P1.2. The material of a tension member is changed from AISI 4340 steel to a unidirectional high-modulus (HM) carbon fiber-reinforced epoxy 1. Calculate the ratio of the cross-sectional areas, axial stiffnesses, and weights of these two members for equal load-carrying capacities 2. Calculate the ratio of the cross-sectional areas, load-carrying cap- acities, and weights of these two members for equal axial stiffness (Hint: Load strength× cross-sectional area, and axial stiffness modulus × cross-sectional area)

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P1.2. The material of a tension member is changed from AISI 4340 steel to a unidirectional high-modulus (HM) carbon fiber-reinforced epoxy 1. Calculate the ratio of the cross-sectional areas, axial stiffnesses, and weights of these two members for equal load-carrying capacities 2. Calculate the ratio of the cross-sectional areas, load-carrying cap- acities, and weights of these two members for equal axial stiffness (Hint: Load strength× cross-sectional area, and axial stiffness modulus × cross-sectional area)

P1.2. The material of a tension member is changed from AISI 4340 steel to a unidirectional high-modulus (HM) carbon fiber-reinforced epoxy 1. Calculate the ratio of the cross-sectional areas, axial stiffnesses, and weights of these two members for equal load-carrying capacities 2. Calculate the ratio of the cross-sectional areas, load-carrying cap- acities, and weights of these two members for equal axial stiffness (Hint: Load strength× cross-sectional area, and axial stiffness modulus × cross-sectional area)

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Fernando01 2025-02-08T19:33:10+05:00 1 Answer 22 views Beginner
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  1. Mechanical Engineering Expert
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    2025-02-08T20:59:54+05:00
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