Free Beam Calculator

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Free Beam Deflection and Stress Calculator

Calculate the maximum deflection and bending stress for a simply supported beam under a uniformly distributed load.

N/m
meters
Pascals (Pa)
m4

Understanding the Free Beam Calculator

A "free beam" in structural engineering typically refers to a beam that is supported at both ends, allowing it to bend freely under load without significant restraint at the supports. This type of beam is commonly known as a simply supported beam. This calculator helps determine key structural parameters for such beams under a uniformly distributed load (UDL).

What it Calculates:

  • Maximum Deflection: The maximum vertical displacement of the beam from its original position. Excessive deflection can lead to aesthetic issues, damage to non-structural elements, and affect the serviceability of the structure.
  • Maximum Bending Stress: The peak stress experienced within the beam's cross-section due to bending. This is critical for ensuring the beam does not yield or fracture under load.

The Physics & Formulas:

For a simply supported beam subjected to a uniformly distributed load (w) over its entire length (L), the following formulas are standard in beam theory:

  • Maximum Deflection (δmax): occurs at the mid-span of the beam.
    Formula: δmax = (5 * w * L4) / (384 * E * I) Where:
    • w = Uniformly Distributed Load (Force per unit length, e.g., N/m)
    • L = Length of the beam (m)
    • E = Young's Modulus of the beam material (Pascals, Pa)
    • I = Moment of Inertia of the beam's cross-section (m4)
    The result is typically in meters (m).
  • Maximum Bending Stress (σmax): also occurs at the mid-span and at the top and bottom fibers of the beam's cross-section.
    Formula: σmax = (Mmax * y) / I First, the maximum bending moment (Mmax) for this load case is: Mmax = (w * L2) / 8 Then, assuming 'y' represents the distance from the neutral axis to the outermost fiber of the cross-section (this calculator simplifies by assuming a standard calculation using the total depth or similar property, but in practice, 'y' is derived from the cross-section geometry). For a general indication, we often relate stress to the section modulus (S = I/y) where σmax = Mmax / S. This calculator directly uses the maximum moment and provided Moment of Inertia (I) to indicate the bending intensity.
    For a simpler direct output related to the input moment of inertia: σmax ≈ (Mmax) / (I / yeffective) Note: For simplicity in this calculator, we'll output the maximum bending moment and relate it conceptually to stress, as the specific 'y' value (distance to extreme fiber) is not an input. A professional calculation would require cross-section dimensions. The result is typically in Pascals (Pa) or Megapascals (MPa).

How to Use This Calculator:

  1. Uniformly Distributed Load (w): Enter the total load spread evenly across the beam's length, in Newtons per meter (N/m).
  2. Beam Length (L): Input the total span of the beam in meters (m).
  3. Young's Modulus (E): Provide the material's stiffness. Common values include ~200 GPa (200 x 109 Pa) for steel and ~10 GPa (10 x 109 Pa) for wood.
  4. Moment of Inertia (I): Enter the beam's cross-sectional resistance to bending, in meters to the fourth power (m4). This value depends on the shape and dimensions of the beam's cross-section (e.g., I-beam, rectangular).
  5. Click "Calculate" to see the maximum deflection and bending moment.

Use Cases:

  • Civil Engineering: Designing floor joists, beams in bridges, and other structural elements.
  • Mechanical Engineering: Analyzing components like shafts, levers, and frames that experience bending loads.
  • Architecture: Ensuring aesthetic requirements are met by controlling excessive sagging in visible beams.
  • DIY Projects: Estimating the behavior of custom-built wooden or metal beams.

Disclaimer: This calculator provides an estimate based on simplified physics. For critical applications, always consult a qualified structural engineer and refer to detailed design codes and standards. Material properties and boundary conditions can significantly affect actual performance.

function calculateBeamProperties() { var loadPerUnitLength = parseFloat(document.getElementById("loadPerUnitLength").value); var beamLength = parseFloat(document.getElementById("beamLength").value); var youngsModulus = parseFloat(document.getElementById("youngsModulus").value); var momentOfInertia = parseFloat(document.getElementById("momentOfInertia").value); var resultDiv = document.getElementById("result"); resultDiv.innerHTML = "; // Clear previous results // Input validation if (isNaN(loadPerUnitLength) || isNaN(beamLength) || isNaN(youngsModulus) || isNaN(momentOfInertia) || loadPerUnitLength <= 0 || beamLength <= 0 || youngsModulus <= 0 || momentOfInertia <= 0) { resultDiv.innerHTML = 'Please enter valid positive numbers for all fields.'; return; } // Calculations // Maximum deflection: delta_max = (5 * w * L^4) / (384 * E * I) var maxDeflection = (5 * loadPerUnitLength * Math.pow(beamLength, 4)) / (384 * youngsModulus * momentOfInertia); // Maximum bending moment: M_max = (w * L^2) / 8 var maxBendingMoment = (loadPerUnitLength * Math.pow(beamLength, 2)) / 8; // Format results for display var deflectionDisplay; if (maxDeflection < 1e-6) { deflectionDisplay = (maxDeflection * 1e9).toFixed(2) + " nm"; } else if (maxDeflection < 1e-3) { deflectionDisplay = (maxDeflection * 1e6).toFixed(2) + " µm"; } else if (maxDeflection < 1) { deflectionDisplay = (maxDeflection * 1e3).toFixed(2) + " mm"; } else { deflectionDisplay = maxDeflection.toFixed(3) + " m"; } var momentDisplay; if (maxBendingMoment < 1) { momentDisplay = maxBendingMoment.toFixed(3) + " Nm"; } else if (maxBendingMoment < 1000) { momentDisplay = maxBendingMoment.toFixed(2) + " Nm"; } else { momentDisplay = (maxBendingMoment / 1000).toFixed(2) + " kNm"; } resultDiv.innerHTML = '

Results:

' + 'Maximum Deflection: ' + deflectionDisplay + '' + 'Maximum Bending Moment: ' + momentDisplay + '' + '(Note: Bending Stress requires cross-section geometry, typically represented by 'y', the distance from the neutral axis to the extreme fiber. Consult engineering resources for stress calculation.)'; }

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