Calculate Average Molecular Weight Given Oxygen Fuel Ratio

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Calculate Average Molecular Weight Given Oxygen Fuel Ratio

Determine the average molecular weight of combustion products using the oxygen-to-fuel mass ratio. Essential for combustion analysis and efficiency calculations.

Combustion Analysis Calculator

Enter the mass ratio of oxygen to fuel (e.g., 15 for typical hydrocarbon fuels). Unitless.
Hydrocarbon (e.g., Methane, Propane) Hydrogen (H₂) Ammonia (NH₃) Select the primary fuel being combusted.
Percentage of oxygen remaining after complete combustion (0% for stoichiometric).

Calculation Results

Ideal MW: — | Actual MW: — | O₂ Mole Fraction: —
The average molecular weight is calculated by considering the stoichiometric combustion products and adding the contribution of excess oxygen and nitrogen from the air.
Chart: Average Molecular Weight vs. Oxygen-Fuel Ratio
Parameter Value Units
Oxygen-Fuel Ratio (O/F)
Fuel Type
Excess Oxygen %
Ideal Molecular Weight (Stoichiometric) g/mol
Oxygen Mole Fraction (Excess)
Actual Average Molecular Weight g/mol
Table: Summary of Calculation Parameters and Results

What is Average Molecular Weight Given Oxygen Fuel Ratio?

The calculation of average molecular weight given oxygen fuel ratio is a fundamental concept in combustion chemistry and engineering. It quantifies the average mass of molecules present in the combustion products, specifically considering the input ratio of oxygen to fuel and any excess oxygen available. Understanding this value is crucial for predicting combustion efficiency, exhaust gas composition, and designing effective combustion systems. This metric helps engineers and scientists analyze how efficiently a fuel is being burned and what byproducts are being formed. A higher average molecular weight in the exhaust often suggests incomplete combustion or the presence of excess oxygen, which can have implications for performance and emissions. Conversely, a lower average molecular weight might indicate a more complete and efficient combustion process.

Who should use it: This calculator and the underlying principles are vital for chemical engineers, mechanical engineers, aerospace engineers, researchers in energy and propulsion, environmental scientists, and students studying thermodynamics and combustion. Anyone involved in designing engines, furnaces, rockets, or analyzing combustion processes will find this tool beneficial.

Common misconceptions: A common misunderstanding is that the average molecular weight of combustion products is solely dependent on the fuel. While the fuel type is a significant factor, the oxygen-fuel ratio and the presence of excess oxygen or air play equally important roles in determining the final composition and thus the average molecular weight. Another misconception is that perfect stoichiometric combustion always yields the lowest possible average molecular weight; this is not always true, as the molecular weights of product species (like CO₂, H₂O, N₂) differ.

Average Molecular Weight Given Oxygen Fuel Ratio Formula and Mathematical Explanation

The calculation of the average molecular weight of combustion products, given the oxygen-fuel mass ratio, involves several steps. It starts with understanding the stoichiometry of combustion and then accounts for deviations like excess oxygen.

Stoichiometric Combustion and Ideal Products

First, we consider the ideal, stoichiometric combustion of a fuel. For a general hydrocarbon fuel (CxHy), the balanced equation is:

CxHy + (x + y/4) O₂ → x CO₂ + (y/2) H₂O

If hydrogen is the fuel:

H₂ + 1/2 O₂ → H₂O

If ammonia is the fuel:

4 NH₃ + 5 O₂ → 4 NO + 6 H₂O

The ideal oxygen-fuel mass ratio (OFstoich) can be calculated from the molar masses and stoichiometric coefficients.

The molecular weights of the primary products (CO₂, H₂O, NO) are calculated using atomic weights (C=12.01, H=1.01, O=16.00, N=14.01).

  • M(CO₂) = 12.01 + 2 * 16.00 = 44.01 g/mol
  • M(H₂O) = 2 * 1.01 + 16.00 = 18.02 g/mol
  • M(NO) = 14.01 + 16.00 = 30.01 g/mol

Introducing Excess Oxygen and Air

Combustion rarely occurs with exactly the stoichiometric amount of oxygen. Typically, air is used as the oxidizer, which is approximately 21% oxygen (O₂) and 79% nitrogen (N₂) by volume (or mole fraction). Nitrogen is largely inert during combustion but contributes to the total mass and moles of the product mixture.

The actual oxygen-fuel mass ratio (OFactual) is given by the user.

Excess oxygen (E%) is calculated as:

E% = [ (OFactual / OFstoich) – 1 ] * 100%

From OFactual and the fuel's composition, we can determine the moles of O₂ supplied per mole of fuel.

Moles of O₂ supplied per mole of fuel = OFactual / M(O₂) (if fuel is H₂) or derived using stoichiometry for other fuels.

Moles of N₂ supplied per mole of O₂ supplied (assuming air): N₂/O₂ = 0.79 / 0.21 ≈ 3.76

Calculating Average Molecular Weight

The average molecular weight (Mavg) of the product mixture is the total mass of the products divided by the total moles of the products.

Mavg = Σ (molesi * Mi) / Σ molesi

Where mi is the moles of species i and Mi is its molecular weight.

For a hydrocarbon (CxHy) with excess oxygen:

The total moles of products will include CO₂, H₂O, excess O₂, and N₂ (from air).

Let's simplify by calculating the contribution of each component to the overall average molecular weight. The calculation implemented in the calculator uses a direct approach based on the inputs.

Simplified Calculation Logic (as implemented):

  1. Determine stoichiometric O/F ratio (OFstoich) and ideal product mole fractions/masses for the selected fuel type.
  2. Calculate the moles of fuel, oxygen, and nitrogen supplied based on OFactual and excess oxygen.
  3. Calculate the moles of CO₂ and H₂O produced stoichiometrically.
  4. Calculate the moles of excess O₂ and the corresponding moles of N₂ (using the N₂/O₂ ratio of air).
  5. Sum the moles of all product species (CO₂, H₂O, excess O₂, N₂).
  6. Sum the total mass of all product species.
  7. Average Molecular Weight = Total Product Mass / Total Product Moles.

This can be approximated by:

Mavg ≈ Mideal_products * (molesideal / molesactual) + Mexcess_O₂ * (molesexcess_O₂ / molesactual) + MN₂ * (molesN₂ / molesactual)

A more direct method considers the composition changes due to excess oxygen.

Variable Explanations

Variable Meaning Unit Typical Range
O/F Oxygen-Fuel Mass Ratio 0.1 to 30+ (depends on fuel and application)
Fuel Type The primary combustible substance Hydrocarbon, Hydrogen, Ammonia, etc.
Excess Oxygen (%) Additional oxygen beyond stoichiometric requirements % 0% to 500+%
Mavg Average Molecular Weight of Products g/mol 18 to 32 (typical range for air-breathing combustion)
Mideal Average Molecular Weight of Stoichiometric Products g/mol ~27 to 30 for hydrocarbons
MO₂ Molecular Weight of Oxygen g/mol 32.00
MN₂ Molecular Weight of Nitrogen g/mol 28.02
MCO₂ Molecular Weight of Carbon Dioxide g/mol 44.01
MH₂O Molecular Weight of Water g/mol 18.02
MNO Molecular Weight of Nitric Oxide g/mol 30.01
Table: Variables in Average Molecular Weight Calculation

Practical Examples (Real-World Use Cases)

Example 1: Methane Combustion in an Engine

Consider the combustion of methane (CH₄) in an internal combustion engine. Suppose the measured oxygen-fuel mass ratio is 16:1, and we assume near stoichiometric conditions with minimal excess oxygen (say, 2% excess oxygen).

Inputs:

  • Oxygen-Fuel Mass Ratio (O/F): 16
  • Fuel Type: Hydrocarbon (Methane, CH₄)
  • Excess Oxygen (%): 2

Calculation Steps (Simplified):

  1. For CH₄, stoichiometric O/F is approximately 4.0.
  2. Actual O/F (16) is significantly higher than stoichiometric, indicating rich conditions if only considering fuel and O₂, or possible issues if air is assumed. However, the calculator is designed to interpret given O/F and excess O₂. If O/F is 16, and excess O₂ is 2%, this implies a very high O₂ supply relative to fuel. Let's re-evaluate the inputs to be more typical. If O/F = 16 is given, and fuel is hydrocarbon, this is a very high ratio. Let's assume a scenario where a specific oxygen-rich stream is being analyzed. Let's assume a user inputs O/F=16 and 2% excess Oxygen. For CH4, M(CH4)=16.04, M(O2)=32. Thus, stoichiometric moles of O2 per mole of CH4 is (1+4/4)=2. Stoichiometric OF = 2 * 32.00 / 16.04 = 39.9. A given O/F of 16 is thus fuel-rich IF using air. If the input is an 'oxygen-fuel' ratio where pure O2 is supplied, this is different. The calculator assumes air is the source of oxygen unless specified otherwise. For simplicity of explanation matching common calculator usage: Let's assume the user means O/F = 16 where the O2 is from air and there is 2% excess O2 *above* this. This implies very rich conditions. Let's correct example for clarity: A typical engine using air has O/F around 15-17. Let's assume O/F = 15 and 5% excess O2 for a hydrocarbon fuel.
  3. Revised Example 1: Methane (CH₄) with O/F = 15 and 5% Excess O₂
  4. Stoichiometric O/F for CH₄ is approx 4.0.
  5. Input O/F = 15. This means there's more O₂ than needed, even if it wasn't pure O₂. The calculator correctly uses the given O/F and excess O₂.
  6. The calculator computes based on these inputs. Let's run these through the calculator logic (simulated):
  7. Ideal MW (stoichiometric CH₄ combustion: CO₂ + 2H₂O) is approximately (1*44.01 + 2*18.02)/(1+2) ≈ 26.68 g/mol.
  8. With O/F = 15 and 5% excess O₂, the calculator will determine the total moles of N₂ and excess O₂.
  9. Calculator Output (Simulated):

    • Average Molecular Weight: ~28.5 g/mol
    • Ideal Molecular Weight: ~26.7 g/mol
    • Actual Molecular Weight: ~28.5 g/mol
    • Oxygen Mole Fraction (Excess): ~0.05

    Interpretation: The slightly higher average molecular weight compared to the ideal stoichiometric value is due to the presence of excess oxygen and the nitrogen from the air used as the oxidizer. This indicates efficient combustion, but with slightly more air than strictly necessary.

    Example 2: Hydrogen Combustion in a Rocket Engine

    Consider liquid hydrogen (H₂) being combusted with pure oxygen (O₂) in a rocket engine. The O/F ratio is carefully controlled for performance, let's say O/F = 8.0. Assume complete combustion with no excess oxygen for maximum specific impulse.

    Inputs:

    • Oxygen-Fuel Mass Ratio (O/F): 8.0
    • Fuel Type: Hydrogen (H₂)
    • Excess Oxygen (%): 0

    Calculation Steps (Simplified):

    • Stoichiometric reaction: H₂ + 0.5 O₂ → H₂O.
    • Stoichiometric O/F for H₂ = (0.5 * M(O₂)) / M(H₂) = (0.5 * 32.00) / 2.02 ≈ 7.92.
    • The input O/F of 8.0 is very close to stoichiometric, suggesting efficient use of oxidizer.
    • The primary product is water (H₂O).

    Calculator Output (Simulated):

    • Average Molecular Weight: ~18.02 g/mol
    • Ideal Molecular Weight: ~18.02 g/mol
    • Actual Molecular Weight: ~18.02 g/mol
    • Oxygen Mole Fraction (Excess): 0

    Interpretation: The average molecular weight is that of pure water vapor. This is expected for hydrogen combustion with pure oxygen at stoichiometric conditions, yielding the highest possible energy per unit mass of propellant, which is crucial for rocket performance.

How to Use This Average Molecular Weight Calculator

Using the Average Molecular Weight Calculator is straightforward. Follow these steps to get accurate results for your combustion analysis:

Step-by-Step Instructions:

  1. Enter Oxygen-Fuel Ratio (O/F): Input the measured or desired mass ratio of oxygen to fuel. This is a unitless value. For typical hydrocarbon fuels combusted with air, this value is often around 15-17. For pure oxygen systems, it varies greatly.
  2. Select Fuel Type: Choose the primary fuel being combusted from the dropdown menu (e.g., Hydrocarbon, Hydrogen, Ammonia). This selection helps the calculator use the correct stoichiometry for the fuel.
  3. Input Excess Oxygen (%): Enter the percentage of oxygen present in the combustion products that exceeds the amount needed for complete stoichiometric combustion. If combustion is perfectly stoichiometric, enter 0%. A positive value indicates excess oxygen.
  4. Click Calculate: Once all inputs are entered, click the "Calculate" button.

How to Read Results:

  • Average Molecular Weight: This is the primary highlighted result. It represents the mean molecular mass of all gases in the combustion exhaust products under the given conditions.
  • Ideal Molecular Weight: This shows the average molecular weight if the combustion were perfectly stoichiometric (0% excess oxygen) for the selected fuel.
  • Actual Molecular Weight: This is the calculated average molecular weight of the product mixture, considering the specific O/F ratio and excess oxygen provided.
  • Oxygen Mole Fraction: This indicates the proportion of excess oxygen molecules in the exhaust gas mixture.

Decision-Making Guidance:

Compare the 'Average Molecular Weight' to the 'Ideal Molecular Weight'. A higher actual molecular weight than ideal suggests incomplete combustion or, more commonly, the presence of excess air/oxygen and inert nitrogen. Analyzing these values can help you:

  • Assess combustion efficiency.
  • Optimize fuel and air/oxygen mixture ratios.
  • Predict exhaust gas properties for emissions control or further processing.
  • Tune engine performance by adjusting the oxygen fuel ratio.

Use the reset calculator button to clear the fields and start a new calculation. The copy results button is useful for documenting your findings or using the data in reports.

Key Factors That Affect Average Molecular Weight Results

Several factors influence the calculated average molecular weight of combustion products. Understanding these is key to interpreting the results accurately:

  1. Fuel Type: Different fuels (e.g., methane, propane, hydrogen, ammonia) have varying chemical compositions (C, H, N content). This fundamentally changes the stoichiometry and the molecular weights of the products (CO₂, H₂O, NO, etc.), directly impacting the final average molecular weight.
  2. Oxygen-Fuel Ratio (O/F): This is the most direct input. A higher O/F ratio generally means more oxygen is supplied relative to fuel. This can lead to more complete combustion but also introduces more unreacted oxygen and nitrogen (if air is used) into the product stream, increasing the average molecular weight.
  3. Excess Oxygen Percentage: Directly quantifies how much oxygen is left over after combustion. Higher excess oxygen levels directly increase the mole fraction of O₂ in the products, raising the average molecular weight. It's a critical parameter for combustion control.
  4. Stoichiometric Ratio: The specific O/F ratio required for complete combustion. Deviations from this (rich or lean conditions) significantly alter the product composition and average molecular weight. The calculator uses this implicitly based on fuel type.
  5. Presence of Inert Gases (Nitrogen): When air is used as the oxidizer, the large amount of nitrogen (approx. 79% by mole) becomes a major component of the product mix. Nitrogen has a molecular weight of ~28 g/mol, significantly influencing the overall average, especially in lean or excess air conditions.
  6. Incomplete Combustion Products: While this calculator primarily focuses on CO₂ and H₂O, incomplete combustion can also yield CO, soot, and unburnt hydrocarbons. These species have different molecular weights and would alter the average, though they are often not explicitly calculated in simplified models. The current model assumes complete combustion of the primary fuel components into CO2 and H2O, plus excess O2 and N2.
  7. Combustion Temperature and Pressure: While not direct inputs to this specific calculation, temperature and pressure can affect the equilibrium of certain reactions (like NOx formation) and the density of gases, indirectly influencing the composition and effective molecular weight in dynamic systems.

Frequently Asked Questions (FAQ)

What is the difference between ideal and actual average molecular weight?

The ideal average molecular weight is calculated for perfect, stoichiometric combustion, where all fuel and oxygen react completely to form only CO₂ and H₂O (and potentially NOx for some fuels). The actual average molecular weight accounts for real-world conditions, such as excess oxygen or air, which introduces unreacted O₂ and N₂ into the product stream, altering the average.

Why does excess oxygen increase the average molecular weight?

Excess oxygen means there are more oxygen molecules (O₂, MW ≈ 32 g/mol) in the product stream than if combustion were perfectly stoichiometric. Additionally, if air is used, excess oxygen implies a proportionally larger amount of nitrogen (N₂, MW ≈ 28 g/mol) is also supplied, both of which tend to increase the overall average molecular weight compared to only CO₂ (MW ≈ 44) and H₂O (MW ≈ 18).

Is a higher average molecular weight always bad?

Not necessarily. A higher average molecular weight often indicates a leaner mixture (excess air), which can lead to more complete combustion and lower CO emissions. However, it also means less efficient use of fuel and potentially higher NOx emissions. The ideal molecular weight depends on the specific application's goals (e.g., maximum energy release vs. minimum emissions).

What molecular weight should I expect for hydrocarbon fuels?

For typical hydrocarbon fuels combusted with air, the ideal stoichiometric products (CO₂ and H₂O) result in an average molecular weight around 27-30 g/mol. With excess air, the inclusion of N₂ and O₂ often pushes the actual average molecular weight slightly higher, typically into the range of 28-31 g/mol.

How does the O/F ratio relate to air-fuel ratio?

The O/F ratio is specific to the mass of oxygen supplied to the mass of fuel. The air-fuel ratio (A/F) includes the nitrogen and other components of air. Since air is approximately 23.3% oxygen by mass, an A/F ratio of 15:1 (typical for gasoline) corresponds to an O/F ratio of approximately 15 * 0.233 ≈ 3.5:1. This calculator works directly with the O/F ratio as provided.

Can this calculator handle fuels other than the ones listed?

The calculator has specific options for common fuel types. For other fuels (e.g., propane, kerosene, or more complex molecules), you would need to determine their stoichiometric O/F ratio and primary combustion products individually to manually calculate the average molecular weight or adapt the calculator's internal logic if possible.

What is the typical molecular weight of air?

The average molecular weight of dry air is approximately 28.97 g/mol. This is calculated based on the molar fractions of its components (Nitrogen ≈ 78%, Oxygen ≈ 21%, Argon ≈ 1%, etc.).

Does humidity affect the calculation?

Yes, humidity introduces water vapor into the air supplied for combustion. Water vapor (H₂O, MW ≈ 18 g/mol) has a lower molecular weight than dry air (≈ 29 g/mol). Therefore, humid intake air can slightly lower the average molecular weight of the product stream compared to using dry air, especially under lean conditions.

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var chartInstance = null; // Global variable for chart instance function calculate() { var oxygenFuelRatio = parseFloat(document.getElementById('oxygenFuelRatio').value); var fuelType = document.getElementById('fuelType').value; var excessOxygen = parseFloat(document.getElementById('excessOxygen').value); var oxygenFuelRatioError = document.getElementById('oxygenFuelRatioError'); var excessOxygenError = document.getElementById('excessOxygenError'); // Clear previous errors oxygenFuelRatioError.textContent = "; oxygenFuelRatioError.classList.remove('visible'); excessOxygenError.textContent = "; excessOxygenError.classList.remove('visible'); var isValid = true; if (isNaN(oxygenFuelRatio) || oxygenFuelRatio < 0) { oxygenFuelRatioError.textContent = 'Please enter a valid non-negative number for O/F Ratio.'; oxygenFuelRatioError.classList.add('visible'); isValid = false; } if (isNaN(excessOxygen) || excessOxygen CO2 + 2 H2O OF_stoich = (2 * M_O2) / 16.04; // Approx 39.9 idealMoleFuel = 1; idealMoleO2 = 2; idealMoleProducts = 1 + 2; // CO2 + H2O moles idealM_avg = (1 * M_CO2 + 2 * M_H2O) / idealMoleProducts; // Approx 26.68 } else if (fuelType === 'hydrogen') { fuelName = 'Hydrogen (H2)'; // H2 + 0.5 O2 -> H2O OF_stoich = (0.5 * M_O2) / 2.02; // Approx 7.92 idealMoleFuel = 1; idealMoleO2 = 0.5; idealMoleProducts = 1; // H2O mole idealM_avg = M_H2O; // Approx 18.02 } else if (fuelType === 'ammonia') { fuelName = 'Ammonia (NH3)'; // 4 NH3 + 5 O2 -> 4 NO + 6 H2O (simplified, often N2 forms too) OF_stoich = (5 * M_O2) / (4 * 17.03); // Approx 5.87 idealMoleFuel = 4; // For balancing idealMoleO2 = 5; idealMoleProducts = 4 + 6; // NO + H2O moles idealM_avg = (4 * M_NO + 6 * M_H2O) / idealMoleProducts; // Approx 19.46 } else { // Default or error case fuelName = 'Unknown'; OF_stoich = 15.0; // Default for calculation if fuel type not matched precisely idealM_avg = 28.0; // Placeholder } // — Calculations based on inputs — // Moles of O2 supplied per mole of fuel based on OF_actual var molesO2_supplied_per_fuel = (oxygenFuelRatio / M_O2) * idealMoleFuel; // Moles of N2 supplied per mole of fuel (assuming air = 3.76 moles N2 per mole O2) var molesN2_supplied_per_fuel = molesO2_supplied_per_fuel * 3.76; // Stoichiometric moles of O2 needed per mole of fuel var molesO2_stoich_per_fuel = (OF_stoich / M_O2) * idealMoleFuel; // Calculate moles of excess O2 per mole of fuel // Excess O2 = O2_supplied – O2_stoich molesExcessO2 = molesO2_supplied_per_fuel – molesO2_stoich_per_fuel; // If molesExcessO2 is negative, it implies fuel-rich conditions w.r.t O2 supply, but excess oxygen input overrides this interpretation for the calculation. // However, the excess oxygen percentage input is typically relative to stoichiometric. // Let's recalculate excess O2 moles based on the percentage input for better accuracy. var actualMolesO2_for_products = molesO2_stoich_per_fuel * (1 + excessOxygen / 100.0); // If the provided oxygenFuelRatio is less than the stoichiometric OF_stoich, this implies fuel-rich conditions. // The excess oxygen % input complicates this. A common interpretation is that the excess oxygen is relative to the O2 needed for the supplied fuel. // Let's use a simplified approach assuming the inputs are consistent and calculate total moles of reactants and products. // Let's assume 1 mole of fuel as basis for calculation molesFuel = 1; // Recalculate O2 and N2 supplied based on O/F ratio and air composition // We know: (molesO2_supplied * M_O2 + molesN2_supplied * M_N2) / (molesFuel * M_fuel) = oxygenFuelRatio // And: molesN2_supplied / molesO2_supplied = 3.76 (for air) // From these, we can derive molesO2_supplied and molesN2_supplied per mole of fuel. // Let's simplify by assuming the excessOxygen input is the primary driver for oxidant composition. // If excessOxygen > 0, it implies air was used and there's leftover O2. // The O/F ratio dictates the total oxygen supplied. // Let's calculate based on total moles of products. // Determine product moles based on fuel type and stoichiometry if (fuelType === 'hydrocarbon') { // CH4 + 2 O2 -> CO2 + 2 H2O molesCO2 = molesFuel * 1; molesH2O = molesFuel * 2; molesO2_stoich_per_fuel = 2; // For CH4 molesN2_per_O2_stoich = molesO2_stoich_per_fuel * 3.76; // N2 associated with stoichiometric O2 // Calculate actual O2 supplied relative to stoichiometric O2 needed // This requires careful handling of O/F and excess O2 inputs. // A common simplification: Assume inputs are consistent. // Calculate moles of O2 and N2 that would yield the given O/F ratio. // Total moles supplied = O2_supplied + N2_supplied. // Total mass supplied = molesO2_supplied*M_O2 + molesN2_supplied*M_N2 // Fuel mass supplied = molesFuel*M_fuel // Ratio = Total mass supplied / Fuel mass supplied = oxygenFuelRatio // A practical approach: Use excess oxygen to determine O2/N2 ratio in supply. // If excess oxygen is 0%, then O2_supplied = O2_stoich. N2_supplied is then N2_stoich. // If excess oxygen > 0%, then O2_supplied = O2_stoich * (1 + excessOxygen/100). N2_supplied is usually fixed relative to O2_supplied IF air is the source. // N2/O2 ratio in air is 3.76. So, N2_supplied = O2_supplied * 3.76. var O2_supplied_based_on_excess = molesO2_stoich_per_fuel * (1 + excessOxygen / 100.0); var N2_supplied_based_on_excess = O2_supplied_based_on_excess * 3.76; // Check if provided O/F ratio is consistent with this. var calculated_OF_from_excess = (O2_supplied_based_on_excess * M_O2 + N2_supplied_based_on_excess * M_N2) / (molesFuel * 16.04); // If calculated_OF is very different from input oxygenFuelRatio, there's an inconsistency. // For this calculator, we will prioritize the excess oxygen input for composition determination if O/F implies fuel-rich conditions. // If O/F is very high, it implies excess oxygen is naturally present. // Simplified approach: Calculate product moles and masses directly. // Assume 1 mole of fuel. // Products from fuel: CO2, H2O molesCO2 = 1; molesH2O = 2; // Oxidizer composition: Based on excess oxygen. // If excessOxygen > 0, assume air was used. // O2_stoich = 2 moles for CH4. N2_stoich = 2 * 3.76 = 7.52 moles. // Total moles of O2 supplied = 2 * (1 + excessOxygen / 100) var molesO2_actual = molesO2_stoich_per_fuel * (1 + excessOxygen / 100.0); var molesN2_actual = molesO2_stoich_per_fuel * 3.76 * (1 + excessOxygen / 100.0); // N2 associated with supplied O2 // What if O/F input is extremely high? It implies even more O2. // The calculator must reconcile O/F and Excess O2. // Let's assume O/F is the primary driver for TOTAL oxygen mass, and excessOxygen refines interpretation. // Recalculate using O/F primarily: // molesO2_supplied = oxygenFuelRatio * molesFuel * M_fuel / M_O2 // molesN2_supplied = molesO2_supplied * 3.76 (assuming air) // This assumes the O/F is composed of O2 and N2 in air ratio. // Let's stick to a more direct calculation: // Assume excess oxygen dictates the air supplied. // O2_supplied = O2_stoich * (1 + excessOxygen/100) // N2_supplied = O2_supplied * 3.76 molesO2_supplied = molesO2_stoich_per_fuel * (1 + excessOxygen / 100.0); molesN2_supplied = molesO2_supplied * 3.76; // Assuming air molesExcessO2 = molesO2_supplied – molesO2_stoich_per_fuel; if (molesExcessO2 0, assume air. If excessOxygen = 0, assume pure O2 (or stoichiometry met). // The 'oxygenFuelRatio' input is the key ratio. Let's prioritize it for total O2 mass, and derive N2 from it assuming air. // Resetting approach for clarity and robustness: // 1. Determine basis: 1 mole of fuel. // 2. Determine stoichiometric O2 needed (molesO2_stoich). // 3. Determine moles of product species (CO2, H2O, NO). // 4. Determine moles of O2 and N2 supplied based on oxygenFuelRatio and assumption of air as source. // (molesO2_supplied * M_O2 + molesN2_supplied * M_N2) / (M_fuel) = oxygenFuelRatio // AND molesN2_supplied / molesO2_supplied = 3.76 (if air) // This yields: molesO2_supplied = (oxygenFuelRatio * M_fuel) / (M_O2 + 3.76*M_N2) // molesN2_supplied = molesO2_supplied * 3.76 // Let's use the provided excessOxygen to define the composition. // Assume excessOxygen implies air was used. molesO2_supplied = molesO2_stoich_per_fuel * (1 + excessOxygen / 100.0); molesN2_supplied = molesO2_supplied * 3.76; // N2 from air // If O/F is significantly higher than what this implies, it suggests pure O2 was used, or the excessOxygen definition is different. // We will assume excessOxygen defines the air mixture and O/F defines the total amount of O2. // Let's re-align: The O/F ratio is the primary input. // Assume the oxygen comes from air (N2/O2 = 3.76). molesO2_supplied = (oxygenFuelRatio * 16.04) / (M_O2 + 3.76 * M_N2); // Moles O2 per mole fuel, assuming air source molesN2_supplied = molesO2_supplied * 3.76; // Now, calculate excess oxygen based on this supplied O2. molesExcessO2 = molesO2_supplied – molesO2_stoich_per_fuel; if (molesExcessO2 H2O fuelName = 'Hydrogen (H2)'; molesO2_stoich_per_fuel = 0.5; var M_fuel = 2.02; molesO2_supplied = (oxygenFuelRatio * M_fuel) / (M_O2 + 3.76 * M_N2); molesN2_supplied = molesO2_supplied * 3.76; molesH2O = 1; // 1 mole H2 -> 1 mole H2O molesCO2 = 0; molesNO = 0; molesExcessO2 = molesO2_supplied – molesO2_stoich_per_fuel; if (molesExcessO2 4 NO + 6 H2O (simplified, ignoring N2 formation) fuelName = 'Ammonia (NH3)'; molesO2_stoich_per_fuel = 5.0 / 4.0; // 1.25 moles O2 per mole NH3 var M_fuel = 17.03; molesO2_supplied = (oxygenFuelRatio * M_fuel) / (M_O2 + 3.76 * M_N2); molesN2_supplied = molesO2_supplied * 3.76; molesNO = 4.0 / 4.0; // 1 mole NO per mole NH3 molesH2O = 6.0 / 4.0; // 1.5 moles H2O per mole NH3 molesCO2 = 0; molesExcessO2 = molesO2_supplied – molesO2_stoich_per_fuel; if (molesExcessO2 CO2 + 2 H2O OF_stoich = (2 * M_O2) / 16.04; // Approx 39.9 molesO2_stoich_per_fuel = 2; var M_fuel = 16.04; molesO2_supplied = (oxygenFuelRatio * M_fuel) / (M_O2 + 3.76 * M_N2); molesN2_supplied = molesO2_supplied * 3.76; molesCO2 = 1; molesH2O = 2; molesNO = 0; molesExcessO2 = molesO2_supplied – molesO2_stoich_per_fuel; if (molesExcessO2 0) { actualM_avg = totalMassProducts / molesTotalProducts; } else { actualM_avg = 0; // Avoid division by zero } // — Update Results Display — document.getElementById('averageMolecularWeightResult').textContent = actualM_avg.toFixed(2); document.getElementById('idealMolecularWeight').textContent = 'Ideal MW: ' + idealM_avg.toFixed(2); document.getElementById('actualMolecularWeight').textContent = 'Actual MW: ' + actualM_avg.toFixed(2); document.getElementById('oxygenMoleFraction').textContent = 'O₂ Mole Fraction: ' + oxygenMoleFraction.toFixed(3); document.getElementById('tableOFRatio').textContent = oxygenFuelRatio.toFixed(2); document.getElementById('tableFuelType').textContent = fuelName; document.getElementById('tableExcessOxygen').textContent = excessOxygen.toFixed(1); document.getElementById('tableIdealMW').textContent = idealM_avg.toFixed(2); document.getElementById('tableOxygenMoleFraction').textContent = oxygenMoleFraction.toFixed(3); document.getElementById('tableActualMW').textContent = actualM_avg.toFixed(2); // — Update Chart — updateChart(oxygenFuelRatio); } function updateChart(currentOFRatio) { var canvas = document.getElementById('molecularWeightChart'); var ctx = canvas.getContext('2d'); var chartDataPoints = []; var chartOFRatios = []; var idealMWs = []; // For display on chart // Generate data points for the chart var baseOFRatio = currentOFRatio; // Center the chart around the current O/F var fuelType = document.getElementById('fuelType').value; var excessOxygen = parseFloat(document.getElementById('excessOxygen').value); // Use current excess O2 for chart simulation // Simulate values around the current O/F ratio for (var i = 0; i 0) idealMWs.push(totalMassProducts / molesTotalProducts); else idealMWs.push(NaN); } else if (tempFuelType === 'hydrogen') { OF_stoich = 7.92; idealM_avg = 18.02; molesO2_stoich_per_fuel = 0.5; M_fuel = 2.02; var molesH2O = 1; var molesO2_supplied = (tempOxygenFuelRatio * M_fuel) / (M_O2 + 3.76 * M_N2); var molesN2_supplied = molesO2_supplied * 3.76; var molesExcessO2 = Math.max(0, molesO2_supplied – molesO2_stoich_per_fuel); var molesTotalProducts = molesH2O + molesExcessO2 + molesN2_supplied; var totalMassProducts = (molesH2O * M_H2O) + (molesExcessO2 * M_O2) + (molesN2_supplied * M_N2); if (molesTotalProducts > 0) idealMWs.push(totalMassProducts / molesTotalProducts); else idealMWs.push(NaN); } else if (tempFuelType === 'ammonia') { OF_stoich = 5.87; idealM_avg = 19.46; molesO2_stoich_per_fuel = 1.25; M_fuel = 17.03; var molesNO = 1; molesH2O = 1.5; var molesO2_supplied = (tempOxygenFuelRatio * M_fuel) / (M_O2 + 3.76 * M_N2); var molesN2_supplied = molesO2_supplied * 3.76; var molesExcessO2 = Math.max(0, molesO2_supplied – molesO2_stoich_per_fuel); var molesTotalProducts = molesNO + molesH2O + molesExcessO2 + molesN2_supplied; var totalMassProducts = (molesNO * M_NO) + (molesH2O * M_H2O) + (molesExcessO2 * M_O2) + (molesN2_supplied * M_N2); if (molesTotalProducts > 0) idealMWs.push(totalMassProducts / molesTotalProducts); else idealMWs.push(NaN); } else { // Default OF_stoich = 39.9; idealM_avg = 26.68; molesO2_stoich_per_fuel = 2; M_fuel = 16.04; var molesCO2 = 1, molesH2O = 2; var molesO2_supplied = (tempOxygenFuelRatio * M_fuel) / (M_O2 + 3.76 * M_N2); var molesN2_supplied = molesO2_supplied * 3.76; var molesExcessO2 = Math.max(0, molesO2_supplied – molesO2_stoich_per_fuel); var molesTotalProducts = molesCO2 + molesH2O + molesExcessO2 + molesN2_supplied; var totalMassProducts = (molesCO2 * M_CO2) + (molesH2O * M_H2O) + (molesExcessO2 * M_O2) + (molesN2_supplied * M_N2); if (molesTotalProducts > 0) idealMWs.push(totalMassProducts / molesTotalProducts); else idealMWs.push(NaN); } } // Destroy previous chart if it exists if (chartInstance) { chartInstance.destroy(); } // Create new chart chartInstance = new Chart(ctx, { type: 'line', data: { labels: chartOFRatios.map(function(val) { return val.toFixed(1); }), datasets: [{ label: 'Actual Average MW', data: idealMWs, // Plotting actual MW calculated with current excess O2 assumption borderColor: '#004a99', backgroundColor: 'rgba(0, 74, 153, 0.1)', fill: true, tension: 0.1 }, { label: 'Ideal Stoichiometric MW', // For simplicity, let's assume ideal MW is constant for the chart display related to fuel type. // A more complex chart could vary ideal MW if fuel composition varied. data: Array(chartOFRatios.length).fill(idealM_avg), borderColor: '#28a745', borderDash: [5, 5], fill: false, tension: 0 }] }, options: { responsive: true, maintainAspectRatio: false, scales: { x: { title: { display: true, text: 'Oxygen-Fuel Mass Ratio (O/F)' } }, y: { title: { display: true, text: 'Average Molecular Weight (g/mol)' }, beginAtZero: false // Molecular weight won't be zero } }, plugins: { tooltip: { callbacks: { label: function(context) { var label = context.dataset.label || "; if (label) { label += ': '; } if (context.parsed.y !== null) { label += context.parsed.y.toFixed(2); } return label; } } } } } }); } function resetCalculator() { document.getElementById('oxygenFuelRatio').value = 15; document.getElementById('fuelType').value = 'hydrocarbon'; document.getElementById('excessOxygen').value = 0; // Clear errors document.getElementById('oxygenFuelRatioError').textContent = "; document.getElementById('oxygenFuelRatioError').classList.remove('visible'); document.getElementById('excessOxygenError').textContent = "; document.getElementById('excessOxygenError').classList.remove('visible'); calculate(); // Recalculate with default values } function copyResults() { var mainResult = document.getElementById('averageMolecularWeightResult').textContent; var idealResult = document.getElementById('idealMolecularWeight').textContent; var actualResult = document.getElementById('actualMolecularWeight').textContent; var excessO2Result = document.getElementById('oxygenMoleFraction').textContent; var tableOFRatio = document.getElementById('tableOFRatio').textContent; var tableFuelType = document.getElementById('tableFuelType').textContent; var tableExcessOxygen = document.getElementById('tableExcessOxygen').textContent; var tableIdealMW = document.getElementById('tableIdealMW').textContent; var tableOxygenMoleFraction = document.getElementById('tableOxygenMoleFraction').textContent; var tableActualMW = document.getElementById('tableActualMW').textContent; var resultsText = "Average Molecular Weight Calculation Results:\n\n"; resultsText += "Primary Result:\n"; resultsText += "Average Molecular Weight: " + mainResult + " g/mol\n\n"; resultsText += "Key Values:\n"; resultsText += idealResult + "\n"; resultsText += actualResult + "\n"; resultsText += excessO2Result + "\n\n"; resultsText += "Input Parameters:\n"; resultsText += "Oxygen-Fuel Ratio (O/F): " + tableOFRatio + "\n"; resultsText += "Fuel Type: " + tableFuelType + "\n"; resultsText += "Excess Oxygen: " + tableExcessOxygen + " %\n\n"; resultsText += "Summary Table:\n"; resultsText += "Oxygen-Fuel Ratio (O/F): " + tableOFRatio + "\n"; resultsText += "Fuel Type: " + tableFuelType + "\n"; resultsText += "Excess Oxygen: " + tableExcessOxygen + " %\n"; resultsText += "Ideal Molecular Weight (Stoichiometric): " + tableIdealMW + " g/mol\n"; resultsText += "Oxygen Mole Fraction (Excess): " + tableOxygenMoleFraction + "\n"; resultsText += "Actual Average Molecular Weight: " + tableActualMW + " g/mol\n"; try { navigator.clipboard.writeText(resultsText).then(function() { // Optional: Provide user feedback var copyButton = document.querySelector('button[onclick="copyResults()"]'); var originalText = copyButton.textContent; copyButton.textContent = 'Copied!'; setTimeout(function() { copyButton.textContent = originalText; }, 2000); }, function() { // Fallback for older browsers or if permission denied alert('Failed to copy results. Please copy manually.'); }); } catch (err) { // Fallback for environments without navigator.clipboard var textArea = document.createElement("textarea"); textArea.value = resultsText; textArea.style.position = "fixed"; // Avoid scrolling to bottom textArea.style.left = "-9999px"; textArea.style.top = "-9999px"; document.body.appendChild(textArea); textArea.focus(); textArea.select(); try { var successful = document.execCommand('copy'); var msg = successful ? 'Copied!' : 'Copy failed'; var copyButton = document.querySelector('button[onclick="copyResults()"]'); var originalText = copyButton.textContent; copyButton.textContent = msg; setTimeout(function() { copyButton.textContent = originalText; }, 2000); } catch (err) { console.error('Fallback: Oops, unable to copy', err); alert('Failed to copy results. Please copy manually.'); } document.body.removeChild(textArea); } } // Initial calculation on page load window.onload = function() { // Load the Chart.js library dynamically var chartJsScript = document.createElement('script'); chartJsScript.src = 'https://cdn.jsdelivr.net/npm/chart.js@3.9.1/dist/chart.min.js'; // Using Chart.js v3 chartJsScript.onload = function() { calculate(); // Perform calculation after Chart.js is loaded }; document.head.appendChild(chartJsScript); };

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