Calculate Flexural Modulus Calculator

Enter your engineering parameters below to compute verified physical and mathematical metrics.

Mid-span concentrated bending load in Newtons (e.g. 500 N).
Distance between 3-point bending supports in mm (e.g. 100 mm).
Specimen cross-sectional width in millimeters (e.g. 10 mm).
Specimen cross-sectional depth in millimeters (e.g. 4 mm).
Measured mid-span deflection in millimeters (e.g. 1.2 mm).

Calculation Results

Primary Metric Output --
Metric Breakdown 1 --
Metric Breakdown 2 --
Metric Breakdown 3 --
Metric Breakdown 4 --
Metric Breakdown 5 --
Mathematical Standard --

Calculated using verified physical methodology: Flexural Modulus: E_f = \F \cdot L^3 / 4 \cdot b \cdot d^3 \cdot \delta
Outer Fiber Bending Stress: \sigma_f = \3 \cdot F \cdot L / 2 \cdot b \cdot d^2 Outer Fiber Bending Strain: \epsilon_f = \6 \cdot \delta \cdot d / L^2

*Note: Results represent standard engineering estimates. Validate with structural codes (AISC, Eurocode) or laboratory test measurements for mission-critical applications.

Quick Summary

The Flexural Modulus Calculator evaluates 3-point bending flexural stiffness ($E_f = \F \cdot L^3 / 4 \cdot b \cdot d^3 \cdot \delta$) for rectangular plastic, composite, wood, and metal specimens according to ASTM D790 / ISO 178 testing standards.

Formula Explanation

Flexural Modulus: E_f = \F \cdot L^3 / 4 \cdot b \cdot d^3 \cdot \delta
Outer Fiber Bending Stress: \sigma_f = \3 \cdot F \cdot L / 2 \cdot b \cdot d^2 Outer Fiber Bending Strain: \epsilon_f = \6 \cdot \delta \cdot d / L^2

How It Works

The Flexural Modulus Calculator applies 3-point bending beam theory (ASTM D790). It multiplies bending force ($F$) by the cube of span length ($L^3$), dividing by $4 \cdot b \cdot d^3 \cdot \delta$. It outputs Flexural Modulus ($E_f$) in GPa and Mpsi alongside maximum outer fiber flexural stress ($\sigma_f$) and flexural strain ($\epsilon_f$).

Step-by-Step Worked Example

Practical Problem: Calculate flexural modulus for a rectangular plastic test bar ($b = 10\text{ mm}$, $d = 4\text{ mm}$, span $L = 100\text{ mm}$) subjected to a 500 N load that deflects by 1.20 mm.

  1. Step 1: Identify Input Parameters: Bending Force $F = 500\text{ N}$, Span $L = 100\text{ mm}$, Width $b = 10\text{ mm}$, Depth $d = 4\text{ mm}$, Deflection $\delta = 1.20\text{ mm}$.
  2. Step 2: Calculate Maximum Outer Fiber Flexural Stress ($\sigma_f$): $\sigma_f = \3 \cdot F \cdot L / 2 \cdot b \cdot d^2 = \3 \times 500 \times 100 / 2 \times 10 \times 16 = \150,000 / 320 = 468.75\text{ MPa}$.
  3. Step 3: Calculate Maximum Outer Fiber Flexural Strain ($\epsilon_f$): $\epsilon_f = \6 \cdot \delta \cdot d / L^2 = \6 \times 1.20 \times 4 / 10,000 = \28.8 / 10,000 = 0.00288$ ($2,880\text{ }\mu\epsilon$).
  4. Step 4: Execute Flexural Modulus Division: $E_f = \\sigma_f / \epsilon_f = \468.75 / 0.00288 = 162,760.42\text{ MPa} = 162.76\text{ GPa}$. Alternatively using formula: $E_f = \500 \times 1,000,000 / 4 \times 10 \times 64 \times 1.20 = \500,000,000 / 3,072 = 162.76\text{ GPa}$.
  5. Step 5: Convert and Interpret Imperial Metric Outputs: Flexural Modulus $E_f = 162.76\text{ GPa}$. Imperial Mpsi: $162.76 \times 0.145038 = 23.61\text{ Mpsi}$.

Real-World Calculation Examples

Scenario 1: Glass-Reinforced Nylon Composite Bar

Parameters: $F = 500\text{ N}$, $L = 100\text{ mm}$, $b = 10\text{ mm}$, $d = 4\text{ mm}$, $\delta = 1.2\text{ mm}$

Result: $E_f = 162.76\text{ GPa}$ (23.61 Mpsi). Structural composite bending modulus.

Scenario 2: Unreinforced ABS Thermoplastic Bar

Parameters: $F = 50\text{ N}$, $L = 64\text{ mm}$, $b = 12.7\text{ mm}$, $d = 3.2\text{ mm}$, $\delta = 1.5\text{ mm}$

Result: $E_f = 2.14\text{ GPa}$ (0.31 Mpsi). ASTM D790 ABS plastic flexural modulus.

Scenario 3: Carbon Fiber Composite Automotive Panel

Parameters: $F = 200\text{ N}$, $L = 100\text{ mm}$, $b = 15\text{ mm}$, $d = 2\text{ mm}$, $\delta = 1.0\text{ mm}$

Result: $E_f = 416.67\text{ GPa}$ (60.43 Mpsi). Ultra-high modulus carbon laminate.

Scenario 4: Structural Hardwood Oak Timber Strip

Parameters: $F = 800\text{ N}$, $L = 300\text{ mm}$, $b = 20\text{ mm}$, $d = 10\text{ mm}$, $\delta = 4.0\text{ mm}$

Result: $E_f = 13.50\text{ GPa}$ (1.96 Mpsi). Structural hardwood flexural stiffness.

Key Benefits of Using This Calculator

ASTM D790 & ISO 178 Compliance

Uses standard 3-point flexural test mechanics for plastics, polymers, and composites.

Bending Stress & Strain Breakdown

Calculates maximum outer fiber bending stress ($\sigma_f$) and flexural strain ($\epsilon_f$) simultaneously.

Dual GPa & Imperial Mpsi Units

Provides flexural modulus in GPa, MPa, and Imperial Mpsi ($10^6\text{ psi}$).

100% Free & Private

Runs locally inside your web browser with real-time recalculation as inputs change.

Frequently Asked Questions (FAQ)

What is Flexural Modulus?

Flexural Modulus (Ef) is a material property measuring resistance to bending deformation in 3-point or 4-point flexural tests.

What is the formula for Flexural Modulus in 3-point bending?

Ef = (F * L³) / (4 * b * d³ * delta), where F is load, L is support span, b is specimen width, d is depth, and delta is deflection.

How does Flexural Modulus differ from Tensile Young's Modulus?

Tensile modulus evaluates pure axial tension; flexural modulus evaluates bending stiffness where top fibers are in compression and bottom fibers are in tension. For homogeneous isotropic materials, Ef equals E.

Why is Flexural Modulus widely used for plastics and composites?

Plastic components in real applications usually experience flexural bending rather than pure axial tension; 3-point bending tests are also much easier to clamp and perform.

What is the difference between 3-point bending and 4-point bending?

3-point bending creates maximum bending moment at the center load point; 4-point bending creates uniform bending moment across the middle third of the span.

How converts GPa to Mpsi?

Multiply GPa by 0.145038 to obtain Mpsi (e.g. 10 GPa = 1.45 Mpsi).

What is maximum outer fiber flexural stress sigma_f?

sigma_f = (3 * F * L) / (2 * b * d²), representing maximum tensile stress on the convex outer surface during 3-point bending.

What is maximum outer fiber flexural strain epsilon_f?

epsilon_f = (6 * delta * d) / L², measuring maximum outer surface strain corresponding to mid-span deflection delta.

Why does specimen depth d have a cubic effect (d³) on flexural stiffness?

Moment of inertia for a rectangular section is I = b*d³/12. Since bending stiffness is proportional to I, doubling depth d increases flexural rigidity 8-fold.

What testing standards govern flexural modulus calculation?

ASTM D790 (plastics and electrical insulation materials) and ISO 178 (flexural properties of plastics).