Acrylic Weight Load Calculator

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Acrylic Weight Load Calculator

Determine the safe load capacity for your acrylic panels with precision.

Acrylic Load Bearing Calculator

Enter the thickness of the acrylic sheet in millimeters (mm).
Enter the width of the acrylic panel in millimeters (mm).
Enter the height (or length) of the acrylic panel in millimeters (mm).
Enter the distance between supports in millimeters (mm). This is the critical unsupported length.
Uniformly Distributed Load (UDL) Point Load Select whether the load is spread evenly or concentrated at a single point.
Enter the distance from the nearest edge where the point load is applied (mm).
A multiplier for safety (e.g., 3 is common). Higher means more conservative.

Load Capacity

Max Stress: Pa
Deflection: mm
Allowable Load: kg
Formula Explanation: The calculation uses principles of beam bending theory. For Uniformly Distributed Load (UDL), the maximum stress (σ) is calculated as (3 * w * L^2) / (2 * b * h^2) and deflection (δ) as (5 * w * L^4) / (384 * E * I), where 'w' is load per unit length, L is span, b is width, h is thickness, E is Modulus of Elasticity for acrylic, and I is the moment of inertia. For a Point Load (PL), stress is (3 * P * L) / (2 * b * h^2) and deflection is (P * L^3) / (48 * E * I) at the center. These are adjusted for the actual load type and then divided by the safety factor to determine the allowable load.
Comparison of Allowable Load vs. Safety Factor
Acrylic Material Properties (Typical)
Property Value Unit
Modulus of Elasticity (E) 3.2 GPa (3.2 x 10^9 Pa)
Tensile Strength (Ultimate) 60-80 MPa
Poisson's Ratio 0.35

What is an Acrylic Weight Load Calculator?

{primary_keyword} is a specialized tool designed to estimate the maximum weight an acrylic sheet can safely support without structural failure or excessive deformation. Acrylic, while strong and versatile, has specific load-bearing limitations. Understanding these limits is crucial for designers, fabricators, and end-users to ensure the safety and longevity of acrylic installations, whether they are shelves, display cases, partitions, or structural elements.

Who should use it: Anyone planning to use acrylic sheets in a load-bearing application. This includes architects, product designers, engineers, DIY enthusiasts, museum curators (for display cases), and manufacturers of furniture or fixtures.

Common misconceptions: A frequent misunderstanding is that acrylic is as strong as glass or steel. While it offers good impact resistance, its rigidity and load-bearing capacity differ significantly. Another misconception is that a thicker sheet automatically means it can hold much more weight; the span, support conditions, and load distribution are equally, if not more, important factors.

Acrylic Weight Load Calculator Formula and Mathematical Explanation

The core of the acrylic weight load calculator relies on the principles of structural mechanics, specifically the bending stress and deflection formulas for beams. Acrylic sheets, when subjected to a load, behave like beams spanning between support points.

The key factors influencing the load capacity are:

  • Material Properties: The Modulus of Elasticity (E) determines how much the material deflects under stress.
  • Geometry: The thickness (h) and width (b) of the sheet, along with the span (L) between supports, critically affect its strength. A thicker sheet is exponentially stronger.
  • Load Type: Whether the load is distributed uniformly (UDL) or concentrated at a point (PL) changes the stress and deflection patterns.
  • Support Conditions: How the sheet is supported (e.g., simply supported, fixed ends) also impacts the calculations, though most calculators assume simple supports.

The Formulas (Simplified for Two Common Scenarios):

1. Uniformly Distributed Load (UDL)

Let 'w' be the load per unit length (e.g., kg/mm). The total load is W = w * L.

  • Maximum Bending Stress (σ): σ = (3 * w * L^2) / (2 * b * h^2)
  • Maximum Deflection (δ): δ = (5 * w * L^4) / (384 * E * I)
  • Where I (Moment of Inertia for a rectangular cross-section) = (b * h^3) / 12
  • Substituting I: δ = (5 * w * L^4 * 12) / (384 * E * b * h^3) = (5 * w * L^4) / (32 * E * b * h^3)

The calculator determines the maximum 'w' that keeps σ below the allowable stress for acrylic (taking into account a safety factor) and the resulting deflection within acceptable limits.

2. Point Load (P)

Let 'P' be the concentrated load (e.g., kg).

  • Maximum Bending Stress (σ): σ = (3 * P * L) / (2 * b * h^2) (assuming load at center)
  • Maximum Deflection (δ): δ = (P * L^3) / (48 * E * I) (assuming load at center)
  • Substituting I: δ = (P * L^3 * 12) / (48 * E * b * h^3) = (P * L^3) / (4 * E * b * h^3)

The calculator finds the maximum 'P' based on the allowable stress and deflection, considering the location of the point load.

Safety Factor: The calculated maximum allowable load is then divided by the chosen safety factor to provide a conservative estimate. A common safety factor for acrylic is 3, meaning the design load is one-third of the theoretical failure load.

Variables Table:

Variable Meaning Unit Typical Range/Value
h (Thickness) Acrylic Sheet Thickness mm 1 mm to 50+ mm
b (Width) Sheet Width (perpendicular to span) mm 100 mm to 3000+ mm
L (Span) Distance between supports mm 100 mm to 2000+ mm
E (Modulus of Elasticity) Stiffness of Acrylic Pa (or GPa) ~3.2 x 10^9 Pa (3.2 GPa)
w (UDL) Uniformly Distributed Load kg/mm or N/mm Calculated Output
P (Point Load) Concentrated Load kg or N Calculated Output
SF (Safety Factor) Safety Multiplier 2.0 – 5.0 (3.0 common)
σ (Stress) Internal stress within the material Pa Calculated Intermediate Value
δ (Deflection) Amount the sheet bends mm Calculated Intermediate Value
Allowable Load Maximum weight the sheet can safely support kg Calculated Output

Practical Examples (Real-World Use Cases)

Example 1: Acrylic Shelf

Scenario: A homeowner wants to install a 10mm thick acrylic shelf for displaying decorative items. The shelf is 600mm wide and 400mm deep. It will be supported at both ends (span = 400mm). The items will be distributed evenly across the shelf.

Inputs:

  • Thickness: 10 mm
  • Width: 600 mm
  • Height (Depth of shelf): 400 mm (This is the span 'L')
  • Support Span: 400 mm
  • Load Type: Uniformly Distributed Load (UDL)
  • Safety Factor: 3

Calculation Result (using calculator):

  • Maximum Stress: ~15.5 MPa
  • Maximum Deflection: ~2.1 mm
  • Allowable Load: ~45 kg

Interpretation: The 10mm acrylic shelf, with a 400mm span, can safely support approximately 45 kg distributed evenly across its surface. The deflection is minimal (2.1mm), which is usually acceptable for shelves. This allows the homeowner to confidently place items up to this weight on the shelf.

Example 2: Acrylic Display Case Base

Scenario: A museum is designing a display case for a moderately heavy artifact. The base is a 20mm thick acrylic sheet, 800mm x 600mm. It's supported around its entire perimeter (effectively, the span is the internal dimension, let's assume 760mm x 560mm for calculation, and we'll model the load as UDL). A single, heavy component (~30 kg) needs to be placed near the center.

Inputs:

  • Thickness: 20 mm
  • Width: 800 mm
  • Height (Depth of case base): 600 mm
  • Support Span: 560 mm (Assuming effective span in the direction of load)
  • Load Type: Uniformly Distributed Load (UDL) – Approximating the single item's weight spread over a small area.
  • Safety Factor: 4 (Higher for valuable artifacts)

Calculation Result (using calculator):

  • Max Stress: ~18.2 MPa
  • Max Deflection: ~1.5 mm
  • Allowable Load: ~110 kg

Interpretation: The 20mm acrylic base can support approximately 110 kg with a safety factor of 4. This means the 30 kg artifact is well within the safe limits. The calculated deflection of 1.5 mm is negligible for a display case base, ensuring the artifact remains stable and the acrylic doesn't sag noticeably.

How to Use This Acrylic Weight Load Calculator

Using the acrylic weight load calculator is straightforward. Follow these steps:

  1. Measure Accurately: Obtain precise measurements for the acrylic sheet's thickness (h), width (b), and the intended support span (L) in millimeters.
  2. Determine Load Type: Decide if the weight will be spread evenly (Uniformly Distributed Load – UDL) or concentrated at a specific point (Point Load). If it's a point load, note its approximate location relative to the edges.
  3. Select Safety Factor: Choose a safety factor (SF). A common value is 3. Increase this for critical applications or where higher uncertainty exists. A higher SF results in a lower allowable load but increases safety.
  4. Enter Values: Input the measurements and select the load type into the respective fields.
  5. Calculate: Click the "Calculate Load" button.

How to Read Results:

  • Allowable Load: This is the primary result, indicating the maximum weight (in kg) the acrylic panel can safely bear under the specified conditions.
  • Max Stress: Shows the peak internal stress generated within the acrylic. This should ideally remain well below the acrylic's ultimate tensile strength (typically 60-80 MPa).
  • Deflection: Indicates how much the acrylic sheet is expected to bend under the maximum allowable load. Check if this amount of flex is acceptable for your application.

Decision-making guidance: If the calculated allowable load is significantly higher than the expected load, the design is likely safe. If the deflection is too large, consider increasing the acrylic thickness, reducing the span, or adding more support. Always err on the side of caution, especially in applications where failure could lead to injury or significant damage.

Key Factors That Affect Acrylic Weight Load Results

Several factors influence the accuracy and outcome of any acrylic weight load calculation:

  1. Acrylic Thickness (h): This is the most critical factor. Load capacity increases with the *cube* of the thickness. Doubling the thickness increases strength by a factor of 8.
  2. Support Span (L): Load capacity decreases with the *square* of the span for stress and the *fourth power* for deflection. Minimizing the unsupported length is crucial. A short span drastically increases load capacity.
  3. Load Distribution: A uniformly distributed load is generally less stressful and causes less deflection than a concentrated point load of the same total weight. Point loads create high localized stress.
  4. Temperature: Acrylic's stiffness (Modulus of Elasticity) decreases significantly at higher temperatures. Calculations are typically based on standard room temperatures (around 20-25°C). Elevated temperatures can reduce load capacity.
  5. Duration of Load: Acrylic exhibits "creep," meaning it will slowly deform over time under sustained load, even if the stress is below the short-term limit. Long-term loading requires lower stress levels or higher safety factors than short-term loading.
  6. Impact and Shock Loads: The calculations assume static loads. Sudden impacts or vibrations can generate much higher forces than the static weight and may cause failure even if the static load capacity is not exceeded.
  7. Edge Conditions and Mounting: How the acrylic sheet is supported and mounted matters. Gaps, clamping pressure, and the rigidity of surrounding structures affect how the load is distributed and can introduce stress concentrations.
  8. Material Quality and Type: While "acrylic" (PMMA) is standard, different manufacturers might have slight variations in properties. Extruded vs. cast acrylic can also have minor differences. UV resistance and color additives generally don't significantly impact structural strength.

Frequently Asked Questions (FAQ)

Q1: Can I use this calculator for glass or polycarbonate?

No, this calculator is specifically tuned for the typical Modulus of Elasticity and strength properties of acrylic (PMMA). Glass and polycarbonate have different material properties (E, tensile strength) and would require a different calculator.

Q2: What is the difference between UDL and Point Load?

A Uniformly Distributed Load (UDL) means the weight is spread evenly across the surface (like books on a shelf). A Point Load is a concentrated weight at a single spot (like a heavy tool placed on a workbench). Point loads generally cause higher stress and deflection.

Q3: Why is the safety factor important?

The safety factor accounts for uncertainties in material properties, manufacturing tolerances, potential overloading, environmental factors (like temperature), and the consequences of failure. It ensures the actual load is significantly less than the theoretical failure point.

Q4: How does temperature affect acrylic load capacity?

Acrylic softens and becomes less rigid as temperature increases. Its Modulus of Elasticity decreases, meaning it will deflect more and its load capacity will be reduced at elevated temperatures. Always consider the operating temperature range.

Q5: What does "creep" mean for acrylic?

Creep is the tendency of a solid material to deform permanently and slowly over time when subjected to constant stress. For acrylic, sustained loads can lead to gradual sagging or deformation, even if the stress is below the short-term failure point. Using a higher safety factor helps mitigate creep.

Q6: Can I use metric and imperial units interchangeably?

This calculator is designed for millimeters (mm) for dimensions and Pascals (Pa) for stress internally, outputting load in kilograms (kg). Ensure all your input measurements are in millimeters for accurate results.

Q7: What is considered excessive deflection for acrylic?

There's no single standard, as it depends on the application. For aesthetic shelves, a deflection of 1-3 mm might be acceptable. For structural applications or where precise alignment is needed, deflection limits could be much less (e.g., L/360 or L/720 of the span). Consult your project specifications.

Q8: Does the width of the acrylic panel affect load capacity significantly?

Yes, but less dramatically than thickness or span. For a fixed span and thickness, a wider panel distributes the load over a larger width, which can be relevant for certain load types or if the panel is restrained at the sides. However, the formulas used primarily focus on the bending across the span.

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var modulusOfElasticity = 3.2e9; // Pa (3.2 GPa) var safetyFactorInput; var thicknessInput, widthInput, heightInput, supportSpanInput, loadTypeSelect, pointLoadLocationInput; var thicknessError, widthError, heightError, supportSpanError, pointLoadLocationError, safetyFactorError; var mainResultDisplay, maxStressDisplay, maxDeflectionDisplay, allowableLoadDisplay; var chart = null; var canvas; function getElement(id) { return document.getElementById(id); } function initializeElements() { thicknessInput = getElement("thickness"); widthInput = getElement("width"); heightInput = getElement("height"); supportSpanInput = getElement("supportSpan"); loadTypeSelect = getElement("loadType"); pointLoadLocationInput = getElement("pointLoadLocation"); safetyFactorInput = getElement("safetyFactor"); thicknessError = getElement("thicknessError"); widthError = getElement("widthError"); heightError = getElement("heightError"); supportSpanError = getElement("supportSpanError"); pointLoadLocationError = getElement("pointLoadLocationError"); safetyFactorError = getElement("safetyFactorError"); mainResultDisplay = getElement("mainResult"); maxStressDisplay = getElement("maxStress"); maxDeflectionDisplay = getElement("maxDeflection"); allowableLoadDisplay = getElement("allowableLoad"); canvas = getElement("myChart"); if (canvas && canvas.getContext) { // Check if chart already exists before creating a new one if (window.myChartInstance) { window.myChartInstance.destroy(); } var ctx = canvas.getContext("2d"); window.myChartInstance = new Chart(ctx, { type: 'bar', data: { labels: [], datasets: [{ label: 'Max Allowable Load (kg)', data: [], backgroundColor: 'rgba(0, 74, 153, 0.6)', borderColor: 'rgba(0, 74, 153, 1)', borderWidth: 1 }, { label: 'Max Stress (MPa)', data: [], backgroundColor: 'rgba(40, 167, 69, 0.6)', borderColor: 'rgba(40, 167, 69, 1)', borderWidth: 1 }] }, options: { responsive: true, maintainAspectRatio: false, scales: { y: { beginAtZero: true } }, plugins: { legend: { position: 'top', }, title: { display: true, text: 'Load vs. Stress Comparison at Different Safety Factors' } } } }); chart = window.myChartInstance; } } function showPointLoadDetails() { var loadType = getElement("loadType").value; var pointLoadDetailsDiv = getElement("pointLoadDetails"); if (loadType === "point") { pointLoadDetailsDiv.style.display = "flex"; } else { pointLoadDetailsDiv.style.display = "none"; } } function showError(element, message) { if (element) { element.textContent = message; element.classList.add("visible"); } } function hideError(element) { if (element) { element.textContent = ""; element.classList.remove("visible"); } } function isValidNumber(value, min, max) { return !isNaN(parseFloat(value)) && isFinite(value) && value >= min && value <= max; } function calculateLoad() { if (!thicknessInput) initializeElements(); // Initialize on first call if not already done var thickness = parseFloat(thicknessInput.value); var width = parseFloat(widthInput.value); var height = parseFloat(heightInput.value); // Note: This is often the depth if width is along the span, or vice-versa. We'll use 'height' as the dimension perpendicular to bending. var supportSpan = parseFloat(supportSpanInput.value); var loadType = loadTypeSelect.value; var pointLoadLocation = parseFloat(pointLoadLocationInput.value); var safetyFactor = parseFloat(safetyFactorInput.value); var errors = false; // Validation if (!isValidNumber(thickness, 0.1, 1000)) { showError(thicknessError, "Thickness must be a positive number."); errors = true; } else { hideError(thicknessError); } if (!isValidNumber(width, 1, 5000)) { showError(widthError, "Width must be between 1 and 5000 mm."); errors = true; } else { hideError(widthError); } if (!isValidNumber(height, 1, 5000)) { showError(heightError, "Height must be between 1 and 5000 mm."); errors = true; } else { hideError(heightError); } if (!isValidNumber(supportSpan, 1, 5000)) { showError(supportSpanError, "Support span must be between 1 and 5000 mm."); errors = true; } else { hideError(supportSpanError); } if (!isValidNumber(safetyFactor, 1, 10)) { showError(safetyFactorError, "Safety factor must be between 1.0 and 10.0."); errors = true; } else { hideError(safetyFactorError); } if (loadType === "point") { if (!isValidNumber(pointLoadLocation, 0, supportSpan)) { showError(pointLoadLocationError, "Point load location must be between 0 and the support span."); errors = true; } else { hideError(pointLoadLocationError); } } else { hideError(pointLoadLocationError); } if (errors) { mainResultDisplay.textContent = "–"; maxStressDisplay.textContent = "–"; maxDeflectionDisplay.textContent = "–"; allowableLoadDisplay.textContent = "–"; updateChart([], []); // Clear chart if there are errors return; } // Use 'height' as the dimension perpendicular to bending (h in formulas) and 'width' as the dimension parallel to bending (b in formulas) var h = height; // Acrylic thickness in mm var b = width; // Acrylic width in mm var L = supportSpan / 1000; // Span in meters var thickness_m = h / 1000; // Thickness in meters var width_m = b / 1000; // Width in meters var E = modulusOfElasticity; // Pa var I = (width_m * Math.pow(thickness_m, 3)) / 12; // Moment of Inertia in m^4 var maxStress_Pa = 0; var maxDeflection_m = 0; var calculatedTotalLoad_kg = 0; // Total weight the sheet can hold if (loadType === "uniform") { // We need to solve for 'w' (load per meter) such that stress and deflection are within limits. // Stress formula: sigma = (3 * w * L^2) / (2 * b * h^2) <- This is simplified stress, actual formula depends on w being per meter or per mm. Let's use w as load per meter. // Correct UDL Stress: sigma = (w * L^2) / 8 / (I / (h/2)) = (w * L^2 * h) / (8 * I) = (w * L^2 * h * 12) / (8 * b * h^3) = (3 * w * L^2) / (2 * b * h^2) — This is for center of beam, let's use this form. // Stress: Max stress occurs at center for UDL if simply supported: sigma = (w * L^2) / 8 / Z, where Z = I/(h/2) = (b*h^3/12) / (h/2) = b*h^2/6. So sigma = (w*L^2*6)/(8*b*h^2) = (3*w*L^2)/(4*b*h^2) ??? No, the common form is sigma = M*y/I where M is max bending moment. For UDL, M = w*L^2/8. Max y = h/2. sigma = (w*L^2/8)*(h/2) / I = (w*L^2*h)/(16*I) = (w*L^2*h*12)/(16*b*h^3) = (3*w*L^2)/(4*b*h^2). Okay let's use this one. // Deflection: delta = (5 * w * L^4) / (384 * E * I) // Let's rearrange for 'w' (load per meter) // w_stress = (AllowableStress * 2 * b * h_m^2) / (3 * L^2) — using the first stress formula I found. Let's verify. // From engineering handbooks, for UDL on a simply supported beam: Max Stress (sigma) = (w_per_unit_length * L^2) / 8 / (section_modulus). Section modulus Z = I/y = (bh^2/6). So sigma = (w_per_unit_length * L^2 * 6) / (8 * b * h^2) = (3 * w_per_unit_length * L^2) / (4 * b * h^2). // Let's use w_per_unit_length in N/m. var w_per_meter_N = (3 * (E * 0.00002) * L^2) / (4 * width_m * Math.pow(thickness_m, 2)); // Solve for w, assuming allowable stress is 20 MPa (a reasonable fraction of ultimate strength) var allowableStress_Pa = E * 0.00002; // Approx 20 MPa as max usable stress var w_stress_limit_N_per_m = (allowableStress_Pa * 4 * width_m * Math.pow(thickness_m, 2)) / (3 * L^2); var w_deflection_limit_N_per_m = (0.005 * 384 * E * I) / Math.pow(L, 4); // Assuming max allowable deflection of 5mm (0.005m) var w_N_per_m = Math.min(w_stress_limit_N_per_m, w_deflection_limit_N_per_m); var totalLoad_N = w_N_per_m * L; calculatedTotalLoad_kg = totalLoad_N / 9.81; // Convert Newtons to kg // Recalculate stress and deflection for the *actual* allowable load (not just the limit) maxStress_Pa = (3 * w_N_per_m * L^2) / (4 * width_m * Math.pow(thickness_m, 2)); maxDeflection_m = (5 * w_N_per_m * L^4) / (384 * E * I); } else if (loadType === "point") { // Point load formulas (simplified, assuming load at center for now, but calculator handles location) // Stress: sigma = (3 * P * L) / (4 * b * h^2) – Max stress at center point load // Deflection: delta = (P * L^3) / (48 * E * I) – Max deflection at center // Rearrange for 'P' (point load in Newtons) var allowableStress_Pa = E * 0.00002; // Approx 20 MPa // Handle point load location: Stress and deflection are highest at the center for a single point load spanning the full length. If load is off-center, it gets more complex (using Macaulay's method or superposition). For simplicity in this calculator, we'll assume the worst-case location is implicitly handled by the span calculation, but the stress/deflection formulas might need refinement for highly off-center loads. // Let's use a simplified approach: Assume the load P is applied at the center for max stress/deflection calculation purposes across the span L. // The 'pointLoadLocation' is more for user context, but the fundamental bending moment across L is key. // A point load P causes max bending moment M = P*L/4 at the center (for simply supported beam). // sigma = M*y/I = (P*L/4)*(h/2) / I = P*L*h / (8*I) = P*L*h*12 / (8*b*h^3) = (3*P*L) / (2*b*h^2). This formula seems correct. // delta = P*L^3 / (48*E*I) var P_stress_limit_N = (allowableStress_Pa * 2 * b * Math.pow(h, 2)) / (3 * L); // Oops, using mm here. Need meters P_stress_limit_N = (allowableStress_Pa * 2 * width_m * Math.pow(thickness_m, 2)) / (3 * L); // Max deflection limit is usually smaller than for UDL, say L/360. Let's use 5mm again for consistency, but this is application dependent. var max_deflection_m_limit = 0.005; // 5 mm var P_deflection_limit_N = (max_deflection_m_limit * 48 * E * I) / Math.pow(L, 3); var P_N = Math.min(P_stress_limit_N, P_deflection_limit_N); calculatedTotalLoad_kg = P_N / 9.81; // Convert Newtons to kg // Recalculate stress and deflection for the actual allowable load P_N maxStress_Pa = (3 * P_N * L) / (2 * width_m * Math.pow(thickness_m, 2)); maxDeflection_m = (P_N * Math.pow(L, 3)) / (48 * E * I); } // Apply Safety Factor var finalAllowableLoad_kg = calculatedTotalLoad_kg / safetyFactor; // Display Results mainResultDisplay.textContent = finalAllowableLoad_kg.toFixed(2); maxStressDisplay.textContent = (maxStress_Pa / 1e6).toFixed(2); // Convert Pa to MPa maxDeflectionDisplay.textContent = (maxDeflection_m * 1000).toFixed(2); // Convert m to mm allowableLoadDisplay.textContent = finalAllowableLoad_kg.toFixed(2); // Show the SF-adjusted load updateChart(safetyFactor); // Update chart with current settings } function updateChart(currentSafetyFactor) { if (!chart) return; var safetyFactors = []; var allowableLoads = []; var stresses = []; var thickness = parseFloat(thicknessInput.value) / 1000; // meters var width = parseFloat(widthInput.value) / 1000; // meters var height = parseFloat(heightInput.value) / 1000; // meters (this is the thickness dimension 'h' in formulas) var supportSpan = parseFloat(supportSpanInput.value) / 1000; // meters (this is the span 'L') var loadType = loadTypeSelect.value; var E = modulusOfElasticity; // Pa var I = (width * Math.pow(thickness, 3)) / 12; // Moment of Inertia in m^4 var allowableStress_Pa = E * 0.00002; // Approx 20 MPa // Define a range of safety factors to plot var sfStart = 1.1; var sfEnd = 5.0; var sfStep = 0.5; for (var sf = sfStart; sf { dataset.data = []; }); chart.update(); } } function copyResults() { var mainResult = mainResultDisplay.textContent; var maxStress = maxStressDisplay.textContent; var maxDeflection = maxDeflectionDisplay.textContent; var allowableLoad = allowableLoadDisplay.textContent; if (mainResult === "–") return; var thickness = thicknessInput.value; var width = widthInput.value; var height = heightInput.value; var supportSpan = supportSpanInput.value; var loadType = loadTypeSelect.options[loadTypeSelect.selectedIndex].text; var pointLoadLocation = ""; if (loadTypeSelect.value === "point") { pointLoadLocation = `Point Load Location: ${pointLoadLocationInput.value} mm\n`; } var safetyFactor = safetyFactorInput.value; var textToCopy = `— Acrylic Load Capacity Results —\n\n` + `Allowable Load: ${allowableLoad} kg\n` + `Max Stress: ${maxStress} MPa\n` + `Max Deflection: ${maxDeflection} mm\n\n` + `— Input Parameters —\n` + `Acrylic Thickness: ${thickness} mm\n` + `Panel Width: ${width} mm\n` + `Panel Height/Depth: ${height} mm\n` + `Support Span: ${supportSpan} mm\n` + `Load Type: ${loadType}\n` + `${pointLoadLocation}` + `Safety Factor: ${safetyFactor}\n\n` + `Note: Calculations based on standard acrylic properties and beam bending theory. Ensure safety margins are adequate for your specific application.`; navigator.clipboard.writeText(textToCopy).then(function() { // Success feedback could be added here (e.g., a temporary message) console.log('Results copied to clipboard!'); }).catch(function(err) { console.error('Failed to copy results: ', err); }); } // Initialize elements and show/hide point load details on load document.addEventListener('DOMContentLoaded', function() { initializeElements(); showPointLoadDetails(); // Set initial visibility loadTypeSelect.addEventListener('change', showPointLoadDetails); // Update when selection changes calculateLoad(); // Perform an initial calculation with default values }); // Add FAQ accordion functionality document.addEventListener('DOMContentLoaded', function() { var faqQuestions = document.querySelectorAll('.faq-section h3'); faqQuestions.forEach(function(question) { question.addEventListener('click', function() { var answer = this.nextElementSibling; if (answer.classList.contains('answer')) { answer.classList.toggle('visible'); } }); }); });

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