Axially loaded structural member problem

In summary, the conversation is about determining the maximum axial force that can be applied to a structural member made of solid round bar steel without causing the axial stress to exceed 175MPa or the total elongation to exceed 0.14% of its length. The correct answer is 343.5 KN, but the method to obtain it is uncertain. The topic of stress and pressure is also mentioned, as well as the need to multiply stress by area and consider the amount of steel stretch per Pa.
  • #1
Pepsi24chevy
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Hey guys, I need setting up this problem. Here it is:
A structural member is fabricated from a solid round bar of steel with a diameter D=50mm. If the member is 6.0m long, determine the maximum axial force that can be applied if the axial stress is not to exceed 175MPa and the total elongation is not to exceed 0.14& of its length.

I know the answer is 343.5 KN but i am unsure of how to get it. Thanks
 
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  • #2
Stress or Pressure [Pa] is Force per Area [N/m^2]
Did you try multiplying the stress by the Area?

Do you know how much the steel stretches per Pa?
 
  • #3


To solve this problem, we need to use the formula for axial stress, which is given by:

σ = F/A

Where σ is the axial stress, F is the applied force, and A is the cross-sectional area of the structural member.

First, we need to calculate the cross-sectional area of the steel bar using its diameter:

A = πr^2 = π(25mm)^2 = 1963.5 mm^2

Next, we need to determine the maximum force that can be applied without exceeding the given stress limit of 175 MPa. This can be done by rearranging the formula:

F = σA = (175 MPa)(1963.5 mm^2) = 343.5 kN

This is the maximum axial force that can be applied to the structural member without exceeding the given stress limit.

To ensure that the total elongation does not exceed 0.14% of the length, we can use the formula for total elongation:

ε = ΔL/L

Where ε is the total elongation, ΔL is the change in length, and L is the original length of the member.

In this case, we know that the total elongation should not exceed 0.14% of 6.0m, which is equal to 0.0084m. We can rearrange the formula to solve for the maximum change in length:

ΔL = εL = (0.0084m)(6.0m) = 0.0504m

Therefore, the maximum change in length that the member can experience without exceeding the given limit is 0.0504m.

To summarize, the maximum axial force that can be applied to the structural member is 343.5 kN, and the maximum change in length that the member can experience is 0.0504m. These values ensure that the axial stress does not exceed 175 MPa and the total elongation does not exceed 0.14% of the length.
 

FAQ: Axially loaded structural member problem

What is an axially loaded structural member problem?

An axially loaded structural member problem is a type of engineering problem that involves analyzing and designing a structural member, such as a beam or column, that is subjected to a compressive or tensile load along its axis. This type of problem is commonly encountered in civil and mechanical engineering applications.

What factors affect the behavior of an axially loaded structural member?

The behavior of an axially loaded structural member is influenced by several factors, including the material properties, cross-sectional dimensions, boundary conditions, and loading conditions. These factors can affect the member's ability to resist the applied load and its overall stability.

How is an axially loaded structural member problem solved?

To solve an axially loaded structural member problem, engineers use mathematical equations and principles of mechanics, such as equilibrium equations, stress-strain relationships, and geometric compatibility. These calculations help determine the internal forces, stresses, and deformations within the member, which can then be used to design a safe and efficient structure.

What are the different types of failure modes for an axially loaded structural member?

The most common failure modes for an axially loaded structural member are buckling, yielding, and rupture. Buckling occurs when the member cannot withstand the compressive load and deforms laterally, while yielding refers to the permanent deformation of the member due to excessive stress. Rupture, on the other hand, is the complete separation of the member due to tensile forces exceeding its strength.

How do engineers ensure the safety of an axially loaded structural member?

Engineers ensure the safety of an axially loaded structural member by performing thorough analysis and design calculations, taking into consideration all applicable codes and standards. They also conduct physical tests and simulations to validate the design and make any necessary adjustments. Additionally, regular inspections and maintenance are crucial to ensure the long-term safety and stability of the structure.

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