Group, LLC Mechanics of Composite Materials,...
please solve 2 and 3 1- The reduced stiffness matrix [Q] is given for a unidirectional lamina as follows: 5.681 0.3164 0 ] [Q]=0.3164 1.217 0 Msi I 0 0 0.6006 Calculate the four engineering constants E1, E2, V12, G12 of the lamina. 2- Calculate the transformed reduced stiffness [Q] for the above problem for 0 = 30°. Glass 3- A glass/epoxy lamina consists of 70% fiber volume fraction. Use properties of glass and epoxy from the tables below to...
I need help with question 6.18 Macromechanics 215 N, 1000 N/m; all remaining components are equal to zero b) Mry 1 Nm/m; all remaining components are equal to sero ) Comment on the coupling efects obsereed 6.12 Compute the strains ( (y, and ry at the interface between the 459 and laminae above the middle surface by using the results of case (b) of Ezercise 6.11 and -45 /a.e3 6.23). cise 6.13 Compute the stresses ơz and σ1 in the...