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Question

Euler's formula holds good only for-

The correct answer is

Long columns

Understanding Euler's Formula for Column Buckling

Euler's formula is a critical concept in structural mechanics, specifically used to determine the critical buckling load for a slender column. Buckling is a form of structural instability where a straight column under axial compression suddenly deflects laterally.

The question asks for which type of column Euler's formula holds good. Let's break down the conditions under which this formula is applicable.

Applicability of Euler's Formula

Euler's buckling formula is derived based on several assumptions, the most important of which is that the column is perfectly straight, made of a homogeneous elastic material, and importantly, it is long enough to fail by elastic buckling before the material reaches its yield strength.

  • Long Columns: These columns have a high slenderness ratio. When subjected to an axial compressive load, they fail by buckling elastically. Euler's formula is specifically developed to predict this elastic buckling load.
  • Short Columns: These columns have a low slenderness ratio. They are stocky and tend to fail by crushing or yielding of the material under the compressive load, rather than by elastic buckling.
  • Intermediate Columns: These columns fall between short and long columns. Their failure mode is a combination of yielding and buckling. Euler's formula is not suitable for these columns because it assumes purely elastic buckling. Other formulas, like Rankine-Gordon or Johnson's parabolic formula, are used for intermediate columns.

Therefore, the fundamental condition for applying Euler's formula is that the column must be sufficiently long so that its failure is governed by elastic buckling.

Analyzing the Options

Let's consider the given options in light of the applicability criteria for Euler's formula:

  • Weak columns: "Weakness" isn't a specific geometric classification like short or long. A column's strength depends on material properties, cross-sectional area, and length. Euler's formula deals with buckling failure, which is more pronounced in slender (long) columns regardless of material 'weakness' in the sense of low yield strength, as long as it remains elastic.
  • Short columns: As discussed, short columns fail by crushing or yielding, not elastic buckling. Euler's formula is not applicable here.
  • Both short and long columns: This is incorrect because Euler's formula is derived for elastic buckling, which is the failure mode for long columns, not short columns.
  • Long columns: This aligns perfectly with the assumption of Euler's formula, which is based on elastic buckling failure characteristic of long, slender columns.

Based on the derivation and assumptions, Euler's formula for the critical buckling load (\(P_{cr}\)) of a column is given by:

\(P_{cr} = \frac{\pi^2 EI}{(KL)^2}\)

Where:

  • \(P_{cr}\) is the critical buckling load
  • \(E\) is the modulus of elasticity of the column material
  • \(I\) is the minimum moment of inertia of the column's cross-section
  • \(L\) is the original length of the column
  • \(K\) is the column effective length factor, which depends on the boundary conditions (how the ends of the column are supported). \(KL\) is the effective length.

This formula predicts the load at which a long column will buckle elastically. It does not account for failure by yielding, which is typical for short columns.

Conclusion

Euler's formula is derived based on the assumption of elastic buckling and is therefore applicable only to long columns where this failure mode occurs before yielding.

Column Type Failure Mode Applicable Formulas
Short Columns Crushing / Yielding Compressive Yield Strength based calculations
Intermediate Columns Combined Buckling and Yielding Rankine-Gordon, Johnson's Parabolic Formula
Long Columns Elastic Buckling Euler's Formula

Revision Table: Euler's Formula and Column Types

Feature Short Columns Long Columns
Slenderness Ratio Low High
Primary Failure Mode Crushing/Yielding Elastic Buckling
Applicable Buckling Formula Generally Not Euler's Euler's Formula
Stress Distribution at Failure Uniform or near uniform compression Combination of bending stress and compression, elastic range

Additional Information on Column Buckling

Understanding column buckling requires grasping the concept of the slenderness ratio (\(\lambda\)), which is a key parameter determining whether a column is considered short, intermediate, or long. It is defined as:

\(\lambda = \frac{KL}{r}\)

Where:

  • \(K\) is the effective length factor
  • \(L\) is the actual length
  • \(r\) is the minimum radius of gyration of the cross-section (\(r = \sqrt{I/A}\), where \(A\) is the cross-sectional area)

The critical slenderness ratio that distinguishes between column types depends on the material's properties, specifically its Young's modulus (\(E\)) and yield strength (\(\sigma_y\)). The critical slenderness ratio (\(\lambda_c\)) below which Euler's formula is not valid can be approximated by:

\(\lambda_c = \sqrt{\frac{\pi^2 E}{\sigma_y}}\)

Columns with a slenderness ratio significantly higher than \(\lambda_c\) are considered long and fail by elastic buckling according to Euler's formula. Columns with a slenderness ratio much lower than \(\lambda_c\) are short and fail by yielding.

The effective length factor \(K\) accounts for different end conditions, influencing the buckling mode shape and critical load:

  • Pinned-Pinned (Hinged at both ends): \(K=1\)
  • Fixed-Fixed (Restrained at both ends): \(K=0.5\)
  • Fixed-Pinned: \(K \approx 0.7\)
  • Fixed-Free (Cantilever): \(K=2\)

These factors modify the column's length in the buckling calculation, representing the length of an equivalent pinned-pinned column.

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Important Questions from Columns

  1. The slenderness ratio of a column, which indicates its susceptibility to buckling, is calculated by dividing its effective length by its:
  2. Effective length of a column is the length between the points of

  3. A structural column characterized by a high slenderness ratio is primarily susceptible to what mode of failure under axial compressive loading?
  4. Which structural member is primarily designed to resist loads perpendicular to its longitudinal axis, causing bending moments and shear forces?

  5. For a column of length (L) and flexural rigidity (EI) which has one end fixed and other end free, the expression for critical load is given as -

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