A continuous-aligned composite lamina is to be designed to have Ec,L= 200 GPa, Ec,T = 10Q3.GPa and o*c,L = 500 MPa. The desired failure strength of the fiber and matrix are o*f = 1000 MPaand o'm = 20 MPa. Calculate the following to design a composite lamina of desired stiffness andstrength;(a) fiber and matrix volume fractions(b) fiber and matrix elastic modulus(c) load fractions of fiber-composite and matrix-composite(d) the calculated stiffness of fiber and matrix correspond closely to which type of fiber andmatrix materials

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A continuous-aligned composite lamina is to be designed to have Ec,L= 200 GPa, Ec,T = 10 Q3. GPa and o*cL = 500 MPa. The desired failure strength of the fiber and matrix are o*t = 1000 MPa and o'm = 20 MPa. Calculate the following to design a composite lamina of desired stiffness and strength; %3D %3D

A continuous-aligned composite lamina is to be designed to have Ec,L= 200 GPa, Ec,T = 10 Q3. GPa and ocL = 500 MPa. The desired failure strength of the fiber and matrix are ot = 1000 MPa and o'm = 20 MPa. Calculate the following to design a composite lamina of desired stiffness and strength; %3D %3D

Elements Of Electromagnetics

7th Edition

ISBN:9780190698614

Author:Sadiku, Matthew N. O.

Publisher:Sadiku, Matthew N. O.

ChapterMA: Math Assessment

Section: Chapter Questions

Problem 1.1MA

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