How to Calculate Weight Distribution on a Beam

Beam Weight Distribution Calculator & Guide :root { –primary-color: #004a99; –success-color: #28a745; –background-color: #f8f9fa; –text-color: #333; –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); margin: 0; padding: 0; line-height: 1.6; } .container { max-width: 1000px; margin: 20px auto; padding: 20px; background-color: #fff; border-radius: 8px; box-shadow: 0 4px 15px var(–shadow-color); } h1, h2, h3 { color: var(–primary-color); margin-bottom: 15px; } h1 { text-align: center; font-size: 2.2em; } h2 { font-size: 1.8em; border-bottom: 2px solid var(–primary-color); padding-bottom: 5px; margin-top: 30px; } h3 { font-size: 1.4em; margin-top: 25px; } .loan-calc-container { background-color: #eef2f7; padding: 25px; border-radius: 8px; margin-top: 20px; box-shadow: inset 0 1px 3px var(–shadow-color); } .input-group { margin-bottom: 20px; display: flex; flex-direction: column; } .input-group label { display: block; margin-bottom: 8px; font-weight: bold; color: var(–primary-color); } .input-group input[type="number"], .input-group select { width: 100%; padding: 12px 15px; border: 1px solid var(–border-color); border-radius: 4px; box-sizing: border-box; font-size: 1em; transition: border-color 0.3s ease; } .input-group input[type="number"]:focus, .input-group select:focus { border-color: var(–primary-color); outline: none; } .input-group .helper-text { font-size: 0.85em; color: #666; margin-top: 5px; } .error-message { color: #dc3545; font-size: 0.8em; margin-top: 5px; display: none; /* Hidden by default */ } .error-message.visible { display: block; } .button-group { display: flex; justify-content: space-between; margin-top: 25px; gap: 10px; } .button-group button { flex: 1; padding: 12px 20px; border: none; border-radius: 5px; cursor: pointer; font-size: 1em; font-weight: bold; transition: background-color 0.3s ease, transform 0.2s ease; } .button-group button.primary { background-color: var(–primary-color); color: white; } .button-group button.primary:hover { background-color: #003366; transform: translateY(-2px); } .button-group button.secondary { background-color: #6c757d; color: white; } .button-group button.secondary:hover { background-color: #5a6268; transform: translateY(-2px); } .results-container { margin-top: 30px; padding: 20px; background-color: #fff; border: 1px solid var(–border-color); border-radius: 8px; text-align: center; } .results-container h3 { margin-top: 0; color: var(–primary-color); } .main-result { font-size: 2.5em; font-weight: bold; color: var(–success-color); margin: 15px 0; padding: 15px; background-color: #e9f7ef; border-radius: 5px; border: 2px dashed var(–success-color); } .intermediate-results div, .assumptions div { margin-bottom: 10px; font-size: 1.1em; } .intermediate-results span, .assumptions span { font-weight: bold; color: var(–primary-color); margin-left: 5px; } table { width: 100%; border-collapse: collapse; margin-top: 20px; box-shadow: 0 2px 5px var(–shadow-color); } th, td { padding: 12px 15px; text-align: left; border: 1px solid var(–border-color); } th { background-color: var(–primary-color); color: white; font-weight: bold; } tr:nth-child(even) { background-color: #f2f7fc; } caption { font-size: 1.1em; font-weight: bold; color: var(–primary-color); margin-bottom: 10px; caption-side: top; text-align: left; } canvas { margin-top: 20px; border: 1px solid var(–border-color); border-radius: 4px; background-color: #fff; } .chart-legend { margin-top: 15px; text-align: center; font-size: 0.9em; color: #555; } .chart-legend span { display: inline-block; margin: 0 10px; position: relative; padding-left: 15px; } .chart-legend span::before { content: "; position: absolute; left: 0; top: 50%; transform: translateY(-50%); width: 10px; height: 10px; border-radius: 2px; } .legend-shear::before { background-color: #1f77b4; } .legend-moment::before { background-color: #ff7f0e; } footer { text-align: center; margin-top: 40px; padding: 20px; font-size: 0.9em; color: #777; border-top: 1px solid var(–border-color); } .article-content { background-color: #fff; padding: 30px; border-radius: 8px; box-shadow: 0 4px 15px var(–shadow-color); margin-top: 20px; } .article-content p { margin-bottom: 15px; } .article-content a { color: var(–primary-color); text-decoration: none; transition: color 0.3s ease; } .article-content a:hover { color: #003366; text-decoration: underline; } /* Responsive adjustments */ @media (max-width: 768px) { .container { margin: 10px; padding: 15px; } h1 { font-size: 1.8em; } h2 { font-size: 1.5em; } .button-group { flex-direction: column; } .button-group button { width: 100%; } }

Beam Weight Distribution Calculator

Accurately determine shear force and bending moments along a beam for structural analysis and safety.

Beam Load Analysis Inputs

Enter the total length of the beam in meters (m).
Enter the magnitude of a single, concentrated load in Newtons (N).
Enter the distance from the left support to the load in meters (m). Must be < Beam Length.
Pin Support (Allows rotation, resists vertical and horizontal forces) Roller Support (Allows rotation and horizontal movement, resists vertical forces)
Select the type of support on the left end of the beam.
Pin Support (Allows rotation, resists vertical and horizontal forces) Roller Support (Allows rotation and horizontal movement, resists vertical forces)
Select the type of support on the right end of the beam.

Analysis Results

0.00 N
Max Shear Force: 0.00 N
Max Bending Moment: 0.00 Nm
Reaction Force (Left): 0.00 N
Reaction Force (Right): 0.00 N

Assumptions:

Beam is straight and has uniform cross-section.
Supports are simple (pin or roller).
Load is a single concentrated force.
Left Support: Pin
Right Support: Roller
Please enter valid inputs above to see the analysis results.

Shear Force and Bending Moment Diagrams

Shear Force Bending Moment
Chart will update with valid inputs.

Beam Load Analysis Table

Beam Load Analysis Details
Location (m) Shear Force (N) Bending Moment (Nm)
Table will populate with valid inputs.

What is Beam Weight Distribution Analysis?

Beam weight distribution analysis, more accurately termed beam load analysis in structural engineering, is the process of calculating the internal forces and stresses that develop within a structural beam when it is subjected to external loads and support conditions. This analysis is fundamental to ensuring that a beam can safely carry the intended loads without failure due to excessive bending, shear, or deflection. It helps engineers and designers determine the optimal beam size, material, and support type required for a specific application, from bridges and buildings to simple shelving units.

This type of analysis is crucial for anyone involved in structural design, construction, or even DIY projects where a beam is used to support weight. This includes:

  • Civil and Structural Engineers: Designing bridges, buildings, and other large structures.
  • Mechanical Engineers: Designing machine frames, support structures, and components.
  • Architects: Understanding load-bearing requirements for aesthetic designs.
  • Construction Professionals: Ensuring safe and proper installation of structural elements.
  • DIY Enthusiasts: Building shelves, decks, pergolas, or any structure requiring a load-bearing beam.

Common misconceptions include assuming that a beam only experiences simple downward force, or that the strength of the beam is solely determined by its material without considering the distribution of loads and support types. Another misconception is that calculating these forces is overly complex for non-professionals; while professional standards require advanced calculations, understanding the principles and using tools like this calculator can provide valuable insights.

Beam Load Analysis Formula and Mathematical Explanation

The analysis of a simply supported beam with a single concentrated load involves calculating support reactions, shear forces, and bending moments. Let's break down the formulas for a beam of length 'L', with a concentrated load 'P' at a distance 'a' from the left support (Reaction RA) and 'b' from the right support (Reaction RB). Note that L = a + b.

1. Support Reactions (RA and RB)

To find the vertical support reactions, we use the principles of static equilibrium:

  • Sum of vertical forces = 0: RA + RB – P = 0
  • Sum of moments about a point = 0: We'll take moments about support A. The clockwise moment due to P must equal the counter-clockwise moment due to RB.

Moment Equation about A:

P * a – RB * L = 0

Therefore, RB = (P * a) / L

Substitute RB back into the force equation:

RA + (P * a) / L – P = 0

RA = P – (P * a) / L

RA = P * (1 – a/L) = P * (L – a) / L = P * b / L

2. Shear Force (V)

Shear force at any point along the beam is the algebraic sum of the vertical forces to the left (or right) of that point. For a single concentrated load:

  • For x < a (left of the load): V = RA
  • For x > a (right of the load): V = RA – P

The shear force is constant between points of loading or support.

3. Bending Moment (M)

Bending moment at any point is the algebraic sum of the moments of all forces to the left (or right) of that point. For a single concentrated load:

  • For x < a (left of the load): M = RA * x
  • For x > a (right of the load): M = RA * x – P * (x – a)

The bending moment is maximum directly under the concentrated load if it's between the supports, or at the point where the shear force crosses zero.

Variable Table:

Load Analysis Variables
Variable Meaning Unit Typical Range/Notes
L Beam Length meters (m) Positive value, e.g., 1m to 20m+
P Concentrated Load Value Newtons (N) Positive value, e.g., 100N to 50000N+
a Load Position (from left support) meters (m) 0m < a < L
b Load Position (from right support) meters (m) b = L – a
RA Reaction Force at Left Support Newtons (N) Calculated value
RB Reaction Force at Right Support Newtons (N) Calculated value
V(x) Shear Force at location x Newtons (N) Varies along the beam
M(x) Bending Moment at location x Newton-meters (Nm) Varies along the beam

Practical Examples (Real-World Use Cases)

Understanding how to calculate weight distribution on a beam is vital in many scenarios. Here are two practical examples:

Example 1: Residential Deck Support Beam

A homeowner is building a deck and needs to support a joist with a single beam spanning 4 meters between two posts. The beam needs to support a concentrated load from the joist directly in the center (2 meters from either end). This concentrated load is estimated to be 8,000 N (from flooring, snow load, and the joist itself).

  • Inputs:
  • Beam Length (L) = 4 m
  • Concentrated Load (P) = 8000 N
  • Load Position (a) = 2 m
  • Support Types: Both are Pin Supports (common for posts)

Using the calculator or formulas:

  • RA = (P * b) / L = (8000 N * 2 m) / 4 m = 4000 N
  • RB = (P * a) / L = (8000 N * 2 m) / 4 m = 4000 N
  • Max Shear Force = RA = 4000 N (just to the right of RA) and RB = 4000 N (just to the left of RB). The shear value is -4000 N just to the right of the load P. The absolute maximum shear occurs at the supports.
  • Max Bending Moment occurs at x = a = 2 m: M = RA * a = 4000 N * 2 m = 8000 Nm

Interpretation: The beam experiences equal reaction forces of 4000 N at each support. The maximum shear force is 4000 N, and the maximum bending moment is 8000 Nm. This bending moment value is critical for selecting a beam (e.g., a specific size of wooden or steel beam) that can withstand this stress without excessive deflection or failure.

Example 2: Workshop Shelf

A craftsman installs a sturdy shelf in his workshop. The shelf is a steel beam with a total length of 1.5 meters, supported by a pin support on the left and a roller support on the right. He places a heavy piece of equipment weighing 2000 N at a distance of 0.5 meters from the left support.

  • Inputs:
  • Beam Length (L) = 1.5 m
  • Concentrated Load (P) = 2000 N
  • Load Position (a) = 0.5 m
  • Left Support Type: Pin
  • Right Support Type: Roller

Using the calculator or formulas:

  • b = L – a = 1.5 m – 0.5 m = 1.0 m
  • RA = (P * b) / L = (2000 N * 1.0 m) / 1.5 m ≈ 1333.33 N
  • RB = (P * a) / L = (2000 N * 0.5 m) / 1.5 m ≈ 666.67 N
  • Max Shear Force = RA ≈ 1333.33 N (left of load) and RA – P ≈ 1333.33 N – 2000 N ≈ -666.67 N (right of load). The absolute max shear is 1333.33 N at the left support.
  • Max Bending Moment occurs at x = a = 0.5 m: M = RA * a = 1333.33 N * 0.5 m ≈ 666.67 Nm

Interpretation: The pin support on the left carries a larger reaction force (1333.33 N) compared to the roller support on the right (666.67 N), which is expected as the load is closer to the left support. The maximum bending moment of approximately 666.67 Nm indicates the point of maximum stress on the shelf beam.

How to Use This Beam Load Analysis Calculator

Our calculator simplifies the process of understanding beam loading. Follow these steps:

  1. Enter Beam Length (L): Input the total span of the beam in meters.
  2. Enter Concentrated Load (P): Specify the magnitude of the main load acting on the beam in Newtons. If you have a distributed load, you might need to approximate its effect as a concentrated load at its centroid or use more advanced calculators.
  3. Enter Load Position (a): Provide the distance from the left end of the beam to where the concentrated load is applied, in meters. Ensure this value is less than the total beam length.
  4. Select Support Types: Choose the type of support (Pin or Roller) for both the left and right ends of the beam. This affects how forces are distributed and resisted. A pin support resists both vertical and horizontal forces, while a roller support primarily resists vertical forces and allows horizontal movement.
  5. Click 'Calculate Load Distribution': The calculator will instantly compute and display the key results.

Reading the Results:

  • Main Highlighted Result: This typically shows the maximum bending moment, often the most critical factor for beam failure due to excessive stress.
  • Intermediate Values: These include the maximum shear force and the reaction forces at each support. These are essential for assessing different failure modes and ensuring support structures are adequate.
  • Assumptions: Review the listed assumptions to understand the context of the calculated results.
  • Shear Force and Bending Moment Diagrams: The chart visually represents how shear force and bending moment change along the length of the beam. The peak values on the chart correspond to the calculated maximums.
  • Analysis Table: This table provides specific values for shear force and bending moment at various points along the beam, useful for detailed design.

Decision-Making Guidance:

Compare the calculated maximum shear force and bending moment against the material properties and design specifications of the beam you intend to use. If the calculated stresses exceed the allowable limits for the material, you must choose a stronger beam, adjust the load, modify the span, or change the support conditions. Always consult relevant engineering codes and standards for critical applications.

Key Factors That Affect Beam Load Analysis Results

Several factors significantly influence the outcome of beam load analysis:

  1. Magnitude and Type of Load: A heavier load (P) will proportionally increase shear forces and bending moments. The distribution also matters; a concentrated load has a different effect than a uniformly distributed load (UDL). While this calculator focuses on concentrated loads, UDLs are common and require different formulas.
  2. Beam Length (L): Longer beams generally experience larger bending moments for the same load, as the moment is often proportional to the load distance and reaction forces which depend on span. This increases the risk of deflection and failure. See our Beam Span Calculator for more insights.
  3. Load Position (a): The closer the load is to a support, the higher the reaction force at that support and potentially the lower the maximum bending moment within the span, though this depends on the specific setup. Eccentric loading (load not centered) is a key consideration.
  4. Support Conditions: The type of support (pin, roller, fixed) dramatically affects reactions, shear, and moment distribution. Fixed supports, for instance, can reduce maximum bending moments but introduce complex reactions and potential for buckling. Understanding Support Reactions is crucial.
  5. Beam's Cross-Sectional Properties (e.g., Moment of Inertia, Section Modulus): While not directly calculated here, these properties (I and S, respectively) are critical for determining the beam's resistance to bending and shear. A beam with a larger moment of inertia (e.g., an I-beam compared to a solid square beam of the same area) can handle greater bending moments for the same deflection.
  6. Material Properties (e.g., Yield Strength, Modulus of Elasticity): The strength of the beam material dictates the maximum stress it can withstand before permanent deformation (yield strength) or fracture. The Modulus of Elasticity (E) determines how much the beam will deflect under load.
  7. Self-Weight of the Beam: For very long or heavily loaded beams, the beam's own weight can be a significant portion of the total load. This adds a uniformly distributed load that must be accounted for in detailed analysis.
  8. Shear Deflection vs. Bending Deflection: While bending stress is often dominant, shear stress can be critical in short, deep beams. This calculator focuses on force and moment, but deflection calculations are also vital for serviceability.

Frequently Asked Questions (FAQ)

Q1: What is the difference between shear force and bending moment?
Shear force is the internal force acting perpendicular to the beam's axis, resulting from unbalanced vertical forces. Bending moment is the internal moment acting about the beam's axis, resulting from unbalanced moments caused by loads and reactions, leading to bending (curvature) of the beam.
Q2: Why is the maximum bending moment often the most critical factor?
Bending moment directly relates to the tensile and compressive stresses developed within the beam's cross-section. Exceeding the material's allowable bending stress can lead to yielding or fracture, causing catastrophic failure.
Q3: Can this calculator handle multiple loads?
No, this calculator is designed for a single concentrated load. For beams with multiple loads, superposition (calculating the effect of each load individually and summing them up) or more advanced analysis software is required.
Q4: What if my load is distributed, not concentrated?
For uniformly distributed loads (UDLs), the formulas change. You might need to use an average load value or a dedicated UDL calculator. For irregular distributions, breaking them into simpler shapes or using numerical methods is common.
Q5: How do pin and roller supports differ in effect?
A pin support provides reaction forces in both vertical and horizontal directions, effectively preventing translation and rotation at that point. A roller support primarily provides a vertical reaction force, allowing horizontal translation. This difference impacts the calculation of reactions and internal forces.
Q6: Is the self-weight of the beam important?
For relatively short spans or light loads, the beam's self-weight is often negligible. However, for long spans (like bridges) or heavy-duty beams, it can constitute a significant portion of the total load and must be included in a comprehensive analysis.
Q7: What is the role of 'a' (load position) in the formulas?
The position 'a' determines how the load 'P' influences the reactions at the supports and the internal shear and moment values along the beam. It dictates the lever arm for moment calculations and the segment lengths for shear force calculations.
Q8: Where can I learn more about structural engineering principles?
For deeper understanding, consult introductory textbooks on statics and mechanics of materials, online engineering resources, or consider relevant engineering courses.

Explore these related tools and resources for a comprehensive understanding of structural analysis and load calculations:

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'Pin Support' : 'Roller Support'); document.getElementById("supportRightAssumption").innerText = "Right Support: " + (supportTypeRight === 'pin' ? 'Pin Support' : 'Roller Support'); // Explain the formula var formulaExplanation = "The reactions are calculated using static equilibrium (sum of forces = 0, sum of moments = 0). Shear force is the sum of vertical forces to one side of a section. Bending moment is the sum of moments to one side. For this setup (single load P at 'a' from left): R_A = P*b/L, R_B = P*a/L. Max Shear ≈ max(|R_A|, |R_B|, |R_A-P|). Max Moment ≈ R_A * a."; document.getElementById("formulaExplanation").innerText = formulaExplanation; // Update results display document.getElementById("resultsContent").querySelector(".main-result").innerText = maxMoment.toFixed(2) + " Nm"; // Generate Table Data populateAnalysisTable(beamLength, loadPosition, reactionLeft, loadValue); // Draw Chart drawDiagramChart(beamLength, loadPosition, reactionLeft, reactionRight, loadValue, maxShear, maxMoment); document.getElementById("chartContainer").style.display = "block"; document.getElementById("resultsTableContainer").style.display = "block"; } function populateAnalysisTable(beamLength, loadPosition, reactionLeft, loadValue) { var tableBody = document.getElementById("analysisTable").getElementsByTagName("tbody")[0]; tableBody.innerHTML = "; // Clear previous rows var points = [0, loadPosition, beamLength]; // Key points var uniquePoints = Array.from(new Set(points)).sort((a, b) => a – b); var shearLeftOfLoad = reactionLeft; var shearRightOfLoad = reactionLeft – loadValue; var reactionRight = (loadValue * (beamLength – loadPosition)) / beamLength; // Recalculate for clarity for (var i = 0; i < uniquePoints.length; i++) { var x = uniquePoints[i]; var shearForce, bendingMoment; if (x loadPosition shearForce = reactionLeft – loadValue; // Value just after the load P bendingMoment = reactionLeft * x – loadValue * (x – loadPosition); } // Special handling for ends if (x === 0) { shearForce = reactionLeft; bendingMoment = 0; } if (x === beamLength) { shearForce = reactionLeft – loadValue; // This is the value approaching the right support if P is not at L. // Correct shear at the support is often considered as reactionRight but opposite sign if considering 'left of support'. // For simplicity, we'll show the value just before R_B counteracts. if (loadPosition === beamLength) shearForce = reactionLeft; // If load is at the very end else shearForce = reactionLeft – loadValue; // Generic value just left of end support bendingMoment = 0; // Moment at a simple support is zero } var row = tableBody.insertRow(); var cell1 = row.insertCell(0); var cell2 = row.insertCell(1); var cell3 = row.insertCell(2); cell1.innerText = x.toFixed(2); cell2.innerText = shearForce.toFixed(2); cell3.innerText = bendingMoment.toFixed(2); } document.getElementById("tableMessage").style.display = "none"; } function drawDiagramChart(beamLength, loadPosition, reactionLeft, reactionRight, loadValue, maxShear, maxMoment) { var canvas = document.getElementById('beamDiagramCanvas'); var ctx = canvas.getContext('2d'); ctx.clearRect(0, 0, canvas.width, canvas.height); // Clear previous drawing var scaleX = (canvas.width – 40) / beamLength; // Scale factor for X-axis var scaleY = (canvas.height / 2 – 20) / Math.max(maxShear * 1.2, Math.abs(maxMoment) * 1.2, 100); // Scale factor for Y-axis, ensure space for labels and moment var originY = canvas.height / 2; // Center line for moments // Draw X-axis (Beam representation) ctx.beginPath(); ctx.moveTo(20, originY); ctx.lineTo(canvas.width – 20, originY); ctx.strokeStyle = '#333′; ctx.lineWidth = 2; ctx.stroke(); ctx.font = '12px Arial'; ctx.fillStyle = '#333'; ctx.fillText('0m', 20, originY + 15); ctx.fillText(beamLength.toFixed(2) + 'm', canvas.width – 40, originY + 15); // — Shear Force Diagram — ctx.beginPath(); ctx.strokeStyle = '#1f77b4'; // Blue for shear ctx.lineWidth = 2; var currentShear = 0; // Start at left support ctx.moveTo(20, originY); // Line to load position if (loadPosition > 0) { currentShear = reactionLeft; // Draw vertical line up/down at start ctx.lineTo(20, originY – currentShear * scaleY); // Draw horizontal line to load position ctx.lineTo(20 + loadPosition * scaleX, originY – currentShear * scaleY); } else { currentShear = reactionLeft; // If load is at 0, shear is already reactionLeft } // Drop at load position var shearAfterLoad = reactionLeft – loadValue; ctx.lineTo(20 + loadPosition * scaleX, originY – shearAfterLoad * scaleY); currentShear = shearAfterLoad; // Line to end of beam ctx.lineTo(canvas.width – 20, originY – currentShear * scaleY); ctx.stroke(); // Indicate zero shear line ctx.setLineDash([5, 5]); ctx.moveTo(20, originY); ctx.lineTo(canvas.width – 20, originY); ctx.strokeStyle = '#ccc'; ctx.stroke(); ctx.setLineDash([]); // — Bending Moment Diagram — ctx.beginPath(); ctx.strokeStyle = '#ff7f0e'; // Orange for moment ctx.lineWidth = 2; var currentMoment = 0; // Start at left support (moment is 0) ctx.moveTo(20, originY); // Moment to load position var momentAtLoad = reactionLeft * loadPosition; // Draw the moment curve – it's a straight line for constant shear ctx.lineTo(20 + loadPosition * scaleX, originY – momentAtLoad * scaleY); currentMoment = momentAtLoad; // Moment from load position to end var momentAtEnd = reactionLeft * beamLength – loadValue * (beamLength – loadPosition); // Should be 0 at simple support // Draw the next segment of moment curve ctx.lineTo(canvas.width – 20, originY – momentAtEnd * scaleY); // Expected to be 0 if calc is correct ctx.stroke(); ctx.font = '12px Arial'; ctx.fillStyle = '#1f77b4'; ctx.fillText('Shear Force (N)', 5, 20); ctx.fillStyle = '#ff7f0e'; ctx.fillText('Bending Moment (Nm)', 5, 40); document.getElementById("chartMessage").style.display = "none"; } function displayError(elementId, message) { var errorElement = document.getElementById(elementId + "Error"); errorElement.innerText = message; errorElement.classList.add("visible"); } function clearErrorMessages() { var errorElements = document.querySelectorAll(".error-message"); for (var i = 0; i < errorElements.length; i++) { errorElements[i].innerText = ""; errorElements[i].classList.remove("visible"); } } function resetForm() { document.getElementById("beamForm").reset(); // Set sensible defaults for calculation document.getElementById("beamLength").value = 5; document.getElementById("loadValue").value = 10000; document.getElementById("loadPosition").value = 2.5; document.getElementById("supportType").value = "pin"; document.getElementById("supportTypeRight").value = "roller"; clearErrorMessages(); document.getElementById("noResults").style.display = "none"; document.getElementById("resultsContent").style.display = "none"; document.getElementById("chartContainer").style.display = "none"; document.getElementById("resultsTableContainer").style.display = "none"; // Trigger a calculation with defaults calculateBeamLoad(); } function copyResults() { var mainResult = document.getElementById("maxMoment").innerText; var reactionLeft = document.getElementById("reactionLeft").innerText; var reactionRight = document.getElementById("reactionRight").innerText; var maxShear = document.getElementById("maxShear").innerText; var supportLeft = document.getElementById("supportAssumption").innerText; var supportRight = document.getElementById("supportRightAssumption").innerText; var formula = document.getElementById("formulaExplanation").innerText; var textToCopy = "Beam Load Analysis Results:\n\n"; textToCopy += "Max Bending Moment: " + mainResult + "\n"; textToCopy += "Max Shear Force: " + maxShear + "\n"; textToCopy += "Reaction Force (Left): " + reactionLeft + "\n"; textToCopy += "Reaction Force (Right): " + reactionRight + "\n\n"; textToCopy += "Assumptions:\n"; textToCopy += "- " + supportLeft + "\n"; textToCopy += "- " + supportRight + "\n"; textToCopy += "- " + document.querySelectorAll(".assumptions div")[2].innerText + "\n"; // Single load assumption textToCopy += "- " + document.querySelectorAll(".assumptions div")[3].innerText + "\n"; // Beam uniform assumption textToCopy += "\nFormula Used: " + formula; // Use a temporary textarea to copy text var textArea = document.createElement("textarea"); textArea.value = textToCopy; textArea.style.position = "fixed"; textArea.style.left = "-9999px"; document.body.appendChild(textArea); textArea.focus(); textArea.select(); try { var successful = document.execCommand('copy'); var msg = successful ? 'Results copied!' : 'Copy failed!'; // console.log(msg); // Optional: show feedback to user } catch (err) { // console.log('Oops, unable to copy'); } document.body.removeChild(textArea); alert("Results copied to clipboard!"); } // Initial calculation on page load with default values document.addEventListener('DOMContentLoaded', function() { resetForm(); // This sets defaults and calculates });

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