For a single lamina unidirectional composite, the on-axis elastic behavior is given by: • E1 = 140 GPa • E2=9GPA • v12=0.3 a) Calculate the reduced stiffness matrix, (Q] and the reduced compliance matrix, [S].
For a single lamina unidirectional composite, the on-axis elastic behavior is given by: • E1 = 140 GPa • E2=9GPA • v12=0.3 a) Calculate the reduced stiffness matrix, (Q] and the reduced compliance matrix, [S].
Chapter2: Loads On Structures
Section: Chapter Questions
Problem 1P
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Answer both parts in good handwriting for an upvote..(handwritten preferred).. thanks
![Macromechanical Analysis of a Angle
Lamina:
For a single lamina unidirectional
composite, the on-axis elastic behavior is
given by:
• E1 = 140 GPa
• E2=9GPA
• v12=0.3
a) Calculate the reduced stiffness matrix, [Q]
and the reduced compliance matrix, [S].
b) Calculate the state of strain when the
lamina is loaded by a shear stress of 10
MPa magnitude.](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F881981d6-3e02-4e67-b4bd-0ffa6ec9cc32%2F7ddd5688-8955-4ee8-963b-6172932bf9c1%2Fdc139p_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Macromechanical Analysis of a Angle
Lamina:
For a single lamina unidirectional
composite, the on-axis elastic behavior is
given by:
• E1 = 140 GPa
• E2=9GPA
• v12=0.3
a) Calculate the reduced stiffness matrix, [Q]
and the reduced compliance matrix, [S].
b) Calculate the state of strain when the
lamina is loaded by a shear stress of 10
MPa magnitude.
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