Question 6 (a) The configuration of a carbon-epoxy laminate is (0/90), with a ply thickness of 2mm. Form the A, B and D

Business, Finance, Economics, Accounting, Operations Management, Computer Science, Electrical Engineering, Mechanical Engineering, Civil Engineering, Chemical Engineering, Algebra, Precalculus, Statistics and Probabilty, Advanced Math, Physics, Chemistry, Biology, Nursing, Psychology, Certifications, Tests, Prep, and more.
Post Reply
answerhappygod
Site Admin
Posts: 899603
Joined: Mon Aug 02, 2021 8:13 am

Question 6 (a) The configuration of a carbon-epoxy laminate is (0/90), with a ply thickness of 2mm. Form the A, B and D

Post by answerhappygod »

Question 6 A The Configuration Of A Carbon Epoxy Laminate Is 0 90 With A Ply Thickness Of 2mm Form The A B And D 1
Question 6 A The Configuration Of A Carbon Epoxy Laminate Is 0 90 With A Ply Thickness Of 2mm Form The A B And D 1 (136.45 KiB) Viewed 18 times
Question 6 (a) The configuration of a carbon-epoxy laminate is (0/90), with a ply thickness of 2mm. Form the A, B and D matrices and ascertain if the laminate possesses the following properties. (i) (ii) (iii) (iv) in-plane isotropy in-plane orthotropy bending isotropy bending orthotropy [15 marks] (b) The reduced stiffness matrix of a unidirectional carbon-epoxy is given by 200 3 0 Q= 3 100 kN/mm² 0 05 Given the stress system in the reference axes (X - Y) as Ox = 150N/mm², Oy = 50 N/mm² and Txy = 75 N/mm², determine the stress system in the material axes (1-2) when 0, the angle between the reference X-axis with the fibre axis, is 60°. [5 marks] (c) Determine the elastic constants E1, E2, G12 and V12 of a unidirectional ply given the a stiffness matrix as follows [5 marks] [40.51 2.03 0 [Q]= 2.03 8.10 0 GPa 0 0 5
Join a community of subject matter experts. Register for FREE to view solutions, replies, and use search function. Request answer by replying!
Post Reply