The change in length of the member assuming an original, Mechanical Engineering

The change in length of the member assuming an original

A tensile member of 2024-0 aluminum alloy used for aircraft fuselage had an original cross-sectional area of 4.0square inches. If the strain hardening exponent, n=0.21 and the strength coefficient Q=56,000 psi, determine:
a) The maximum load that can be carried by the member?
b) The change in length of the member assuming an original length of 4.0 feet?

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Mechanical Engineering: The change in length of the member assuming an original

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Request for Solution File

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Mechanical Engineering: The change in length of the member assuming an original

Reference No:- TGS0428871

Have a Question? (oR Write a Review)

Recent Questions Asked Mechanical Engineering

Q : What is the new pressure inside the container

Q : Calculate the force on the piston

Q : Determine what volume would methane occupy

Q : Find out the final temperature of the mixture

Q : The change in length of the member assuming an original

Q : What is the freezing-point depression of the solvent

Q : Moles of ar present

Q : How much oxygen gas is needed for this reaction

Q : What is the average thickness of the sheet in meters

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Request for Solution File

Ask an Expert for Answer!!

Mechanical Engineering: The change in length of the member assuming an original

Reference No:- TGS0428871

Recent Questions Asked Mechanical Engineering

Q : What is the new pressure inside the container

Q : Calculate the force on the piston

Q : Determine what volume would methane occupy

Q : Find out the final temperature of the mixture

Q : The change in length of the member assuming an original

Q : What is the freezing-point depression of the solvent

Q : Moles of ar present

Q : How much oxygen gas is needed for this reaction

Q : What is the average thickness of the sheet in meters

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