Stiff lightweight beam: $M = E^{1/2}/\rho$
Strong lightweight beam: $M = \sigma_y^{2/3}/\rho$
Stiff lightweight tie: $M = E/\rho$
Materials above-left of a guideline line outperform those below-right.
Plot 30 material families on log-log axes. Switch X/Y axes freely to explore stiffness-weight, strength-weight, and fracture toughness trade-offs with performance index guidelines.
Stiff lightweight beam: $M = E^{1/2}/\rho$
Strong lightweight beam: $M = \sigma_y^{2/3}/\rho$
Stiff lightweight tie: $M = E/\rho$
Materials above-left of a guideline line outperform those below-right.
The core idea is to derive a Performance Index (M) that isolates the material properties for a given design goal (like minimum mass). For a lightweight beam in bending, we minimize mass while meeting a stiffness constraint.
$$ M = \frac{E^{1/2}}{\rho}$$Here, $E$ is Young's Modulus (stiffness), and $\rho$ is density. A higher $M$ means a lighter beam for the same stiffness. On a log-log plot of $E$ vs. $\rho$, lines of constant $M$ have a slope of 2, because $\log E = 2 \log \rho + \text{constant}$.
For a different loading case, like a lightweight tie (strut) in tension, the objective changes. Here, we minimize mass while meeting a strength (yield stress) constraint, leading to a different index.
$$ M = \frac{\sigma_y^{2/3}}{\rho}$$Here, $\sigma_y$ is the yield strength. For a stiff tie, where deflection is limited, the index becomes $M = E/\rho$, producing a slope of 1 on the Ashby chart. The slope of the performance line is the key visual filter for selection.
Aerospace Structural Frames: Airframe ribs and spars are beams in bending. Engineers use the $E^{1/2}/\rho$ index on Ashby charts to select materials like aluminum alloys, titanium, or carbon fiber composites to minimize weight while maintaining rigidity, directly impacting fuel efficiency.
High-Performance Bicycle Frames: The main triangle of a bike frame acts primarily as a beam. Material selection charts help designers choose between advanced aluminum, titanium, or carbon fiber, balancing the stiffness-to-weight ratio (governed by $E^{1/2}/\rho$) against cost and manufacturability.
Tension Members in Bridges & Cranes: Cables and tie rods are pure tension members. For these, the performance index is $E/\rho$ for stiffness or $\sigma_y/\rho$ for strength. This is why steel cables are common, but charts show where high-strength polymers or composites could offer weight savings.
Automotive Control Arms: Suspension components like control arms experience complex loads but often have bending-dominated behavior. Using the strong beam index ($\sigma_y^{2/3}/\rho$), engineers compare forged aluminum to high-strength steels to reduce unsprung mass, improving vehicle handling and efficiency.
When you start using this chart, there are a few common pitfalls to watch out for. First, don't judge a material solely by its position on the plot. The chart is primarily a first-pass screening tool. For example, while CFRP appears clearly superior to aluminum alloys on the lightweight stiff beam index, in actual design, factors not shown on the chart—like cost, manufacturability, corrosion resistance, and reliability data—are often decisive. That's why aluminum is frequently chosen.
Next, beware of pitfalls in axis selection. Even when we say "strength," there are different types: tensile strength, yield strength, fatigue strength, etc. For static loads, yield strength might be fine, but for components under cyclic loading, plotting with fatigue strength data is essential. When selecting "Strength" in this tool, be clear about the specific failure mode you are dealing with. Also, remember that the data represents typical values, and real materials have variability.
Finally, understand the meaning of the performance index slopes. The material ranking can reverse between a slope of 2 and a slope of 1.5. For instance, the index for a "lightweight stiff plate" is $M = E^{1/3} / \rho$, resulting in a line with a slope of 3. The optimal material changes between a beam and a plate. Therefore, clearly identify from the start whether your design is a "beam," a "plate," or a "tie," and use the corresponding guideline line.
Design a lightweight cantilever beam (L = 1.5 m, load F = 5 kN, maximum deflection δ_max = 3 mm). Steel (E = 200 GPa, ρ = 7850 kg/m³) requires I = 1.24×10⁻⁵ m⁴ and cross-section mass ≈ 14.8 kg/m. Aluminum 7075-T6 (E = 72 GPa, ρ = 2810 kg/m³) needs I = 3.44×10⁻⁵ m⁴ but delivers only 8.2 kg/m—a 45% weight saving. Carbon fiber epoxy (E = 140 GPa, ρ = 1600 kg/m³) achieves I = 1.76×10⁻⁵ m⁴ at 2.1 kg/m. The Ashby chart reveals the performance envelope: plot (E/ρ) for candidate materials and identify the upper-left region where stiffness-to-weight dominates.