DOFPro Team

Combustion reactions are rapid oxidation reactions. One usually burns a fuel (typically coal, oil or natural gas) in air (or rarely pure oxygen). The principal atomic species in combustion reactions are carbon, hydrogen, sulfur and oxygen.
Solid Fuels: Principally coal, coke, wood, charcoal, and solid waste.
Liquid Fuels: Principally hydrocarbons and alcohols.
Gaseous Fuels: Principally natural gas.
Coal is really nasty stuff. There is no other way to put it.
| Component | Percentage |
|---|---|
| carbon [\(\mathrm{C}\)] | 75–90 |
| hydrogen [\(\mathrm{H}\)] | 4.5–5.5 |
| nitrogen [\(\mathrm{N}\)] | 1–1.5 |
| sulfur [\(\mathrm{S}\)] | 1–2 |
| oxygen \(\mathrm{[O}\)] | 5–20 |
| ash | 2–10 |
| moisture [\(\mathrm{H_2O}\)] | 1–10 |
http://www.chemistryexplained.com/Ce-Co/Coal.html
| Component | Bituminous | Subbituminous | Lignite |
|---|---|---|---|
| SiO2 | 20–60 | 40–60 | 15–45 |
| Al2O3 | 5–35 | 20–30 | 10–25 |
| Fe2O3 | 10–40 | 4–10 | 4–15 |
| CaO | 1–12 | 5–30 | 15–40 |
| MgO | 0–5 | 1–6 | 3–10 |
| SO3 | 0–4 | 0–2 | 0–10 |
| Na2O | 0–4 | 0–2 | 0–6 |
| K2O | 0–3 | 0–4 | 0–4 |
| LOI | 0–15 | 0–3 | 0–5 |
https://www.fhwa.dot.gov/publications/research/infrastructure/structures/97148/cfa51.cfm
https://pubs.usgs.gov/fs/2015/3037/pdf/fs2015-3037.pdf
The heating value of a fuel is the negative of its heat of combustion. There are two types
Higher Heating Value (HHV): Assumes the final state of the water is liquid (same as for heat of combustion).
Lower Heating Value (LHV): Assumes the final state of the water is vapor.
\[ HHV = LHV + n_\mathrm{H_2O} \Delta \hat{H}_v\ (\mathrm{H_2O},\ 25\ ^\circ\mathrm{C}) \]
\[ HV_\mathrm{mix} = \sum x_i HV_i \]
If we operate a combustor such that we extract no heat from the combustor, all of the enthalpy of reaction has to go into heating the combustion products.

\(T_\mathrm{in}\)
\(T_\mathrm{out} = T_\mathrm{af}\)
\(Q\text{ or }\dot{Q} = 0\)
\(\Delta H\text{ or }\Delta \dot{H} = 0\)
\[ \sum_\mathrm{out} \dot{n}_j \int\limits_{T_\mathrm{ref}}^{T_\mathrm{out} = T_\mathrm{af}} C_{pj} dT - \sum_\mathrm{in} \dot{n}_i \int\limits_{T_\mathrm{ref}}^{T_\mathrm{in}} C_{pi} dT + \sum_\mathrm{rxns} \dot{\xi}_k(\Delta \hat{H}_r^\circ)_k = \dot{Q} = 0 \]
The adiabatic flame temperature is the maximum temperature a fuel-air mixture can reach when it burns. The maximum adiabatic flame temperature occurs when burning with stoichiometric air. To be useable, some heat has to be extracted from the burning mixture, which lowers the maximum temperature.
Many of the \(C_p\) formulas found in the literature do not go to a high enough temperature range to permit calculation of \(T_\mathrm{af}\) for near-stoichiometric fuel-air mixtures.
To process materials at higher temperatures than adiabatic flame temperatures, some other technique such as electromagnetic, or laser heating must be used.
For fuel-air mixtures that are either too fuel lean or too fuel rich, the oxidation reaction does not generate enough heat to sustain a flame or reaction. The limits of fuel-air mixtures are called the flammability limits.
The Flash Point is the temperature above which the vapor pressure is high enough to create a flammable mixture.
The Autoignition Temperature is the temperature above which a fuel-air mixture will combust without an additional source of spark or flame.
| Species | LFL/LEL in vol. % | UFL/UEL in vol. % | Flash Point | Autoignition temperature |
|---|---|---|---|---|
| Acetone | 2.6–3 | 12.8–13 | −17 °C | 465 °C, 485 °C |
| Benzene | 1.2 | 7.8 | −11 °C | 560 °C |
| n-butane | 1.6 | 8.4 | −60 °C | 420–500 °C |
| CO | 12[6] | 75 | Fl. gas | 609 °C |
| Diesel fuel | 0.6 | 7.5 | >62 °C | 210 °C |
| Ethanol | 3–3.3 | 19 | 12.8 °C | 365 °C |
| Gasoline | 1.4 | 7.6 | <−40 °C | 246–280 °C |
| Hydrogen | 4/18.3[25] | 75/59 | Fl. gas | 500–571 °C |
| Isopropanol | 2[6] | 12 | 12 °C | 398–399 °C |
| Jet A-1 fuel | 0.6–0.7 | 4.9–5 | >38 °C | 210 °C |
| Methane | 5.0 | 14.3 | Fl. gas | 580 °C |
| Propylene | 2 | 11.1 | −108 °C | 458 °C |
| Veg. oil | 327 °C |
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