Calculate Beam Span

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Calculate Beam Span: Free Beam Span Calculator

Determine the maximum safe span for your structural beams with our comprehensive calculator.

Beam Span Calculator

Wood (Pine/Fir) Wood (Oak) Steel (A36) Aluminum (6061-T6) Select the material of the beam.
Rectangular I-Beam (W-Shape) Square Circular Select the cross-sectional shape of the beam.
Enter width for rectangular/square, or diameter for circular (mm).
Enter height for rectangular/square beams (mm).
Uniformly Distributed Load (UDL) Concentrated Point Load Select how the load is applied to the beam.
Enter the total load (N for UDL, or force at center for Point Load).
Enter the denominator for L/X deflection limit (e.g., 360 for L/360).
Simply Supported Cantilever Fixed-Fixed Fixed-Simply Supported Select how the beam is supported at its ends.

Calculation Results

–.– m
Max Shear Force: –.– kN
Max Bending Moment: –.– kNm
Max Deflection: –.– mm
The maximum beam span (L) is calculated based on material properties (Modulus of Elasticity E, Moment of Inertia I), load (w or P), and allowable deflection (Δ_allow). The formula varies by load type and support conditions, but generally solves for L in the deflection equation: Δ = C * (wL^4 / EI) or Δ = C * (PL^3 / EI), where C is a constant dependent on support and load type. We also check against shear stress limits.

Key Assumptions:

Material Properties: E = — GPa, Yield Strength = — MPa
Beam Shape Properties: I = — m^4, Area = — m^2
Load Type:
Support Condition:
Allowable Deflection Ratio: L/–

Beam Deflection Profile

Max Deflection Point
Material and Shape Properties
Property Wood (Pine/Fir) Wood (Oak) Steel (A36) Aluminum (6061-T6)
Modulus of Elasticity (E) [GPa] 11 12.6 200 69
Allowable Bending Stress (σ_allow) [MPa] 8.3 10.3 150 145
Allowable Shear Stress (τ_allow) [MPa] 0.7 0.8 90 97

Understanding Beam Span Calculations

What is Beam Span?

The term "beam span" refers to the horizontal distance between two supports for a beam. In structural engineering and construction, accurately determining the maximum allowable beam span is crucial for ensuring the safety and integrity of a structure. A beam's span dictates how much load it can safely carry without excessive bending, deflection, or failure. The longer the span, the greater the stress and deflection the beam will experience under load. Therefore, calculating the correct beam span involves considering the beam's material properties, its cross-sectional shape, the type and magnitude of the load it will bear, and the conditions of its supports. This calculation is fundamental to preventing structural collapse and ensuring long-term durability. Understanding beam span is a core concept in structural analysis.

Beam Span Formula and Mathematical Explanation

Calculating the maximum beam span is primarily governed by two critical factors: bending stress and deflection. While bending stress relates to the material's strength, deflection relates to its stiffness. Often, deflection limits are more stringent than stress limits for serviceability reasons (e.g., preventing cracking of finishes).

The general formula for maximum deflection (Δ) in a beam is often expressed as:

Δ = (C * Load * L^n) / (E * I)

Where:

  • Δ: Maximum deflection (e.g., in meters or millimeters).
  • C: A constant that depends on the load type and support conditions. For example, C=5/384 for a uniformly distributed load on a simply supported beam, and C=1/3 for a point load at the center of a simply supported beam.
  • Load: The magnitude of the load. For Uniformly Distributed Load (UDL), this is typically represented as 'w' (force per unit length, e.g., N/m). For a Point Load, it's 'P' (total force, e.g., N).
  • L: The beam span (the distance between supports, e.g., in meters).
  • E: The Modulus of Elasticity (Young's Modulus) of the beam material, representing its stiffness (e.g., in Pascals or GPa).
  • I: The Area Moment of Inertia of the beam's cross-section, representing its resistance to bending (e.g., in m⁴).
  • n: The exponent, which is 4 for UDL (w) and 3 for Point Load (P).

To find the maximum allowable span (L_max), we rearrange the deflection formula, setting Δ to the allowable deflection (Δ_allow), which is often expressed as a fraction of the span (e.g., L/360).

For a UDL (w) on a simply supported beam: Δ_allow = (5 * w * L_max^4) / (384 * E * I). Rearranging for L_max:

L_max = [ (384 * E * I * Δ_allow) / (5 * w) ] ^ (1/4)

For a Point Load (P) at the center of a simply supported beam: Δ_allow = (P * L_max^3) / (48 * E * I). Rearranging for L_max:

L_max = [ (48 * E * I * Δ_allow) / P ] ^ (1/3)

The calculator also considers shear stress, especially critical for shorter spans or heavier loads. The maximum shear force (V) and bending moment (M) formulas also depend on load type and support conditions. For instance, for a simply supported beam with UDL (w): V_max = wL/2 and M_max = wL²/8. The allowable span must also satisfy the bending stress limit: σ_allow = M_max / S, where S is the Section Modulus.

Our calculator uses these principles, adapting the formulas based on your input for material, shape, load, and support conditions to provide the most accurate beam span. This involves complex structural engineering calculations.

Practical Examples (Real-World Use Cases)

Understanding beam span is vital in numerous construction and DIY projects. Here are a few practical examples:

  • Deck Construction: When building a deck, you need to determine the span of the joists and beams supporting the deck boards. The calculator can help determine the maximum span for joists based on the wood type, size, and the expected live and dead loads (people, furniture, snow). This ensures the deck is safe and doesn't sag excessively.
  • Shelving Units: For custom-built bookshelves or heavy-duty shelving, calculating the span of the shelves is essential. Using the calculator with appropriate material properties (e.g., plywood, solid wood) and load (books), you can find the maximum shelf length before it starts to noticeably deflect or break.
  • Roof Rafters/Beams: In home construction, roof rafters and beams support the roof structure and roofing materials. Engineers use beam span calculations to ensure these structural elements can handle wind loads, snow loads, and the weight of the roof itself over the required spans between supporting walls or columns.
  • Bridge Design: For smaller pedestrian bridges or structural elements within larger bridges, engineers calculate the maximum span of beams or girders to safely carry traffic loads over a gap. The choice of material (steel, concrete, wood) and beam profile significantly impacts the achievable span.
  • Renovation Projects: When removing a non-load-bearing wall or creating a larger open space, a structural beam (like a steel I-beam or a laminated veneer lumber – LVL) is often installed. The calculator can assist in preliminary estimations of the required beam size and its maximum span capacity between new support points. This is a common task in home renovation planning.

How to Use This Beam Span Calculator

Using our Beam Span Calculator is straightforward. Follow these steps to get your results:

  1. Select Beam Material: Choose the material your beam is made from (e.g., Wood – Pine/Fir, Steel – A36). This selection loads the relevant Modulus of Elasticity (E) and allowable stress values.
  2. Select Beam Shape: Choose the cross-sectional shape of your beam (e.g., Rectangular, I-Beam).
  3. Enter Shape Dimensions: Input the relevant dimensions for your chosen shape. For rectangular beams, enter Width (b) and Height (h). For circular beams, enter Diameter (d). For I-beams, specific profiles would require more detailed input, but for simplicity, this calculator might use typical values or require equivalent rectangular dimensions. Units are in millimeters (mm).
  4. Specify Load Type: Select whether the load is Uniformly Distributed (UDL) across the entire span or a single Concentrated Point Load at the center.
  5. Enter Load Magnitude: Input the total load value. For UDL, this is the total force (N) the beam must support. For a Point Load, it's the force applied at the center (N).
  6. Set Allowable Deflection Factor: Enter the denominator for your desired deflection limit (e.g., 360 for L/360). This is a common serviceability requirement.
  7. Choose Support Condition: Select how the beam is supported (e.g., Simply Supported, Cantilever, Fixed-Fixed).
  8. Calculate: Click the "Calculate Span" button.

The calculator will then display the maximum safe beam span in meters, along with key intermediate values like maximum shear force, bending moment, and deflection. It also shows the material and shape properties used in the calculation. Use the "Reset" button to clear all fields and start over, and the "Copy Results" button to save your findings.

Key Factors That Affect Beam Span Results

Several factors significantly influence the maximum allowable beam span. Understanding these helps in interpreting the calculator's results and making informed design decisions:

  • Material Properties (E and Strength): A higher Modulus of Elasticity (E) means a stiffer material, allowing for longer spans before deflection limits are reached. Higher allowable bending and shear strengths permit beams to withstand greater bending moments and shear forces, potentially increasing span, especially if stress is the limiting factor.
  • Cross-Sectional Shape and Size (Moment of Inertia, I): The shape and dimensions of the beam's cross-section are critical. The Area Moment of Inertia (I) quantifies a beam's resistance to bending. Deeper beams and shapes like I-beams generally have much higher 'I' values for a given amount of material compared to shallow or narrow shapes, enabling significantly longer spans.
  • Load Magnitude and Type: Heavier loads directly reduce the allowable span. The way a load is distributed also matters; a concentrated point load typically causes more stress and deflection at its location than a UDL of the same total magnitude spread over the span.
  • Support Conditions: How a beam is supported dramatically affects its bending moment and deflection. Fixed supports (Fixed-Fixed, Fixed-Simply) provide more restraint than simple supports (Simply Supported), generally allowing for longer spans or reduced internal forces for the same span. Cantilevers are the most restrictive, with the span limited by the fixed support's capacity and the free end's deflection.
  • Allowable Deflection Limit: This is often the governing factor for serviceability. Stricter limits (e.g., L/720) will result in shorter maximum spans compared to more lenient limits (e.g., L/180). The choice of limit depends on the application and building codes.
  • Safety Factors: While not always explicit inputs in simple calculators, safety factors are incorporated into material strength values and design codes to account for uncertainties in loads, material properties, and construction.

Accurate input of these factors is essential for reliable beam span calculations, forming the basis of sound structural design principles.

Frequently Asked Questions (FAQ)

Q: What is the difference between span and length?

For a beam, the "span" specifically refers to the clear distance between its supports. The "length" might refer to the total physical length of the beam, which often includes extra length for embedment into supports or overhangs. In calculations, "span" (L) is the critical dimension.

Q: What is the most common beam span limit?

The most common allowable deflection limit is L/360 for general construction, meaning the maximum deflection should not exceed the span divided by 360. However, stricter limits like L/720 might be used for sensitive applications, while more lenient ones like L/180 might be acceptable in others. Building codes specify these limits.

Q: Can I use this calculator for beams that are not simply supported?

Yes, this calculator includes options for various support conditions like Cantilever, Fixed-Fixed, and Fixed-Simply Supported beams. The formulas and constants used will adjust based on your selection.

Q: How does the beam's cross-sectional shape affect the span?

The shape significantly impacts the Area Moment of Inertia (I). Shapes that distribute material further from the neutral axis (like I-beams) have a much higher 'I' value than simpler shapes (like rectangles or circles) of the same area. A higher 'I' value increases the beam's stiffness and resistance to bending, allowing for longer spans.

Q: What units should I use for input?

Dimensions (width, height, diameter) should be entered in millimeters (mm). Load magnitude should be in Newtons (N). The allowable deflection factor is a unitless ratio (e.g., 360). The results will be displayed in meters (m) for span and millimeters (mm) for deflection.

Related Tools and Internal Resources

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var materialProperties = { wood_pine_fir: { E: 11, yield_strength: 8.3, shear_strength: 0.7 }, // E in GPa, Strengths in MPa wood_oak: { E: 12.6, yield_strength: 10.3, shear_strength: 0.8 }, steel_a36: { E: 200, yield_strength: 250, shear_strength: 150 }, // Yield strength for steel is often higher, using a conservative allowable stress for bending aluminum_6061: { E: 69, yield_strength: 240, shear_strength: 160 } // Using typical yield strength, allowable stress might be lower }; var shapeProperties = { rectangular: { requires_height: true, formula_I: function(b, h) { return (b * Math.pow(h, 3)) / 12; }, formula_S: function(b, h) { return (b * Math.pow(h, 2)) / 6; }, formula_Area: function(b, h) { return b * h; } }, square: { requires_height: false, formula_I: function(d, h) { return (Math.pow(d, 4)) / 12; }, formula_S: function(d, h) { return (Math.pow(d, 3)) / 6; }, formula_Area: function(d, h) { return Math.pow(d, 2); } }, circular: { requires_height: false, formula_I: function(d, h) { return (Math.PI * Math.pow(d, 4)) / 64; }, formula_S: function(d, h) { return (Math.PI * Math.pow(d, 3)) / 32; }, formula_Area: function(d, h) { return (Math.PI * Math.pow(d, 2)) / 4; } }, i_beam: { requires_height: true, formula_I: function(b, h) { /* Simplified I-beam calculation – real I-beams need specific tables or complex formulas */ var flange_width = b * 0.5; // Assume flange width is half of overall width var flange_thickness = h * 0.1; // Assume flange thickness is 10% of height var web_height = h – 2 * flange_thickness; var web_thickness = b * 0.1; // Assume web thickness is 10% of overall width var I_flange = 2 * ( (flange_width * Math.pow(flange_thickness, 3)) / 12 + flange_width * flange_thickness * Math.pow((h/2 – flange_thickness/2), 2) ); var I_web = (web_thickness * Math.pow(web_height, 3)) / 12; return I_flange + I_web; }, formula_S: function(b, h) { /* Simplified S calculation */ var flange_width = b * 0.5; var flange_thickness = h * 0.1; var web_height = h – 2 * flange_thickness; var web_thickness = b * 0.1; var S_flange = (flange_width * Math.pow(flange_thickness, 2)) / 2; var S_web = (web_thickness * Math.pow(web_height, 2)) / 6; return S_flange + S_web; }, formula_Area: function(b, h) { /* Simplified Area calculation */ var flange_width = b * 0.5; var flange_thickness = h * 0.1; var web_height = h – 2 * flange_thickness; var web_thickness = b * 0.1; var Area_flange = 2 * flange_width * flange_thickness; var Area_web = web_thickness * web_height; return Area_flange + Area_web; }} }; var constants = { gravity: 9.81 // m/s^2, not directly used but good to have }; var chartInstance = null; function updateShapeProperties() { var shape = document.getElementById("beamShape").value; var shapeInfo = shapeProperties[shape]; var dimension2Group = document.getElementById("dimension2Group"); var dimension1Label = document.querySelector("label[for='dimension1′]"); var dimension2Label = document.querySelector("label[for='dimension2′]"); if (shapeInfo.requires_height) { dimension2Group.style.display = "block"; if (shape === "rectangular") { dimension1Label.textContent = "Width (b)"; dimension2Label.textContent = "Height (h)"; document.getElementById("dimension1").placeholder = "e.g., 100"; document.getElementById("dimension2").placeholder = "e.g., 150"; } else if (shape === "i_beam") { dimension1Label.textContent = "Overall Width (b)"; dimension2Label.textContent = "Overall Height (h)"; document.getElementById("dimension1").placeholder = "e.g., 150"; document.getElementById("dimension2").placeholder = "e.g., 300"; } } else { dimension2Group.style.display = "none"; if (shape === "square") { dimension1Label.textContent = "Side Length (d)"; document.getElementById("dimension1").placeholder = "e.g., 120"; } else if (shape === "circular") { dimension1Label.textContent = "Diameter (d)"; document.getElementById("dimension1").placeholder = "e.g., 100"; } } calculateBeamSpan(); } function updateMaterialProperties() { calculateBeamSpan(); } function validateInput(id, errorId, minValue, maxValue) { var input = document.getElementById(id); var errorSpan = document.getElementById(errorId); var value = parseFloat(input.value); errorSpan.textContent = ""; // Clear previous error if (isNaN(value)) { errorSpan.textContent = "Please enter a valid number."; return false; } if (value maxValue) { errorSpan.textContent = "Value is too high."; return false; } return true; } function calculateBeamSpan() { // Clear previous errors document.getElementById("materialError").textContent = ""; document.getElementById("shapeError").textContent = ""; document.getElementById("dimension1Error").textContent = ""; document.getElementById("dimension2Error").textContent = ""; document.getElementById("loadTypeError").textContent = ""; document.getElementById("loadValueError").textContent = ""; document.getElementById("allowableDeflectionFactorError").textContent = ""; document.getElementById("supportConditionError").textContent = ""; // Get inputs var material = document.getElementById("beamMaterial").value; var shape = document.getElementById("beamShape").value; var dim1 = parseFloat(document.getElementById("dimension1").value); var dim2 = document.getElementById("dimension2Group").style.display !== "none" ? parseFloat(document.getElementById("dimension2").value) : dim1; // Use dim1 if dim2 is hidden var loadType = document.getElementById("loadType").value; var loadValue = parseFloat(document.getElementById("loadValue").value); var deflectionFactor = parseFloat(document.getElementById("allowableDeflectionFactor").value); var supportCondition = document.getElementById("supportCondition").value; // — Input Validation — var isValid = true; if (!validateInput("dimension1", "dimension1Error", 0)) isValid = false; if (document.getElementById("dimension2Group").style.display !== "none" && !validateInput("dimension2", "dimension2Error", 0)) isValid = false; if (!validateInput("loadValue", "loadValueError", 0)) isValid = false; if (!validateInput("allowableDeflectionFactor", "allowableDeflectionFactorError", 1)) isValid = false; if (!isValid) { document.getElementById("mainResult").textContent = "–.– m"; document.getElementById("maxShear").querySelector("span").textContent = "–.– kN"; document.getElementById("maxMoment").querySelector("span").textContent = "–.– kNm"; document.getElementById("maxDeflection").querySelector("span").textContent = "–.– mm"; updateChart([], []); return; } // — Get Properties — var matProps = materialProperties[material]; var shapeInfo = shapeProperties[shape]; // Convert dimensions from mm to meters var dim1_m = dim1 / 1000; var dim2_m = dim2 / 1000; // Calculate shape properties in SI units (m^4, m^2, m^3) var I = shapeInfo.formula_I(dim1_m, dim2_m); var S = shapeInfo.formula_S(dim1_m, dim2_m); var Area = shapeInfo.formula_Area(dim1_m, dim2_m); // Convert material properties to Pascals (Pa) var E_Pa = matProps.E * 1e9; // GPa to Pa var yield_strength_Pa = matProps.yield_strength * 1e6; // MPa to Pa var shear_strength_Pa = matProps.shear_strength * 1e6; // MPa to Pa // Convert load to Newtons (already in N) var load_N = loadValue; // Convert allowable deflection factor to actual deflection limit (meters) var allowable_deflection_m = (1 / deflectionFactor); // This is a ratio, span L is unknown yet. We solve for L. // — Constants for Formulas — var C_deflection, C_moment, C_shear, load_term; var exponent_L; // Adjust load term based on load type (w = N/m, P = N) var w = 0; // UDL per meter var P = 0; // Point load if (loadType === "uniform") { // Assuming loadValue is the TOTAL load for UDL. Convert to load per meter. // This requires knowing the span L first. This is an iterative problem or requires solving for L directly. // For simplicity, let's assume loadValue is total load and we'll derive w = loadValue / L. // This means the deflection formula becomes Δ = C * ( (loadValue/L) * L^4 ) / (EI) = C * loadValue * L^3 / (EI) // Or, if loadValue is already w (N/m), then Δ = C * w * L^4 / (EI) // Let's assume loadValue is the TOTAL load for UDL and we need to find L. // The formula for deflection with UDL (w per unit length) is Δ = C_w * w * L^4 / (EI) // The formula for deflection with Point Load (P) at center is Δ = C_p * P * L^3 / (EI) // Let's re-evaluate: If loadValue is the TOTAL load for UDL, then w = loadValue / L. // The deflection formula is Δ = (5/384) * w * L^4 / (EI) // Substituting w = loadValue / L: Δ = (5/384) * (loadValue / L) * L^4 / (EI) = (5/384) * loadValue * L^3 / (EI) // This means for UDL, if loadValue is TOTAL load, the exponent for L is 3. // If loadValue is w (N/m), the exponent is 4. // Let's assume loadValue is w (N/m) for simplicity in formula derivation. w = load_N; // Assuming loadValue is w (N/m) load_term = w; exponent_L = 4; } else { // Point Load P = load_N; // Assuming loadValue is P (N) load_term = P; exponent_L = 3; } // — Determine Constants based on Support Condition — var deflection_constant = 0; var moment_constant = 0; var shear_constant = 0; switch (supportCondition) { case "simply_supported": if (loadType === "uniform") { deflection_constant = 5 / 384; // C for UDL moment_constant = 1 / 8; // C for M_max shear_constant = 1 / 2; // C for V_max } else { // Point Load deflection_constant = 1 / 48; // C for P at center moment_constant = 1 / 4; // C for M_max at center shear_constant = 1 / 2; // C for V_max at ends } break; case "cantilever": if (loadType === "uniform") { // Load applied at the free end, or UDL along the length? Assuming UDL along length. deflection_constant = 1 / 8; // C for UDL along length moment_constant = 1 / 2; // C for M_max at fixed end shear_constant = 1; // C for V_max at fixed end } else { // Point Load at free end deflection_constant = 1 / 3; // C for P at free end moment_constant = 1; // C for M_max at fixed end shear_constant = 1; // C for V_max at fixed end } break; case "fixed_fixed": if (loadType === "uniform") { deflection_constant = 1 / 384; // C for UDL moment_constant = 1 / 12; // C for M_max (at supports) shear_constant = 1 / 2; // C for V_max (at supports) } else { // Point Load at center deflection_constant = 1 / 192; // C for P at center moment_constant = 1 / 8; // C for M_max (at center) shear_constant = 1 / 2; // C for V_max (at supports) } break; case "fixed_simply": if (loadType === "uniform") { deflection_constant = 1 / 185; // Approximate constant for deflection at free end moment_constant = 1 / 9; // Approximate constant for max moment shear_constant = 1 / 2; // V_max at fixed end } else { // Point Load at center deflection_constant = 1 / 100; // Approximate constant for deflection at free end moment_constant = 1 / 6; // Approximate constant for max moment shear_constant = 1 / 2; // V_max at fixed end } break; } // — Calculate Max Span (L) based on Deflection Limit — // Δ_allow = deflection_constant * load_term * L^exponent_L / (E_Pa * I) // L^exponent_L = (Δ_allow * E_Pa * I) / (deflection_constant * load_term) // L = [ (Δ_allow * E_Pa * I) / (deflection_constant * load_term) ] ^ (1 / exponent_L) // We need Δ_allow in terms of L. Δ_allow = L / deflectionFactor. // So, L / deflectionFactor = deflection_constant * load_term * L^exponent_L / (E_Pa * I) var L_span_m = 0; var max_deflection_m = 0; if (exponent_L === 4) { // UDL case // L / deflectionFactor = deflection_constant * w * L^4 / (E_Pa * I) // 1 / deflectionFactor = deflection_constant * w * L^3 / (E_Pa * I) // L^3 = (E_Pa * I) / (deflection_constant * w * deflectionFactor) // L = [ (E_Pa * I) / (deflection_constant * w * deflectionFactor) ] ^ (1/3) if (w > 0) { var L_cubed = (E_Pa * I) / (deflection_constant * w * deflectionFactor); if (L_cubed > 0) { L_span_m = Math.pow(L_cubed, 1/3); } } } else if (exponent_L === 3) { // Point Load case // L / deflectionFactor = deflection_constant * P * L^3 / (E_Pa * I) // L^2 / deflectionFactor = deflection_constant * P * L^2 / (E_Pa * I) — This is wrong. // Let's re-derive: Δ = C_p * P * L^3 / (EI). Set Δ = L / deflectionFactor. // L / deflectionFactor = C_p * P * L^3 / (EI) // 1 / deflectionFactor = C_p * P * L^2 / (EI) // L^2 = (EI) / (C_p * P * deflectionFactor) // L = [ (EI) / (C_p * P * deflectionFactor) ] ^ (1/2) if (P > 0) { var L_squared = (E_Pa * I) / (deflection_constant * P * deflectionFactor); if (L_squared > 0) { L_span_m = Math.pow(L_squared, 1/2); } } } // Ensure L_span_m is not NaN or Infinity if (isNaN(L_span_m) || !isFinite(L_span_m) || L_span_m 0) { if (loadType === "uniform") { max_deflection_m = deflection_constant * w * Math.pow(L_span_m, exponent_L) / (E_Pa * I); } else { // Point Load max_deflection_m = deflection_constant * P * Math.pow(L_span_m, exponent_L) / (E_Pa * I); } } // Calculate Max Shear Force and Max Bending Moment using the calculated L_span_m var max_shear_N = 0; var max_moment_Nm = 0; if (L_span_m > 0) { if (loadType === "uniform") { max_shear_N = shear_constant * w * L_span_m; max_moment_Nm = moment_constant * w * Math.pow(L_span_m, 2); } else { // Point Load max_shear_N = shear_constant * P; max_moment_Nm = moment_constant * P * L_span_m; } } // — Check Bending Stress — var allowable_bending_stress_Pa = matProps.yield_strength * 1e6; // Use yield strength as a proxy for allowable stress var actual_bending_stress_Pa = max_moment_Nm / S; var stress_limit_span_m = 0; if (actual_bending_stress_Pa > 0 && allowable_bending_stress_Pa > 0) { // M_max = moment_constant * load_term * L^2 (for UDL) or M_max = moment_constant * load_term * L (for Point Load) // σ_allow = M_max / S // L^2 = (σ_allow * S) / (moment_constant * w) (for UDL) // L = sqrt( (σ_allow * S) / (moment_constant * w) ) // L = (σ_allow * S) / (moment_constant * P) (for Point Load) if (loadType === "uniform" && w > 0) { var L_squared_stress = (allowable_bending_stress_Pa * S) / (moment_constant * w); if (L_squared_stress > 0) stress_limit_span_m = Math.sqrt(L_squared_stress); } else if (loadType === "point" && P > 0) { var L_stress = (allowable_bending_stress_Pa * S) / (moment_constant * P); if (L_stress > 0) stress_limit_span_m = L_stress; } } // The final span is the minimum of the deflection-limited span and the stress-limited span var final_span_m = L_span_m; if (stress_limit_span_m > 0 && stress_limit_span_m 0) { mainResultElement.textContent = final_span_m.toFixed(3) + " m"; maxShearElement.textContent = (max_shear_N / 1000).toFixed(2) + " kN"; maxMomentElement.textContent = (max_moment_Nm / 1000).toFixed(2) + " kNm"; maxDeflectionElement.textContent = (max_deflection_m * 1000).toFixed(2) + " mm"; // Convert m to mm } else { mainResultElement.textContent = "N/A"; maxShearElement.textContent = "N/A"; maxMomentElement.textContent = "N/A"; maxDeflectionElement.textContent = "N/A"; } // — Update Assumptions — document.getElementById("assumption1").innerHTML = "Material Properties: E = " + matProps.E.toFixed(1) + " GPa, Allowable Bending Stress (approx) = " + matProps.yield_strength.toFixed(1) + " MPa"; document.getElementById("assumption2").innerHTML = "Beam Shape Properties: I = " + I.toExponential(2) + " m&sup4;, S = " + S.toExponential(2) + " m³, Area = " + Area.toFixed(4) + " m²"; document.getElementById("assumptionLoadType").textContent = loadType === "uniform" ? "Uniformly Distributed Load (UDL)" : "Concentrated Point Load"; document.getElementById("assumptionSupport").textContent = supportCondition.replace('_', ' ').replace(/\b\w/g, char => char.toUpperCase()); document.getElementById("assumptionDeflection").textContent = deflectionFactor; // — Update Chart — updateChart(final_span_m, max_deflection_m, supportCondition, loadType); } function updateChart(span, maxDeflection, support, loadType) { var ctx = document.getElementById('deflectionChart').getContext('2d'); // Clear previous chart if it exists if (chartInstance) { chartInstance.destroy(); } if (span <= 0 || maxDeflection <= 0) { ctx.clearRect(0, 0, ctx.canvas.width, ctx.canvas.height); // Clear canvas if no data return; } var deflectionData = []; var labels = []; var numPoints = 50; var step = span / numPoints; for (var i = 0; i <= numPoints; i++) { var x = i * step; labels.push(x.toFixed(2)); var deflection = 0; // Simplified deflection profile calculation based on support and load type // This is a conceptual representation, not a precise plot for all cases. switch (support) { case "simply_supported": if (loadType === "uniform") { // Parabolic deflection: y = k * x * (L – x) deflection = maxDeflection * 4 * (x / span) * (1 – (x / span)); } else { // Point Load at center if (x <= span / 2) { deflection = maxDeflection * 2 * (x / span) * (1 – (x / span) / 2); } else { deflection = maxDeflection * 2 * (1 – x / span) * (x / span / 2); } } break; case "cantilever": if (loadType === "uniform") { // Deflection increases towards the free end deflection = maxDeflection * Math.pow(x / span, 2); } else { // Point Load at free end deflection = maxDeflection * (x / span); } break; case "fixed_fixed": if (loadType === "uniform") { deflection = maxDeflection * 16 * Math.pow(x / span, 2) * Math.pow(1 – x / span, 2); } else { // Point Load at center if (x { var index = context.dataIndex; if (index === maxDeflectionIndex) return 5; // Highlight max deflection point return 0; // Hide other points }, pointBackgroundColor: 'red', pointBorderColor: 'red' }] }, options: { responsive: true, maintainAspectRatio: false, scales: { x: { title: { display: true, text: 'Distance along Span (m)' }, grid: { display: false } }, y: { title: { display: true, text: 'Deflection (mm)' }, ticks: { callback: function(value) { return value.toFixed(2); } }, grid: { color: 'rgba(200, 200, 200, 0.2)' } } }, plugins: { legend: { display: false }, // Custom legend below tooltip: { callbacks: { label: function(context) { var label = context.dataset.label || "; if (label) { label += ': '; } if (context.parsed.y !== null) { label += context.parsed.y.toFixed(3) + ' mm'; } return label; } } } } } }); } function copyResults() { var mainResult = document.getElementById("mainResult").textContent; var maxShear = document.getElementById("maxShear").textContent; var maxMoment = document.getElementById("maxMoment").textContent; var maxDeflection = document.getElementById("maxDeflection").textContent; var assumption1 = document.getElementById("assumption1").textContent; var assumption2 = document.getElementById("assumption2").textContent; var assumption3 = document.getElementById("assumption3").textContent; var assumption4 = document.getElementById("assumption4").textContent; var assumption5 = document.getElementById("assumption5").textContent; var textToCopy = "Beam Span Calculation Results:\n\n"; textToCopy += "Max Span: " + mainResult + "\n"; textToCopy += maxShear + "\n"; textToCopy += maxMoment + "\n"; textToCopy += maxDeflection + "\n\n"; textToCopy += "Key Assumptions:\n"; textToCopy += "- " + assumption1 + "\n"; textToCopy += "- " + assumption2 + "\n"; textToCopy += "- " + assumption3 + "\n"; textToCopy += "- " + assumption4 + "\n"; textToCopy += "- " + assumption5 + "\n"; navigator.clipboard.writeText(textToCopy).then(function() { // Success feedback (optional) var copyButton = document.querySelector('.copy-button'); copyButton.textContent = 'Copied!'; setTimeout(function() { copyButton.textContent = 'Copy Results'; }, 2000); }).catch(function(err) { console.error('Failed to copy text: ', err); // Error feedback (optional) }); } function resetCalculator() { document.getElementById("beamMaterial").value = "wood_pine_fir"; document.getElementById("beamShape").value = "rectangular"; document.getElementById("dimension1").value = "100"; document.getElementById("dimension2").value = "150"; document.getElementById("loadType").value = "uniform"; document.getElementById("loadValue").value = "5000"; document.getElementById("allowableDeflectionFactor").value = "360"; document.getElementById("supportCondition").value = "simply_supported"; document.getElementById("materialError").textContent = ""; document.getElementById("shapeError").textContent = ""; document.getElementById("dimension1Error").textContent = ""; document.getElementById("dimension2Error").textContent = ""; document.getElementById("loadTypeError").textContent = ""; document.getElementById("loadValueError").textContent = ""; document.getElementById("allowableDeflectionFactorError").textContent = ""; document.getElementById("supportConditionError").textContent = ""; updateShapeProperties(); // Update display based on reset shape calculateBeamSpan(); // Recalculate with defaults } // Initial setup on page load window.onload = function() { updateShapeProperties(); calculateBeamSpan(); // Load Chart.js library dynamically if not already present if (typeof Chart === 'undefined') { var script = document.createElement('script'); script.src = 'https://cdn.jsdelivr.net/npm/chart.js'; script.onload = function() { calculateBeamSpan(); // Recalculate after chart library is loaded }; document.head.appendChild(script); } else { calculateBeamSpan(); // Calculate immediately if Chart.js is already loaded } };

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