Is there a solution for compression of cylinder?

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Discussion Overview

The discussion revolves around the problem of axial compression of an elastic cylinder, specifically seeking to determine the stress and strain in the axial direction. Participants explore the theoretical underpinnings and potential references for analytical expressions related to this scenario.

Discussion Character

  • Exploratory
  • Technical explanation
  • Debate/contested

Main Points Raised

  • One participant expresses difficulty in finding references for the axial compression of a full elastic cylinder and seeks analytical expressions.
  • Another participant suggests that the problem is akin to column compression, noting that the cross-section's shape primarily affects area considerations.
  • A later reply reiterates the initial inquiry, framing the compressive strain as the compressive stress divided by Young's modulus, drawing a parallel to tension scenarios.
  • One participant posits that finding an analytical expression for elastic behavior may be complex and potentially require advanced computational resources.
  • Another participant questions the specific challenges of the problem and outlines several assumptions necessary for standard solutions, including the cylinder's dimensions relative to its diameter and the nature of the applied force.
  • This participant also highlights that the referenced material may pertain to failure conditions rather than non-destructive loading scenarios.

Areas of Agreement / Disagreement

Participants do not reach a consensus on the availability of analytical solutions or the specific challenges of the problem. Multiple viewpoints regarding the assumptions and complexity of the scenario remain present.

Contextual Notes

Participants mention several assumptions that affect the problem's tractability, including the cylinder's length relative to its diameter, the nature of the applied force, and the isotropy of the material. These factors may limit the applicability of standard solutions.

Mugged
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Hello,

for some reason I can't seem to be able to find this.

Suppose you have a elastic cylinder, a full cylindrical bar (not hollow), and you want to compress the two end faces (axial compression) together and find the stress in the axial direction...or strain.

I can't seem to be able to find this problem posed anywhere in a google search and it seems easy enough for there to be a textbook analytical expression.

anyone know of any references?

Thank you
 
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Mugged said:
Hello,

for some reason I can't seem to be able to find this.

Suppose you have a elastic cylinder, a full cylindrical bar (not hollow), and you want to compress the two end faces (axial compression) together and find the stress in the axial direction...or strain.

I can't seem to be able to find this problem posed anywhere in a google search and it seems easy enough for there to be a textbook analytical expression.

anyone know of any references?

Thank you

This is the same problem of a bar in tension, except that the imposed tension stress is negative. The compressive strain is just the compressive stress divided by Young's modulus.
 
Last edited:
If its elastic than you probably won't find an analytical expression that doesn't require a supercomputer to solve.
 
Mugged, what is special about your cylinder or axial loading that makes this problem difficult?

The answer by Mech_Engineer is one of the first things in any mechanics of materials book.

However this assumes several things.

Firstly that the cylinder axis is long compared to its diameter

Secondly that the applied force is (sensibly) normal to the end faces

Thirdly that the applied force is applied via a large stiff plate, larger than the diameter of the cylinder

Fourthly that the cylinder is not restrained from expansion along its curved surfaces

Fifthly that the material is isotropic

Please note one more thing about Mech_eng link.
The link refers to failure, where stresses are different.
I presume you are asking about a non destructive load?

The problem is still tractable however, Aero51 is over the top with his suggestion.
 

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