Aviation Fuel Weight Calculator

Aviation Fuel Weight Calculator: Calculate Your Aircraft's Fuel Load :root { –primary-color: #004a99; –success-color: #28a745; –background-color: #f8f9fa; –text-color: #333; –border-color: #ccc; –shadow-color: rgba(0, 0, 0, 0.1); –accent-color: #e9ecef; } body { font-family: 'Segoe UI', Tahoma, Geneva, Verdana, sans-serif; line-height: 1.6; color: var(–text-color); background-color: var(–background-color); margin: 0; padding: 0; } .container { max-width: 960px; margin: 20px auto; padding: 20px; background-color: #fff; border-radius: 8px; box-shadow: 0 4px 12px var(–shadow-color); } h1, h2, h3 { color: var(–primary-color); text-align: center; margin-bottom: 20px; } h1 { font-size: 2.5em; } h2 { font-size: 1.8em; margin-top: 30px; border-bottom: 2px solid var(–primary-color); padding-bottom: 5px; } h3 { font-size: 1.3em; margin-top: 20px; } .calculator-wrapper { background-color: var(–accent-color); padding: 25px; border-radius: 8px; margin-bottom: 30px; box-shadow: inset 0 2px 4px var(–shadow-color); } .input-group { margin-bottom: 20px; display: flex; flex-direction: column; align-items: stretch; } .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: 10px 12px; border: 1px solid var(–border-color); border-radius: 4px; font-size: 1em; box-sizing: border-box; /* Important for consistent sizing */ transition: border-color 0.2s ease-in-out, box-shadow 0.2s ease-in-out; } .input-group input[type="number"]:focus, .input-group select:focus { outline: none; border-color: var(–primary-color); box-shadow: 0 0 0 3px rgba(0, 74, 153, 0.2); } .input-group .helper-text { font-size: 0.85em; color: #6c757d; margin-top: 5px; } .error-message { color: #dc3545; font-size: 0.9em; margin-top: 5px; display: none; /* Hidden by default */ } .buttons-container { display: flex; justify-content: space-between; gap: 10px; margin-top: 25px; } button { padding: 12px 20px; border: none; border-radius: 4px; cursor: pointer; font-size: 1em; font-weight: bold; transition: background-color 0.2s ease, transform 0.1s ease; flex-grow: 1; } button:hover { opacity: 0.9; transform: translateY(-1px); } button:active { transform: translateY(0); } .btn-primary { background-color: var(–primary-color); color: white; } .btn-secondary { background-color: var(–border-color); color: var(–text-color); } .btn-copy { background-color: #6c757d; color: white; } #results { margin-top: 30px; background-color: var(–primary-color); color: white; padding: 20px; border-radius: 8px; text-align: center; box-shadow: 0 2px 8px var(–shadow-color); } #results h3 { color: white; margin-bottom: 15px; font-size: 1.5em; } .result-item { margin-bottom: 10px; font-size: 1.1em; } .result-label { font-weight: bold; opacity: 0.9; } .highlight-result { font-size: 2em; font-weight: bold; margin-top: 15px; padding: 10px; background-color: var(–success-color); border-radius: 5px; display: inline-block; min-width: 50%; } .formula-explanation { margin-top: 15px; font-size: 0.95em; color: #555; text-align: left; border-left: 3px solid var(–primary-color); padding-left: 10px; } table { width: 100%; border-collapse: collapse; margin-top: 20px; margin-bottom: 30px; box-shadow: 0 2px 8px 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: var(–accent-color); } caption { font-size: 1.1em; font-weight: bold; color: var(–primary-color); margin-bottom: 10px; text-align: left; } .chart-container { width: 100%; max-width: 700px; /* Limit chart width */ margin: 20px auto; background-color: #fff; padding: 20px; border-radius: 8px; box-shadow: 0 4px 12px var(–shadow-color); } canvas { display: block; width: 100% !important; height: auto !important; } .article-content { margin-top: 40px; background-color: #fff; padding: 30px; border-radius: 8px; box-shadow: 0 4px 12px var(–shadow-color); } .article-content p, .article-content ul, .article-content ol { margin-bottom: 20px; } .article-content li { margin-bottom: 10px; } .article-content a { color: var(–primary-color); text-decoration: none; font-weight: bold; } .article-content a:hover { text-decoration: underline; } .faq-item { margin-bottom: 15px; padding: 10px; border-left: 3px solid var(–primary-color); background-color: var(–accent-color); border-radius: 4px; } .faq-item strong { color: var(–primary-color); } .related-tools ul { list-style: none; padding: 0; } .related-tools li { margin-bottom: 15px; } /* Responsive adjustments */ @media (max-width: 768px) { .container { margin: 10px; padding: 15px; } h1 { font-size: 1.8em; } h2 { font-size: 1.4em; } button { font-size: 0.9em; padding: 10px 15px; } .buttons-container { flex-direction: column; } #results .highlight-result { font-size: 1.6em; } } /* Specific styling for chart legend */ .chart-legend { text-align: center; margin-top: 10px; font-size: 0.9em; color: #6c757d; } .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; } .chart-legend .fuel-weight::before { background-color: #007bff; /* Blue for fuel weight */ } .chart-legend .standard-density::before { background-color: #ffc107; /* Yellow for standard density */ }

Aviation Fuel Weight Calculator

Calculate Aviation Fuel Weight

Enter the details below to determine the precise weight of your aircraft's fuel load.

Enter the total volume of fuel in gallons (US).
Jet A Jet A-1 Avgas 100LL Custom Density Select your aircraft's fuel type.
Enter density in pounds per US gallon (lbs/gal).
Pounds per US Gallon (lbs/gal) Kilograms per Liter (kg/L) Pounds per Liter (lbs/L) Kilograms per US Gallon (kg/gal) Select the unit for your density value.

Results Summary

Fuel Density:
Fuel Weight (Total):
Fuel Weight (Calculated):
Fuel Volume in Liters:

The aviation fuel weight is calculated by multiplying the fuel volume by its density. We convert units to ensure accuracy based on your selection.

Calculated Fuel Weight Typical Fuel Density Range
Fuel Weight vs. Typical Density Range

What is Aviation Fuel Weight Calculation?

The aviation fuel weight calculation is a critical process in aviation that determines the total mass of fuel onboard an aircraft. This is not merely an academic exercise; it's fundamental to flight safety, performance, and efficiency. Understanding the exact weight of fuel allows pilots and flight planners to accurately calculate an aircraft's total weight, which directly impacts its performance characteristics such as takeoff distance, climb rate, cruise speed, and landing speed. An incorrect estimation of fuel weight can lead to miscalculations in the aircraft's center of gravity, potentially compromising its stability and controllability. Therefore, the aviation fuel weight calculation is a cornerstone of responsible flight operations.

Who should use it:

  • Pilots: Essential for pre-flight planning to ensure the aircraft is within its weight and balance limits.
  • Flight Dispatchers and Planners: Responsible for calculating fuel requirements and ensuring safe load distribution for commercial and cargo flights.
  • Aircraft Maintenance Technicians: May need to verify fuel quantities and weights during maintenance or for weight and balance record updates.
  • Aviation Students and Instructors: For learning and teaching fundamental aviation principles.
  • Aerospace Engineers: In the design and performance analysis phases of aircraft development.

Common misconceptions:

  • Fuel weight is constant: Fuel density varies with temperature and composition, meaning its weight per unit volume is not fixed.
  • All fuel is the same weight: Different types of aviation fuel (e.g., Jet A vs. Avgas) have distinct densities.
  • Calculating fuel weight is simple addition: It requires precise conversion factors and an understanding of different units (gallons, liters, pounds, kilograms).
  • Overestimating fuel is always safe: Carrying excessive fuel adds unnecessary weight, negatively impacting performance and fuel efficiency, and can even exceed weight limits.

Aviation Fuel Weight Formula and Mathematical Explanation

The core of the aviation fuel weight calculation relies on a fundamental physics principle: mass equals volume multiplied by density. However, in aviation, we often deal with volume in gallons or liters and weight in pounds or kilograms, necessitating careful unit conversions.

The primary formula is:

Fuel Weight = Fuel Volume × Fuel Density

To make this practical, we need to account for different units. Our calculator handles conversions transparently. The process involves:

  1. Ensuring the Fuel Volume is in a standard unit (e.g., US Gallons).
  2. Determining the correct Fuel Density based on the fuel type and units selected.
  3. Applying the formula and converting the result to the desired output unit (e.g., Pounds or Kilograms).

Variable Explanations:

Variable Meaning Unit Typical Range
Fuel Volume The total amount of fuel measured in liquid volume. US Gallons (gal) / Liters (L) 10 – 50,000+ (aircraft dependent)
Fuel Density The mass of the fuel per unit volume. This varies with temperature and fuel type. Pounds per US Gallon (lbs/gal) / Kilograms per Liter (kg/L) 5.8 – 7.1 (lbs/gal) for common fuels
Fuel Weight The total mass of the fuel. Pounds (lbs) / Kilograms (kg) Varies greatly based on volume and density.

Detailed Formula Breakdown with Unit Conversion:

Let's assume we input Volume in US Gallons (V_gal) and Density in Pounds per US Gallon (D_lbs_gal). The initial Fuel Weight (W_lbs) is:

W_lbs = V_gal × D_lbs_gal

If the user inputs volume in Liters (V_L) and density in Kilograms per Liter (D_kg_L), the weight would be:

W_kg = V_L × D_kg_L

Our calculator uses internal conversion factors:

  • 1 US Gallon ≈ 3.78541 Liters
  • 1 Kilogram ≈ 2.20462 Pounds

The calculator first converts the input volume to liters if necessary, then uses the selected density (potentially converting it to the desired output unit, e.g., lbs/gal), and finally calculates the weight. For instance, if Volume is in gallons and Density is in kg/L, we'd convert gallons to liters and then use the kg/L density to get weight in kg, which can then be converted to lbs.

Practical Examples (Real-World Use Cases)

Example 1: Cessna 172 Fuel Load

A pilot is planning a flight in a Cessna 172, which has a fuel capacity of 56 US gallons (total). They intend to fill the tanks completely for a longer flight. The typical fuel is Jet A with a standard density of approximately 6.7 lbs/gal.

  • Inputs:
    • Fuel Volume: 56 gal
    • Fuel Type: Jet A (using default density for Jet A)
    • Density Unit: Pounds per US Gallon (lbs/gal)
  • Calculation:
    • Fuel Density (Jet A): ~6.7 lbs/gal
    • Fuel Weight = 56 gal × 6.7 lbs/gal = 375.2 lbs
  • Outputs:
    • Fuel Density: 6.7 lbs/gal
    • Fuel Weight (Total): 375.2 lbs
  • Interpretation: The total fuel load weighs approximately 375.2 pounds. This figure is crucial for calculating the aircraft's total weight and balance, ensuring it remains within safe operating limits for the planned flight.

Example 2: Boeing 737 Fuel Planning (Simplified)

A flight dispatcher is calculating the fuel needed for a Boeing 737. The aircraft requires 15,000 liters of Jet A-1 fuel for the trip. Jet A-1 has a density that averages around 0.81 kg/L at typical operating temperatures.

  • Inputs:
    • Fuel Volume: 15,000 L
    • Fuel Type: Jet A-1 (using default density for Jet A-1)
    • Density Unit: Kilograms per Liter (kg/L)
  • Calculation:
    • Fuel Density (Jet A-1): ~0.81 kg/L
    • Fuel Weight = 15,000 L × 0.81 kg/L = 12,150 kg
  • Outputs:
    • Fuel Density: 0.81 kg/L
    • Fuel Weight (Total): 12,150 kg (or approximately 26,785 lbs after conversion)
  • Interpretation: The required 15,000 liters of fuel represent a significant portion of the aircraft's payload, weighing over 12 metric tons. This weight directly affects the aircraft's performance and range.

How to Use This Aviation Fuel Weight Calculator

Using the Aviation Fuel Weight Calculator is straightforward and designed for quick, accurate results. Follow these steps:

  1. Enter Fuel Volume: Input the total amount of fuel you have or need. Specify the unit (gallons or liters) using the helper text as a guide.
  2. Select Fuel Type: Choose your fuel type from the dropdown. Common types like Jet A, Jet A-1, and Avgas 100LL have pre-set typical densities. If your fuel type isn't listed or you have a specific density value, select "Custom Density".
  3. Enter Custom Density (If Applicable): If you selected "Custom Density", input the precise density value for your fuel.
  4. Select Density Unit: Choose the units in which your fuel density is measured (e.g., lbs/gal, kg/L). This is crucial for accurate calculation.
  5. Click 'Calculate': Press the "Calculate" button. The calculator will process your inputs.

How to Read Results:

  • Fuel Density: Displays the density of the fuel used in the calculation, based on your selection or input.
  • Fuel Weight (Total): This is the primary, highlighted result – the total weight of your fuel load in pounds.
  • Fuel Weight (Calculated): Shows the calculated weight in both pounds and kilograms for your reference.
  • Fuel Volume in Liters: Displays the converted volume of fuel in liters.
  • Formula Explanation: A brief description of the calculation method is provided below the results.

Decision-Making Guidance:

  • Compare the calculated Fuel Weight (Total) against your aircraft's weight and balance limitations.
  • Ensure the fuel quantity aligns with your flight plan's endurance requirements, considering performance impacts.
  • Use the results to optimize fuel loading, balancing the need for range with the negative effects of excess weight on performance and fuel efficiency.

Key Factors That Affect Aviation Fuel Weight Results

Several factors can influence the accuracy and application of aviation fuel weight calculations. Understanding these is vital for precise flight planning:

  1. Fuel Density Variation: This is the most significant variable. Fuel density changes with temperature. Colder fuel is denser (heavier per unit volume), while warmer fuel is less dense. Standard densities are averages; actual density on a given day can differ.
  2. Fuel Type: Different fuels have inherently different densities. Jet fuels (like Jet A and Jet A-1) are generally denser than Avgas (like 100LL). Using the correct density for the fuel type loaded is essential.
  3. Units of Measurement: Aviation operates globally, leading to various units. Gallons (US vs. Imperial), Liters, Pounds, and Kilograms are common. Mismatched units during calculation will lead to significant errors. Our calculator helps manage this, but awareness is key.
  4. Temperature Effects: As mentioned, temperature impacts density. While often accounted for in standard density figures, extreme temperatures can necessitate precise adjustments, particularly for long-range flights or when operating in very hot or cold climates.
  5. Fuel Contamination/Additives: While typically minimal, the presence of water or certain additives can slightly alter the fuel's overall density and weight. Flight crews are trained to check for water, which is denser than fuel and sinks.
  6. Aircraft Fuel System Design: The usable versus total fuel capacity and the placement of fuel tanks affect the aircraft's center of gravity. Calculating the weight of the fuel loaded is just one part; understanding its distribution is equally important for weight and balance.
  7. Calculation Precision: Using rounded density figures or incorrect conversion factors can introduce small errors that accumulate, especially on large aircraft or during complex flight planning. Using a reliable calculator mitigates this.

Frequently Asked Questions (FAQ)

Q1: What is the standard density for Jet A fuel?

A1: The standard density for Jet A fuel is typically around 6.7 lbs/US gallon (or about 0.80 kg/L) at 15°C (59°F). However, this can vary slightly with temperature.

Q2: How does temperature affect fuel weight?

A2: Fuel expands when warm and contracts when cold. Therefore, warm fuel is less dense (lighter per gallon/liter), and cold fuel is denser (heavier per gallon/liter). This variation needs to be considered for maximum accuracy, especially in extreme climates.

Q3: Can I use US gallons and Imperial gallons interchangeably?

A3: No. A US gallon is smaller than an Imperial gallon (1 US gal ≈ 0.833 Imperial gal). Always ensure you know which standard your volume measurement refers to, as using the wrong one will cause significant errors.

Q4: Is Avgas 100LL heavier or lighter than Jet A?

A4: Avgas 100LL is typically slightly heavier per volume than Jet A. Standard density for Avgas 100LL is around 6.0 lbs/US gallon, whereas Jet A is around 6.7 lbs/US gallon. (Note: There can be variations, but this is a common rule of thumb).

Q5: Why is fuel weight so important for aircraft performance?

A5: Aircraft performance (takeoff distance, climb rate, range, cruise speed) is directly related to the aircraft's total weight. More fuel means more weight, which degrades performance. Accurate fuel weight calculation ensures the aircraft operates within its certified performance envelope.

Q6: How does the calculator handle different density units?

A6: The calculator allows you to select the unit of your input density (e.g., lbs/gal, kg/L). It then uses the appropriate conversion factors to calculate the fuel weight in both pounds and kilograms, ensuring accuracy regardless of your input unit.

Q7: What is the difference between "Fuel Weight (Total)" and "Fuel Weight (Calculated)"?

A7: "Fuel Weight (Total)" is the primary, highlighted result, typically shown in pounds, representing the total weight of the fuel. "Fuel Weight (Calculated)" provides the weight in both pounds and kilograms for comprehensive understanding and potential use in different contexts.

Q8: Does this calculator account for fuel purchased at different temperatures?

A8: This calculator uses standard or user-defined densities. While it allows for custom density input, it does not automatically adjust for real-time ambient temperature variations at the point of fuel purchase. For extreme accuracy, especially in critical flight phases, pilots may consult specific fuel density charts based on local temperature data.

© 2023 Your Aviation Insights. All rights reserved.
var fuelTypeDensities = { "Jet A": { lbs_per_gal: 6.7, kg_per_liter: 0.80, lbs_per_liter: 0.61, kg_per_gal: 14.77 }, "Jet A-1": { lbs_per_gal: 6.7, kg_per_liter: 0.81, lbs_per_liter: 0.61, kg_per_gal: 14.77 }, "Avgas 100LL": { lbs_per_gal: 6.0, kg_per_liter: 0.72, lbs_per_liter: 0.54, kg_per_gal: 13.23 } }; var conversionFactors = { gal_to_liter: 3.78541, liter_to_gal: 0.264172, kg_to_lbs: 2.20462, lbs_to_kg: 0.453592 }; function getInputValue(id) { var inputElement = document.getElementById(id); if (inputElement) { return parseFloat(inputElement.value); } return NaN; } function setTexContent(id, value) { var element = document.getElementById(id); if (element) { element.textContent = value; } } function setDisplayDensity(densityValue, unit) { var displayUnit = unit.replace('_', '/'); setTexContent('displayDensity', densityValue.toFixed(2) + ' ' + displayUnit); } function getDensityForFuelType(fuelType, unit) { if (fuelTypeDensities[fuelType] && fuelTypeDensities[fuelType][unit]) { return fuelTypeDensities[fuelType][unit]; } return NaN; // Should not happen for predefined types } function convertDensity(fromValue, fromUnit, toUnit) { var from_lbs_gal = 0, from_kg_liter = 0, from_lbs_liter = 0, from_kg_gal = 0; var to_lbs_gal = 0, to_kg_liter = 0, to_lbs_liter = 0, to_kg_gal = 0; if (fromUnit === 'lbs_per_gal') from_lbs_gal = fromValue; else if (fromUnit === 'kg_per_liter') from_kg_liter = fromValue; else if (fromUnit === 'lbs_per_liter') from_lbs_liter = fromValue; else if (fromUnit === 'kg_per_gal') from_kg_gal = fromValue; if (toUnit === 'lbs_per_gal') to_lbs_gal = 1; else if (toUnit === 'kg_per_liter') to_kg_liter = 1; else if (toUnit === 'lbs_per_liter') to_lbs_liter = 1; else if (toUnit === 'kg_per_gal') to_kg_gal = 1; // Base conversion to lbs/gal for intermediate calculation if needed var base_lbs_gal = from_lbs_gal || (from_kg_liter * conversionFactors.kg_to_lbs / conversionFactors.gal_to_liter) || (from_lbs_liter * conversionFactors.gal_to_liter) || (from_kg_gal * conversionFactors.kg_to_lbs); if (to_lbs_gal) return base_lbs_gal; if (to_kg_liter) return base_lbs_gal * conversionFactors.lbs_to_kg * conversionFactors.gal_to_liter; if (to_lbs_liter) return base_lbs_gal * conversionFactors.lbs_to_kg; if (to_kg_gal) return base_lbs_gal / conversionFactors.kg_to_lbs; return NaN; // Should not happen } function calculateFuelWeight() { var fuelVolume = getInputValue('fuelVolume'); var fuelType = document.getElementById('fuelType').value; var customDensity = getInputValue('customDensity'); var densityUnit = document.getElementById('densityUnit').value; var volumeError = document.getElementById('fuelVolumeError'); var densityUnitError = document.getElementById('densityUnitError'); var customDensityError = document.getElementById('customDensityError'); // Reset errors volumeError.style.display = 'none'; densityUnitError.style.display = 'none'; customDensityError.style.display = 'none'; var isValid = true; if (isNaN(fuelVolume) || fuelVolume <= 0) { volumeError.textContent = 'Please enter a valid positive fuel volume.'; volumeError.style.display = 'block'; isValid = false; } var effectiveDensity = NaN; var displayDensityValue = NaN; var displayDensityUnit = densityUnit.replace('_', '/'); if (fuelType === "Custom") { if (isNaN(customDensity) || customDensity <= 0) { customDensityError.textContent = 'Please enter a valid positive custom density.'; customDensityError.style.display = 'block'; isValid = false; } else { effectiveDensity = customDensity; displayDensityValue = effectiveDensity; } } else { effectiveDensity = getDensityForFuelType(fuelType, densityUnit); if (isNaN(effectiveDensity)) { // Try converting standard density if direct match not found var standardDensityObj = fuelTypeDensities[fuelType]; if (standardDensityObj) { var referenceUnit = 'lbs_per_gal'; // Assume a reference unit var standardValue = standardDensityObj[referenceUnit]; effectiveDensity = convertDensity(standardValue, referenceUnit, densityUnit); displayDensityValue = effectiveDensity; } else { densityUnitError.textContent = 'Density data not available for this fuel type and unit.'; densityUnitError.style.display = 'block'; isValid = false; } } else { displayDensityValue = effectiveDensity; } } if (!isValid) { setTexContent('displayDensity', '–'); setTexContent('calculatedWeight', '–'); setTexContent('highlight-result', '–'); setTexContent('volumeInLiters', '–'); updateChart([], []); // Clear chart return; } // Ensure calculations use consistent internal units if needed, or directly use converted values var weightInPounds = NaN; var weightInKilograms = NaN; var volumeInLiters = fuelVolume * conversionFactors.gal_to_liter; // Assuming default input is gallons // Recalculate based on selected density unit var fuelVolumeInputUnit = document.getElementById('fuelVolume'); var volumeIsGallons = true; // Assume gallons by default based on input helper text // If we need to be more robust about input volume units, add a selector. // For now, assume 'fuelVolume' is always US Gallons as per helper text. // Convert input volume to liters if density is in kg/L or lbs/L var inputVolumeLiters = fuelVolume * conversionFactors.gal_to_liter; var inputVolumeGallons = fuelVolume; var calculatedWeightValue = NaN; var calculatedWeightUnit = 'lbs'; // Default output unit if (densityUnit === 'lbs_per_gal') { calculatedWeightValue = inputVolumeGallons * effectiveDensity; calculatedWeightUnit = 'lbs'; } else if (densityUnit === 'kg_per_liter') { calculatedWeightValue = inputVolumeLiters * effectiveDensity; calculatedWeightUnit = 'kg'; } else if (densityUnit === 'lbs_per_liter') { calculatedWeightValue = inputVolumeLiters * effectiveDensity; calculatedWeightUnit = 'lbs'; } else if (densityUnit === 'kg_per_gal') { calculatedWeightValue = inputVolumeGallons * effectiveDensity; calculatedWeightUnit = 'kg'; } weightInPounds = (calculatedWeightUnit === 'lbs') ? calculatedWeightValue : calculatedWeightValue * conversionFactors.kg_to_lbs; weightInKilograms = (calculatedWeightUnit === 'kg') ? calculatedWeightValue : calculatedWeightValue * conversionFactors.lbs_to_kg; // Update results display setDisplayDensity(displayDensityValue, displayDensityUnit); setTexContent('highlight-result', weightInPounds.toFixed(1) + ' lbs'); setTexContent('calculatedWeight', weightInKilograms.toFixed(1) + ' kg'); setTexContent('volumeInLiters', volumeInLiters.toFixed(1) + ' L'); updateChart(weightInPounds, displayDensityValue); } function resetCalculator() { document.getElementById('fuelVolume').value = 500; document.getElementById('fuelType').value = "Jet A"; document.getElementById('customDensityGroup').style.display = 'none'; document.getElementById('customDensity').value = 6.7; document.getElementById('densityUnit').value = "lbs_per_gal"; // Clear error messages var errorElements = document.querySelectorAll('.error-message'); for (var i = 0; i 0) { effectiveDensity = customDensityValue; displayDensityValue = effectiveDensity; } } else { customDensityGroup.style.display = 'none'; effectiveDensity = getDensityForFuelType(fuelType, densityUnit); if (isNaN(effectiveDensity)) { // Try converting standard density if direct match not found var standardDensityObj = fuelTypeDensities[fuelType]; if (standardDensityObj) { var referenceUnit = 'lbs_per_gal'; // Assume a reference unit var standardValue = standardDensityObj[referenceUnit]; effectiveDensity = convertDensity(standardValue, referenceUnit, densityUnit); displayDensityValue = effectiveDensity; } } else { displayDensityValue = effectiveDensity; } } if (!isNaN(displayDensityValue)) { setDisplayDensity(displayDensityValue, displayDensityUnit); } else { setTexContent('displayDensity', '–'); } } // Charting Logic var myChart = null; // Global variable to hold the chart instance function updateChart(weightInPounds, typicalDensity) { var canvas = document.getElementById('fuelWeightChart'); if (!canvas) return; var ctx = canvas.getContext('2d'); // Clear previous chart instance if it exists if (myChart) { myChart.destroy(); } // Define typical density ranges for common fuels var typicalDensities = { "Jet A": { min: 6.5, max: 6.9 }, // lbs/gal "Jet A-1": { min: 6.5, max: 6.9 }, // lbs/gal "Avgas 100LL": { min: 5.9, max: 6.1 } // lbs/gal }; var selectedFuelType = document.getElementById('fuelType').value; var densityRange = typicalDensities[selectedFuelType] || { min: 6.0, max: 7.0 }; // Default range if fuel type not found var fuelVolume = getInputValue('fuelVolume'); if (isNaN(fuelVolume) || fuelVolume <= 0) { fuelVolume = 500; // Use default if invalid } // Calculate weight at min/max density for the chosen fuel type var minWeight = fuelVolume * densityRange.min; var maxWeight = fuelVolume * densityRange.max; // Prepare data for the chart var chartData = { labels: ['Fuel Load'], datasets: [ { label: 'Calculated Fuel Weight (lbs)', data: [weightInPounds], backgroundColor: 'rgba(0, 123, 255, 0.6)', // Primary color variation borderColor: 'rgba(0, 123, 255, 1)', borderWidth: 1, barThickness: 40 // Make bars thicker }, { label: 'Typical Density Range (lbs)', data: [minWeight, maxWeight], // Represent range backgroundColor: 'rgba(255, 193, 7, 0.5)', // Yellowish for range borderColor: 'rgba(255, 193, 7, 0.8)', borderWidth: 1, type: 'bar', // Use bars for range representation order: 2 // Ensure it's drawn below the primary bar } ] }; // Configure chart options var options = { responsive: true, maintainAspectRatio: false, scales: { y: { beginAtZero: true, title: { display: true, text: 'Weight (lbs)' } }, x: { title: { display: true, text: 'Fuel Load Scenario' } } }, plugins: { legend: { display: false // Legend is handled by custom div }, title: { display: true, text: 'Comparison of Fuel Weight', font: { size: 16 } } }, layout: { padding: { left: 10, right: 10, top: 10, bottom: 10 } } }; // Create the chart myChart = new Chart(ctx, { type: 'bar', // Base type, can be overridden by dataset type data: chartData, options: options }); } // Initial setup and event listeners document.addEventListener('DOMContentLoaded', function() { var fuelTypeSelect = document.getElementById('fuelType'); var densityUnitSelect = document.getElementById('densityUnit'); fuelTypeSelect.addEventListener('change', function() { updateFuelTypeDensityDisplay(); // Recalculate and update chart when fuel type changes calculateFuelWeight(); }); densityUnitSelect.addEventListener('change', function() { updateFuelTypeDensityDisplay(); // Recalculate and update chart when density unit changes calculateFuelWeight(); }); document.getElementById('customDensity').addEventListener('input', function() { calculateFuelWeight(); }); document.getElementById('fuelVolume').addEventListener('input', function() { calculateFuelWeight(); }); // Initial calculation on page load resetCalculator(); updateFuelTypeDensityDisplay(); // Ensure density display is correct initially });

Leave a Comment