๐Ÿ”ฅ Combustion Products Analysis

Calculate wet/dry molar compositions of flue gas products and theoretical air for various hydrocarbon fuel mixtures and excess air values.

โšก Fortran 90 Engine Double Precision (IEEE 754) โœ“ ISO / ASME Validated
Combustion Products Analysis Tools
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๐Ÿ“… Released Jun 2026
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๐Ÿ“ Configuration

โ›ฝ Fuel
๐Ÿงช Custom Composition (mass fractions)
Key:
Oโ‚‚_stoich = C/12 + H/4 โˆ’ O/32 + S/32
T_ad = T_air + Hc / ฮฃ(nแตขยทCpแตข)

๐Ÿ“Š Results

Configure inputs and click Compute.

๐Ÿ“˜ Methodology

Stoichiometry

Complete combustion stoichiometry computes the theoretical Oโ‚‚ demand from the fuel's ultimate analysis (C, H, O, S mass fractions). Excess air ensures complete combustion and determines the Oโ‚‚ content in flue gas.

Adiabatic Flame Temperature

T_ad = T_air + Hc / ฮฃ(nแตขยทCpแตข), where Hc is the lower heating value and nแตข are the product moles. This is a simplified first-law estimate assuming no dissociation or heat loss.

Air-Fuel Ratio

AFR = actual_air ร— MW_air / fuel_mass. Higher excess air lowers flame temperature but ensures complete combustion. Typical values: 10-20% excess for gas, 20-50% for solid fuels.

๐Ÿ“˜ Calculation Methodology: Flue Gas Combustion Products & Stoichiometric Air

Mathematical Model & Theory

Combustion stoichiometry calculates the theoretical oxygen and atmospheric air required to oxidize hydrocarbon fuels $C_x H_y O_z$, predicting wet and dry flue gas composition:

$$C_x H_y O_z + \lambda n_{th}(O_2 + 3.76 N_2) \to x CO_2 + \frac{y}{2}H_2O + (\lambda-1)n_{th} O_2 + 3.76 \lambda n_{th} N_2$$
$$n_{th} = x + \frac{y}{4} - \frac{z}{2}, \quad \text{Excess Air \%} = (\lambda - 1)\times 100\%$$

Assumptions

  • Complete combustion without unburned hydrocarbons or carbon monoxide.
  • Standard dry air composition: $21\%\ O_2, 79\%\ N_2$.

Academic References

  1. Turns, S. R.: An Introduction to Combustion, McGraw-Hill.
  2. ASME PTC 4: Fired Steam Generators Performance Test Code.

Worked Engineering Example

Problem Statement:
Propane ($C_3H_8$) burns with $20\%$ excess air ($\lambda = 1.20$). Calculate stoichiometric air-to-fuel ratio $(AF)_{stoich}$ and total moles of flue gas per mole fuel.

Step-by-step Solution:
1. $n_{th} = 3 + 8/4 = 5.0\text{ moles } O_2$.
2. $(AF)_{stoich} = \frac{5.0 \times 32 + 5.0 \times 3.76 \times 28.02}{44.09} = \frac{160 + 526.8}{44.09} = 15.58\text{ kg air/kg fuel}$.
3. Flue gas per mole $C_3H_8$: $3 CO_2 + 4 H_2O + (1.2-1)(5) O_2 + 1.2(5)(3.76) N_2 = 3 + 4 + 1.0 + 22.56 = 30.56\text{ moles}$.
Final Result:
Stoichiometric air/fuel ratio is $\mathbf{15.58\text{ kg/kg}}$ producing $\mathbf{30.56\text{ mol flue gas/mol fuel}}$.