In structural engineering, the slenderness ratio of a compression member is defined as the ratio of its effective length to its least radius of gyration, used to assess buckling tendency.

Difficulty: Easy

Correct Answer: Effective length / least radius of gyration (L_eff / r_min)

Explanation:


Introduction / Context:
In steel and reinforced concrete design, compression members such as columns can fail by buckling well before the material reaches its compressive strength. The key non-dimensional parameter that signals buckling vulnerability is the slenderness ratio, which compares a member's effective length to its least radius of gyration.


Given Data / Assumptions:

  • Member carries primarily axial compression.
  • Effective length L_eff accounts for end restraints (fixed, pinned, free, etc.).
  • r_min is the least radius of gyration among the principal axes.


Concept / Approach:
The radius of gyration r about an axis is r = sqrt(I/A). Slenderness ratio is defined as lambda = L_eff / r. Buckling is more likely as lambda increases; therefore the least radius of gyration r_min must be used because buckling occurs about the weakest (least stiff) axis.


Step-by-Step Solution:
Define r = sqrt(I/A)Identify r_min among available axesCompute L_eff based on boundary conditions (for example, pinned-pinned: L_eff = L; fixed-free: L_eff = 2L)Slenderness ratio lambda = L_eff / r_min


Verification / Alternative check:
If end conditions are changed, only L_eff changes; the expression remains L_eff / r_min, confirming the definition is independent of material strength and depends purely on geometry and restraint.


Why Other Options Are Wrong:

  • r_min / L_eff reverses the definition and would decrease with increasing slenderness, which contradicts buckling behavior.
  • A / I and I / A are unrelated ratios; they neither include length nor capture end restraint effects.


Common Pitfalls:

  • Using actual length L instead of effective length L_eff.
  • Using radius of gyration about the strong axis rather than the least (critical) axis.


Final Answer:
Effective length / least radius of gyration (L_eff / r_min)

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