Concept of aspect ratio

spaceframe
2 min readFeb 28, 2024

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The length-to-finish ratio is an important concept in structural engineering design for assessing the stability of a member under stress.

Derived from Euler’s formula, the application of the slenderness ratio has become more sophisticated through a history of successful or failed engineering cases and continuous technological advances.

Euler’s formula is the formula used in structural engineering to calculate the buckling critical load of slender columns under axial compression. It is the key to understanding the stability of slender members.

Euler’s formula to study the stability model of short and long columns

Pcr=(KL)2π2EI

- ( Pcr) is the buckling critical load (i.e., the maximum vertical force that the member can withstand before it becomes unstable).

- ( E ) is the modulus of elasticity of the material.

- ( I ) is the moment of inertia of the member section.

- ( K ) is the effective length factor.

  • ( L ) is the actual length of the member

Relation of length-to-finish ratio to Euler’s formula:

For straight bars, the length-to-finish ratio is defined as the effective length of the member divided by its radius of gyration. (For plate shells, the aspect ratio is defined as the length of the plate divided by its thickness.)

λ=iKL

The radius of gyration is determined by the moment of inertia of the cross-section and the cross-sectional area. i=AI

Substituting these two into Euler’s formula gives the relationship between the buckling critical load and the length-to-slenderness ratio:

Pcr=(KL)2π2EAi2=λ2π2EA

This indicates that the larger the aspect ratio, i.e., the longer the member is, the smaller its buckling critical load is and the more likely it is to be unstable.

The slenderness ratio is also considered to be one of the stability parameters that contribute the most to the application of Euler’s formula to engineering design.

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spaceframe
spaceframe

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