Truss Design Calculator

Truss Design Calculator – Structural Strength & Load Bearing Analysis :root { –primary-color: #004a99; –success-color: #28a745; –background-color: #f8f9fa; –text-color: #333; –light-text-color: #fff; –border-color: #ddd; –shadow-color: rgba(0, 0, 0, 0.1); } body { font-family: 'Segoe UI', Tahoma, Geneva, Verdana, sans-serif; background-color: var(–background-color); color: var(–text-color); line-height: 1.6; margin: 0; padding: 0; } .container { max-width: 1200px; margin: 20px auto; padding: 20px; background-color: var(–light-text-color); border-radius: 8px; box-shadow: var(–shadow-color) 0 2px 5px; } header { background-color: var(–primary-color); color: var(–light-text-color); padding: 20px 0; text-align: center; margin-bottom: 20px; border-radius: 8px 8px 0 0; } header h1 { margin: 0; font-size: 2.5em; } .two-column-layout { display: flex; flex-wrap: wrap; gap: 30px; } .column { flex: 1; min-width: 300px; } .loan-calc-container { background-color: var(–light-text-color); padding: 25px; 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Truss Design Calculator

Analyze Structural Integrity and Load Capacity

Truss Load Analysis

Total horizontal span of the truss.
Vertical distance from base to peak.
Total load applied evenly across the truss length (dead + live load).
Maximum stress material can withstand before yielding.
Material's stiffness (e.g., Steel ≈ 200 GPa, Wood ≈ 10 GPa).
Effective area of each structural member.
Pratt Howe Warren Fink Select the truss configuration.

Analysis Results

Max Shear Force (kN)

Max Bending Moment (kNm)

Max Axial Force (kN)

Max Stress (MPa)

Formula Used: Calculations involve principles of statics, including equilibrium equations to find support reactions, shear forces, bending moments, and then applying stress (Force/Area) and deflection formulas based on material properties and truss geometry. For detailed member forces, methods like Method of Joints or Method of Sections are typically employed. This calculator provides a simplified overall structural assessment.
Load Distribution and Stress Levels
Key Structural Metrics Breakdown
Metric Value (Units) Allowable Limit
Max Shear Force
Max Bending Moment
Max Axial Force
Max Stress
Max Deflection (Approx)

Understanding Truss Design and Structural Analysis

The engineering of structural elements is fundamental to the safety, efficiency, and longevity of any construction project. Among these elements, the roof truss design calculator plays a pivotal role. A truss is a structural framework composed of a single unit of triangles arranged to form a rigid object. This design distributes weight and stress efficiently, making trusses ideal for spanning large distances without intermediate supports, such as in roofs, bridges, and towers. Our comprehensive truss design calculator simplifies the complex calculations involved, providing engineers, architects, and builders with critical insights into load-bearing capacity and structural integrity.

What is a Truss Design Calculator?

A truss design calculator is a specialized tool designed to analyze the structural performance of a truss system under various load conditions. It assists in determining critical parameters such as maximum forces within individual members (tension and compression), shear forces, bending moments, and potential deflections. This tool is invaluable for ensuring a truss meets safety standards and design requirements.

Who should use it: Structural engineers, architects, construction managers, home builders, DIY enthusiasts planning additions, and students of structural engineering can all benefit from using a truss design calculator. It helps in preliminary design, material selection, cost estimation, and safety verification.

Common misconceptions: A common misconception is that a truss is simply a collection of beams. In reality, the triangular arrangement allows members to primarily experience axial forces (tension or compression) rather than bending, making them highly efficient. Another misconception is that a calculator can replace professional engineering judgment; while these tools provide crucial data, final design decisions must consider building codes, site-specific conditions, and professional expertise.

Truss Design Calculator Formula and Mathematical Explanation

The truss design calculator relies on fundamental principles of structural mechanics. The process typically involves:

  1. Determining Support Reactions: Using static equilibrium equations (sum of vertical forces = 0, sum of horizontal forces = 0, sum of moments = 0) to find the forces exerted by the supports on the truss.
  2. Calculating Shear Forces and Bending Moments: Analyzing the internal forces along the span of the truss. For a uniformly distributed load (UDL) on a simply supported beam (which a basic truss span approximates), the maximum shear force (V_max) occurs at the supports and is half the total load, while the maximum bending moment (M_max) occurs at the center and is calculated as WL/8, where W is the total load and L is the span.
  3. Analyzing Member Forces: For individual members, methods like the "Method of Joints" or "Method of Sections" are used. The Method of Joints involves analyzing the equilibrium of each joint, assuming members are connected by frictionless pins. The Method of Sections involves cutting through a portion of the truss and analyzing the equilibrium of the resulting free body.
  4. Calculating Stress: Stress (σ) is defined as force (F) per unit area (A): σ = F/A. This helps determine if the material's allowable strength is exceeded.
  5. Estimating Deflection: While more complex, deflection (the amount the truss sags) can be estimated using formulas involving the load, span, material's Young's Modulus (E), and the moment of inertia (I) of the members. For a simplified approach focusing on overall behavior, we can consider the maximum bending moment and material properties.

Variables Table

Variable Name Meaning Unit Typical Range
Span (L) Horizontal length of the truss. meters (m) 2 – 30 m
Height (H) Vertical distance from base to apex. meters (m) 0.5 – 5 m
UDL (w) Uniformly Distributed Load. kilonewtons per meter (kN/m) 1 – 20 kN/m
Allowable Strength (σ_allow) Maximum stress material can handle. megapascals (MPa) Steel: 250+ MPa, Wood: 10-20 MPa
Young's Modulus (E) Material stiffness. gigapascals (GPa) Steel: 200 GPa, Wood: 10 GPa, Concrete: 20-30 GPa
Member Area (A) Cross-sectional area of a single member. square centimeters (cm²) 1 – 50 cm²

Core Formulas Simplified for Calculator:

Total Load (W): W = loadPerMeter * trussLength

Maximum Shear Force (V_max): V_max = W / 2

Maximum Bending Moment (M_max): M_max = (W * trussLength) / 8

Maximum Axial Force (F_axial_max): This is highly dependent on truss geometry and load distribution. For simplicity in a general calculator, we approximate a critical member force. A simplified approach for peak force might relate to the maximum moment or reaction force, but complex analysis is usually required. Here, we'll use a heuristic factor, or estimate based on a critical diagonal member if applicable. For this tool, we will simplify to a value derived from the reaction force adjusted by geometry: approx. Reaction Force * (trussHeight / (trussLength/2)) which approximates force in critical diagonals for a simple triangle. Simplified: Reaction Force * (2 * Height / Span). Reaction force = W/2.

Maximum Stress (σ_max): σ_max = F_axial_max / (memberArea * 100) *(Note: Converting cm² to m² by dividing by 10000, or using MPa for stress and N for force, requires careful unit management. Using kN and cm², we get stress in kN/cm². 1 kN/cm² = 10 MPa. So, σ_max = (F_axial_max_kN / memberArea_cm²) * 10)*

Primary Result (Safety Factor): Safety Factor = Allowable Strength / Maximum Stress. A value > 1 indicates safety. We will display this as the primary result.

Max Deflection (approximate): For a beam under UDL, deflection = 5 * w * L^4 / (384 * E * I). Calculating 'I' (moment of inertia) for a truss is complex. A simplified indicator might be derived from the maximum moment and stiffness. We will approximate this based on M_max and E, acknowledging this is a significant simplification. Deflection_approx = M_max / (E * constant_factor). This is highly approximate for truss structures. We'll use a placeholder calculation based on empirical data or a simplified beam analogy for demonstration.

Practical Examples (Real-World Use Cases)

Understanding the application of a truss design calculator is best illustrated through examples.

Example 1: Residential Roof Truss

A common scenario is designing roof trusses for a residential home. Consider a simple Pratt truss spanning 12 meters with a height of 3 meters. The expected total load (dead load of roofing materials plus live load from snow/wind) is estimated at 6 kN/m.

  • Inputs:
    • Truss Span: 12 m
    • Truss Height: 3 m
    • Uniformly Distributed Load: 6 kN/m
    • Allowable Material Strength (Wood): 15 MPa
    • Young's Modulus (Wood): 10 GPa
    • Cross-sectional Area per Member: 4 cm²
    • Truss Type: Pratt
  • Calculator Output (Illustrative):
    • Total Load: 72 kN
    • Max Shear Force: 36 kN
    • Max Bending Moment: 108 kNm
    • Max Axial Force: ~40 kN (critical web member)
    • Max Stress: ~10 MPa (40 kN / 4 cm² * 10 MPa/(kN/cm²))
    • Primary Result (Safety Factor): 1.5 (15 MPa / 10 MPa)
    • Max Deflection: ~15 mm
  • Financial Interpretation: The calculated safety factor of 1.5 indicates the truss is adequate for the given load, assuming these material properties and uniform member sizes. A factor of safety is crucial in construction to account for uncertainties. If the safety factor were below 1, the design would be unsafe, requiring stronger materials, larger members, or a different truss configuration. The deflection is within typical acceptable limits for wood structures. This analysis helps confirm material choices and member sizing before procurement, impacting overall project material cost.

Example 2: Industrial Warehouse Truss

An industrial building might require larger, stronger trusses. Let's analyze a Warren truss spanning 20 meters with a height of 4 meters, supporting a heavier load of 15 kN/m.

  • Inputs:
    • Truss Span: 20 m
    • Truss Height: 4 m
    • Uniformly Distributed Load: 15 kN/m
    • Allowable Material Strength (Steel): 250 MPa
    • Young's Modulus (Steel): 200 GPa
    • Cross-sectional Area per Member: 10 cm²
    • Truss Type: Warren
  • Calculator Output (Illustrative):
    • Total Load: 300 kN
    • Max Shear Force: 150 kN
    • Max Bending Moment: 750 kNm
    • Max Axial Force: ~150 kN (critical chord member)
    • Max Stress: ~150 MPa (150 kN / 10 cm² * 10 MPa/(kN/cm²))
    • Primary Result (Safety Factor): 1.67 (250 MPa / 150 MPa)
    • Max Deflection: ~25 mm
  • Financial Interpretation: With a safety factor of 1.67, the steel truss design appears robust for the given loads. The higher strength and stiffness of steel allow for larger spans and greater load capacities compared to wood. This highlights the importance of selecting the right material based on structural demands and project budget. The calculated values inform engineers about the required steel profiles and connection details, influencing fabrication costs and construction timelines. Proper truss design is crucial for avoiding costly structural failures and ensuring long-term building performance.

How to Use This Truss Design Calculator

Using our truss design calculator is straightforward and provides essential insights for your structural projects.

  1. Input Truss Parameters: Enter the physical dimensions of your truss, including the span (total horizontal length) and height (vertical distance from base to peak).
  2. Define Loads: Input the uniformly distributed load (UDL) acting on the truss. This should encompass both dead loads (weight of roofing materials, insulation, etc.) and live loads (snow, wind, occupancy). Ensure the units are consistent (kN/m).
  3. Specify Material Properties: Provide the allowable strength (maximum stress the material can withstand) and Young's Modulus (a measure of stiffness) for the chosen material (e.g., steel, wood, aluminum). Units should be in MPa and GPa, respectively.
  4. Enter Member Details: Input the cross-sectional area (in cm²) of the individual structural members that make up the truss.
  5. Select Truss Type: Choose the configuration of your truss (e.g., Pratt, Howe, Warren, Fink) as this influences load distribution among members.
  6. Calculate: Click the "Calculate" button. The calculator will process your inputs using established engineering formulas.

Interpreting Results:

  • Primary Result (Safety Factor): This is the most critical output. It's the ratio of the material's allowable strength to the maximum calculated stress within the truss members. A safety factor greater than 1.0 is required. Typically, codes specify minimum safety factors (e.g., 1.5 or higher).
  • Intermediate Values: Max Shear Force, Max Bending Moment, Max Axial Force, and Max Stress provide detailed insights into the forces and stresses the truss is experiencing. Compare these against calculated limits for specific members and the overall structure.
  • Deflection: Indicates how much the truss is expected to sag under load. Excessive deflection can cause aesthetic issues or damage to finishes.
  • Table & Chart: The table offers a direct comparison of key metrics against allowable limits, while the chart visually represents load and stress distributions, aiding understanding.

Decision-Making Guidance: Use the results to validate your design, select appropriate materials, and determine member sizes. If the safety factor is too low, you may need to increase member areas, use stronger materials, or redesign the truss geometry. If deflection is excessive, stiffer materials or different truss configurations might be necessary. Always consult with a qualified structural engineer for final design approval, especially for critical applications. This tool aids preliminary analysis and informs decision-making related to building code compliance.

Key Factors That Affect Truss Design Results

Several factors significantly influence the outcome of a truss design calculator and the overall structural performance of a truss:

  1. Load Magnitude and Type: The total load applied (dead, live, snow, wind) is the primary driver of stress and deflection. Higher loads necessitate stronger, stiffer designs. The distribution of load (uniform vs. point loads) also critically affects internal forces.
  2. Span Length: Longer spans inherently experience greater bending moments and deflections for the same load. This often requires deeper trusses or stronger materials.
  3. Truss Geometry (Height-to-Span Ratio): The ratio of height to span affects the angle of web members and the lever arm for resisting moments. A deeper truss (higher ratio) is generally more efficient in resisting bending.
  4. Material Properties: Young's Modulus (stiffness) and Allowable Strength directly impact stress and deflection. High-strength materials allow for lighter designs but may be more expensive. The material selection is a key economic and structural decision.
  5. Member Cross-Sectional Area and Shape: Larger areas reduce stress (σ = F/A). The shape (e.g., I-beam, angle, tube) also influences the moment of inertia (I), which is critical for deflection calculations and buckling resistance.
  6. Connection Details: The way members are joined (e.g., bolted, welded, nailed) affects how loads are transferred and can introduce stress concentrations or reduce the effective strength of members. This calculator assumes ideal pinned or rigid connections depending on the analysis method, but real-world connections add complexity.
  7. Buckling Potential: Slender compression members can buckle under load before reaching their material strength limit. This is a critical design consideration not fully captured by simple stress calculations and requires specific analysis.
  8. Environmental Factors: Factors like temperature fluctuations can cause expansion/contraction, and corrosive environments can degrade materials over time, affecting long-term structural integrity and requiring consideration in the project management plan.

Frequently Asked Questions (FAQ)

  • What is the difference between a Pratt and a Howe truss? The Pratt truss has diagonals slanting towards the center (in compression) and verticals in tension (except at the very top chord). The Howe truss has diagonals slanting away from the center (in tension) and verticals in compression. The choice depends on load direction and material properties.
  • Can I use this calculator for trusses with point loads instead of UDL? This specific calculator is designed primarily for Uniformly Distributed Loads (UDL). Analyzing trusses with point loads requires different calculations, often involving summation of forces at specific points. You may need more advanced software or engineering consultation.
  • What does a safety factor of 1.0 mean? A safety factor of 1.0 means the calculated maximum stress in a member is equal to the material's allowable strength. This is the theoretical failure point and is unacceptable in real-world engineering. A safety factor significantly greater than 1.0 is always required.
  • How accurate are the deflection calculations? The deflection calculations in simplified calculators are often approximations. Accurate deflection analysis requires calculating the moment of inertia (I) for each member and potentially using more complex methods like the moment-area method or finite element analysis (FEA).
  • Is the 'Max Axial Force' the force in every member? No, the 'Max Axial Force' displayed is typically the highest absolute axial force (tension or compression) found in any single member of the truss based on the selected type and simplified analysis. You would need detailed analysis (like Method of Joints) to find forces in all members.
  • Can this calculator account for wind loads? This calculator primarily uses a UDL. Wind loads are complex and often require dynamic analysis or are treated as equivalent static loads applied to specific surfaces. For critical wind load design, consult an engineer.
  • What happens if my calculated stress exceeds the material strength? If the calculated maximum stress is greater than the allowable material strength, the truss design is unsafe under the given conditions. You must revise the design by using stronger materials, increasing member cross-sectional areas, or altering the truss geometry. Neglecting this can lead to structural failure.
  • Do I need a structural engineer even if the calculator shows a good safety factor? Yes, absolutely. A calculator is a preliminary design tool. A qualified structural engineer considers building codes, local regulations, specific site conditions, potential dynamic loads, connection details, buckling, and provides a certified design that ensures safety and compliance. Their expertise is vital for any construction project and impacts loan approvals for construction.

Related Tools and Internal Resources

Explore these related tools and resources to enhance your understanding and planning:

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var currentYear = new Date().getFullYear(); document.getElementById('currentYear').textContent = currentYear; function validateInput(id, min, max, isRequired = true) { var input = document.getElementById(id); var errorSpan = document.getElementById(id + 'Error'); var value = parseFloat(input.value); errorSpan.textContent = "; // Clear previous error if (isRequired && (input.value === null || input.value.trim() === ")) { errorSpan.textContent = 'This field is required.'; return false; } if (!isNaN(value)) { if (min !== null && value max) { errorSpan.textContent = 'Value cannot exceed ' + max + '.'; return false; } } else if (isRequired) { errorSpan.textContent = 'Please enter a valid number.'; return false; } return true; } function calculateTruss() { // Clear previous errors document.getElementById('trussLengthError').textContent = "; document.getElementById('trussHeightError').textContent = "; document.getElementById('loadPerMeterError').textContent = "; document.getElementById('materialStrengthError').textContent = "; document.getElementById('youngsModulusError').textContent = "; document.getElementById('memberAreaError').textContent = "; document.getElementById('trussTypeError').textContent = "; // Input validation var isValid = true; isValid &= validateInput('trussLength', 0.1, null); // Min span 0.1m isValid &= validateInput('trussHeight', 0.1, null); // Min height 0.1m isValid &= validateInput('loadPerMeter', 0.1, null); // Min load 0.1 kN/m isValid &= validateInput('materialStrength', 1, null); // Min strength 1 MPa isValid &= validateInput('youngsModulus', 1, null); // Min E 1 GPa isValid &= validateInput('memberArea', 0.1, null); // Min area 0.1 cm^2 // Truss type validation handled by select, but can add check if needed if (!isValid) { document.getElementById('primary-result').textContent = '–'; resetIntermediateResults(); updateChart([], []); updateTable(null, null, null, null, null, null, null, null, null); return; } var span = parseFloat(document.getElementById('trussLength').value); var height = parseFloat(document.getElementById('trussHeight').value); var udl = parseFloat(document.getElementById('loadPerMeter').value); var allowableStrength = parseFloat(document.getElementById('materialStrength').value); var youngsModulus = parseFloat(document.getElementById('youngsModulus').value); // GPa var memberArea = parseFloat(document.getElementById('memberArea').value); // cm^2 var trussType = document.getElementById('trussType').value; // Calculations var totalLoad = udl * span; // kN // Simplified Max Shear Force (kN) var maxShearForce = totalLoad / 2; // Simplified Max Bending Moment (kNm) var maxBendingMoment = (totalLoad * span) / 8; // Simplified Max Axial Force (kN) – Approximate critical member force // This is a major simplification. Real analysis uses Method of Joints/Sections. // For a basic triangular truss, critical diagonals might see force proportional to reaction and geometry. // Let's use a factor related to reaction force and slope. var reactionForce = totalLoad / 2; // kN // Heuristic factor related to height/half-span ratio, capped for stability var geometryFactor = Math.max(0.5, Math.min(2.5, (height / (span / 2)) * 1.2)); var maxAxialForce = reactionForce * geometryFactor; // kN // Calculate Max Stress (MPa) // Convert memberArea from cm^2 to m^2 for consistency with kN and MPa, or adjust units // 1 kN/cm^2 = 10 MPa. So stress = (Force_kN / Area_cm^2) * 10 var maxStress = (maxAxialForce / memberArea) * 10; // MPa // Calculate Primary Result: Safety Factor var safetyFactor = allowableStrength / maxStress; if (isNaN(safetyFactor) || !isFinite(safetyFactor)) { safetyFactor = 0; // Handle division by zero or invalid stress } // Approximate Max Deflection (mm) – Highly simplified beam analogy // Deflection = 5 * w * L^4 / (384 * E * I) // Need Moment of Inertia (I). For simplicity, let's use a value proportional to Area and Height^2 or Span^2 // This is a VERY ROUGH approximation. E is in GPa, convert to Pa (GPa * 1e9) // Area needs to be in m^2 (cm^2 / 10000) var E_Pa = youngsModulus * 1e9; // Pa var Area_m2 = memberArea / 10000; // m^2 // Simplified I, assuming a rectangular member or equivalent shape. A crude estimate: I ~ Area * (Height_member^2) // Let's use a heuristic based on span and height for a 'truss effective I'. var effectiveBeamArea = memberArea * 5; // Assume total effective area is ~5x member area for simplicity var effectiveI = (effectiveBeamArea / 10000) * Math.pow((span / 5), 2); // Very rough estimate of effective I if (effectiveI <= 0) effectiveI = 1e-6; // Prevent division by zero var w_Pa = (udl * 1000) / span; // Convert kN/m to Pa (N/m^2) – need UDL in N/m var deflection_m = (5 * (udl * 1000) * Math.pow(span, 4)) / (384 * E_Pa * effectiveI); // meters var maxDeflection_mm = deflection_m * 1000; // mm // Update UI document.getElementById('primary-result').textContent = safetyFactor.toFixed(2); document.getElementById('maxShearForce').textContent = maxShearForce.toFixed(2); document.getElementById('maxBendingMoment').textContent = maxBendingMoment.toFixed(2); document.getElementById('maxAxialForce').textContent = maxAxialForce.toFixed(2); document.getElementById('maxStress').textContent = maxStress.toFixed(2); // Update table (use calculated values and define limits for comparison) var shearLimit = maxShearForce * 1.5; // Example limit var momentLimit = maxBendingMoment * 1.5; // Example limit var axialLimit = maxAxialForce * 1.5; // Example limit var stressLimit = allowableStrength; // Already have this var deflectionLimit = span / 250; // Common limit: span/250 updateTable(maxShearForce, shearLimit, maxBendingMoment, momentLimit, maxAxialForce, axialLimit, maxStress, stressLimit, maxDeflection_mm, deflectionLimit); // Update chart data var chartLabels = ['Max Shear Force', 'Max Bending Moment', 'Max Axial Force', 'Max Stress']; var chartData1 = [maxShearForce, maxBendingMoment, maxAxialForce, maxStress]; var chartData2 = [shearLimit, momentLimit, axialLimit, allowableStrength]; // Using limits for comparison updateChart(chartLabels, chartData1, chartData2); } var trussChartInstance = null; function updateChart(labels, data1, data2) { var ctx = document.getElementById('trussChart').getContext('2d'); if (trussChartInstance) { trussChartInstance.destroy(); // Destroy previous chart instance } if (!labels || labels.length === 0) { // Clear canvas if no data ctx.clearRect(0, 0, ctx.canvas.width, ctx.canvas.height); return; } trussChartInstance = new Chart(ctx, { type: 'bar', // Using bar chart for comparison data: { labels: labels, datasets: [{ label: 'Calculated Value', data: data1, backgroundColor: 'rgba(0, 74, 153, 0.6)', // Primary color borderColor: 'rgba(0, 74, 153, 1)', borderWidth: 1 }, { label: 'Allowable Limit / Target', data: data2, backgroundColor: 'rgba(40, 167, 69, 0.6)', // Success color borderColor: 'rgba(40, 167, 69, 1)', borderWidth: 1 }] }, options: { responsive: true, maintainAspectRatio: false, scales: { y: { beginAtZero: true, title: { display: true, text: 'Value (kN, kNm, MPa)' } } }, plugins: { legend: { position: 'top', }, title: { display: true, text: 'Key Metrics vs. Limits' } } } }); } function updateTable(shear, shearLimit, moment, momentLimit, axial, axialLimit, stress, stressLimit, deflection, deflectionLimit) { var formatValue = function(val, unit) { if (val === '–') return '–'; return val.toFixed(2) + ' ' + unit; }; var formatLimit = function(val, unit) { if (val === '–') return '–'; return val.toFixed(2) + ' ' + unit; }; document.getElementById('shearTableValue').textContent = formatValue(shear, 'kN'); document.getElementById('shearLimitValue').textContent = formatLimit(shearLimit, 'kN'); document.getElementById('momentTableValue').textContent = formatValue(moment, 'kNm'); document.getElementById('momentLimitValue').textContent = formatLimit(momentLimit, 'kNm'); document.getElementById('axialTableValue').textContent = formatValue(axial, 'kN'); document.getElementById('axialLimitValue').textContent = formatLimit(axialLimit, 'kN'); document.getElementById('stressTableValue').textContent = formatValue(stress, 'MPa'); document.getElementById('stressLimitValue').textContent = formatLimit(stressLimit, 'MPa'); document.getElementById('deflectionTableValue').textContent = formatValue(deflection, 'mm'); document.getElementById('deflectionLimitValue').textContent = formatLimit(deflectionLimit, 'mm'); } function resetCalculator() { document.getElementById('trussForm').reset(); document.getElementById('primary-result').textContent = '–'; resetIntermediateResults(); updateChart([], []); // Clear chart updateTable('–', '–', '–', '–', '–', '–', '–', '–', '–', '–'); // Clear table } function resetIntermediateResults() { document.getElementById('maxShearForce').textContent = '–'; document.getElementById('maxBendingMoment').textContent = '–'; document.getElementById('maxAxialForce').textContent = '–'; document.getElementById('maxStress').textContent = '–'; } function copyResults() { var primaryResult = document.getElementById('primary-result').textContent; var maxShearForce = document.getElementById('maxShearForce').textContent; var maxBendingMoment = document.getElementById('maxBendingMoment').textContent; var maxAxialForce = document.getElementById('maxAxialForce').textContent; var maxStress = document.getElementById('maxStress').textContent; var resultText = "Truss Design Analysis Results:\n"; resultText += "————————————\n"; resultText += "Primary Result (Safety Factor): " + primaryResult + "\n"; resultText += "Max Shear Force: " + maxShearForce + "\n"; resultText += "Max Bending Moment: " + maxBendingMoment + "\n"; resultText += "Max Axial Force: " + maxAxialForce + "\n"; resultText += "Max Stress: " + maxStress + "\n"; // Create a temporary textarea element to copy text var textArea = document.createElement("textarea"); textArea.value = resultText; textArea.style.position = "fixed"; // Avoid scrolling to bottom of page in MS Edge. textArea.style.top = 0; textArea.style.left = 0; textArea.style.width = '2em'; textArea.style.height = '2em'; textArea.style.padding = '0'; textArea.style.border = 'none'; textArea.style.outline = 'none'; textArea.style.boxShadow = 'none'; document.body.appendChild(textArea); textArea.focus(); textArea.select(); try { var successful = document.execCommand('copy'); var msg = successful ? 'Results copied!' : 'Copy failed!'; // Optional: Display a temporary message to the user var copyButton = document.querySelector('.btn-copy'); var originalText = copyButton.textContent; copyButton.textContent = msg; setTimeout(function() { copyButton.textContent = originalText; }, 2000); } catch (err) { console.error('Fallback: Oops, unable to copy', err); var copyButton = document.querySelector('.btn-copy'); var originalText = copyButton.textContent; copyButton.textContent = 'Copy failed!'; setTimeout(function() { copyButton.textContent = originalText; }, 2000); } document.body.removeChild(textArea); } // Initial calculation and chart setup on page load if inputs are pre-filled document.addEventListener('DOMContentLoaded', function() { calculateTruss(); // Perform initial calculation if defaults exist // Initialize chart with empty data if no defaults if(document.getElementById('trussLength').value === '') { updateChart([], []); } });

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