Ashby Chart Visualizer Back
Materials Engineering

Material Selection Ashby Chart Visualizer

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.

Axis & Display
X-Axis Property
Y-Axis Property
Preset Charts
Material Class Filter
Click or hover a data point to show material properties
Ashby
Theory & Key Formulas

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.

What is an Ashby Chart?

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What exactly is this chart with all the bubbles? It looks like a map of materials, but why are the axes on a log scale?
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Great observation! This is an Ashby chart, a fundamental tool in materials selection. Basically, it plots Young's Modulus (stiffness, $E$) against density ($\rho$) on log-log axes. The log scale lets us see data spanning many orders of magnitude—like the difference between a soft foam and stiff steel—all on one clear plot. Try selecting different "Material Families" in the simulator to see how groups like metals, polymers, and ceramics cluster together.
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Wait, really? So it's just a map. How does it help me choose a material for, say, a lightweight bike frame?
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Exactly! The map becomes a selection tool when we add performance lines. For a lightweight, stiff beam (like that bike frame), the key is the index $E^{1/2}/\rho$. On this log-log plot, that index creates a line with a slope of 2. In the simulator, choose "Stiff Lightweight Beam" from the "Performance Index" dropdown. You'll see a line appear. Materials above and to the left of this line are better—they give more stiffness per unit weight. Notice how carbon fiber composites (CFRP) soar above aluminum and steel!
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That makes sense! But what if my part isn't a beam? What if it's just a rod being pulled—a "tie"? Does the rule change?
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Excellent question! The physics changes completely. For a tie (in pure tension), the goal is to maximize stiffness per weight, which is simply $E/\rho$. This gives a performance line with a slope of 1. Switch the simulator's dropdown to "Stiff Lightweight Tie" and watch the line rotate. Now, materials like ceramics and diamond, which are very stiff but brittle, shoot up the ranking for this specific job. It's a perfect example of how the loading dictates the best material.

Physical Model & Key Equations

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.

Frequently Asked Questions

From the dropdown menu at the top of the screen, you can select the material properties (such as Young's modulus, density, strength, fracture toughness, etc.) to assign to the X-axis and Y-axis. When you switch axes, the plot and performance index guidelines are automatically recalculated.
The guidelines indicate the performance index for a specific design goal (e.g., a lightweight stiff beam). Materials located to the upper left of the line have a higher performance index and are more suitable for that design. The slope corresponds to the formula of the performance index (e.g., a slope of 2 for E^1/2/ρ).
The chart shows representative (average) values of materials and does not reflect processing conditions, temperature dependence, cost, or availability. When selecting materials, be sure to check the detailed data sheets of candidate materials and verify their properties under actual operating conditions.
Hovering the mouse cursor over each point (material family) on the plot will display a tooltip showing the family name and representative material examples. Clicking on a point will open a separate window with a list of property values for individual materials belonging to that family.

Real-World Applications

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.

Common Misunderstandings and Points to Note

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.

How to Use

  1. Select material families (aluminum alloys, carbon fiber composites, titanium, steel, polymers) from the left panel
  2. Choose axes: stiffness (E in GPa) vs. density or strength (σ_y in MPa) vs. density on log-log scales
  3. Drag selection box across the chart to highlight materials in target performance envelopes; hover over points to read Young's modulus, yield strength, and density values
  4. Apply performance index filters (E/ρ for beams under bending, σ_y/ρ for ties under tension) to shade feasible material regions

Worked Example

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.

Practical Notes

  1. For aerospace tie members (tension-critical), prioritize high (σ_y/ρ): titanium alloys (σ_y ≈ 900 MPa, ρ ≈ 4500 kg/m³) and carbon composites (σ_y ≈ 1400 MPa, ρ ≈ 1600 kg/m³) outperform steel by 2–3×
  2. Composite materials exhibit property anisotropy; input fiber-aligned values for predictions and validate with laminate theory for multi-directional layups
  3. Cost and manufacturing constraints: aluminum 5083-H321 (marine, corrosion-resistant) trades stiffness (E = 69 GPa) for weldability; specify material grade and condition (T6, H321) when finalizing designs