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Material Selection Index Strength⚠ unverified

Mechanical / Materials · Compute the strength-limited material selection index

Parameters

InputSymbolUnitDefaultDescription
SySyPa1.0Yield strength of the material
rhoρkg/m**31.0Mass density of the material
OutputSymbolUnitDescription
resultMkg/m**3Strength-limited selection index, in pascals per (kg/m**3)

The science & history

Understanding the Parameters

Derivation (Approaching a Proof)

For a tension tie of fixed length $L$ carrying load $F$ without yielding, the minimum area is $A = F/S_y$ and the mass is

$$m = \rho A L = (F L)\,\frac{\rho}{S_y}.$$

With $F$ and $L$ fixed, mass is minimised by maximising $S_y/\rho$ — the same derivation as Specific Strength. The two cards compute the identical index.

Dimensional check. $M = \dfrac{S_y}{\rho} = \dfrac{\text{Pa}}{\text{kg}/\text{m}^3} = \dfrac{\text{J}}{\text{kg}}$ — energy per mass, confirming the registry's kg/m³ label is incorrect.

History and Development

The strength index $S_y/\rho$ (or $\sigma_f/\rho$) is a core Ashby material-selection index (1980s), plotted as a slope-1 guideline on the strength–density Ashby Charts. It drove the adoption of aluminium and composites in aircraft primary structure, where strength-per-weight, not absolute strength, is the binding constraint.

Related Concepts: Specific Strength, Material Selection Index Stiffness, Ashby Chart Index, Ashby Charts, Material Selection Index Toughness, Hardness to Tensile Strength

Notes: Duplicate of Specific Strength ($S_y/\rho$). Output unit should be J/kg (registry mislabels kg/m³). Tie index — bending-limited members use $S_y^{2/3}/\rho$.

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