In the study ofcombustion, theadiabatic flame temperature is the temperature reached by a flame under ideal conditions. It is an upper bound of the temperature that is reached in actual processes.

There are two types ofadiabatic flame temperature:constant volume andconstant pressure, depending on how the process is completed. Theconstant volume adiabatic flame temperature is the temperature that results from a complete combustion process that occurs without anywork,heat transfer or changes inkinetic orpotential energy. Its temperature is higher than in theconstant pressure process because no energy is utilized to change the volume of the system (i.e., generate work).

In daily life, the vast majority of flames one encounters are those caused by rapidoxidation ofhydrocarbons in materials such aswood,wax,fat,plastics,propane, andgasoline. The constant-pressure adiabatic flame temperature of such substances in air is in a relatively narrow range around 1,950 °C (2,220 K; 3,540 °F).^{[citation needed]} This is mostly because theheat of combustion of these compounds is roughly proportional to the amount of oxygen consumed, which proportionally increases the amount of air that has to be heated, so the effect of a larger heat of combustion on the flame temperature is offset. Incomplete reaction at higher temperature further curtails the effect of a larger heat of combustion.^{[citation needed]}

Because most combustion processes that happen naturally occur in the open air, there is nothing that confines the gas to a particular volume like the cylinder in an engine. As a result, these substances will burn at a constant pressure, which allows the gas to expand during the process.

Assuming initial atmospheric conditions (1 bar and 20 °C), the following table^[1] lists the flame temperature for various fuels under constant pressure conditions. The temperatures mentioned here are for astoichiometricfuel-oxidizer mixture (i.e.equivalence ratioφ = 1).

Note that these are theoretical, not actual, flame temperatures produced by a flame that loses no heat. The closest will be the hottest part of a flame, where the combustion reaction is most efficient. This also assumes complete combustion (e.g. perfectly balanced, non-smoky, usually bluish flame). Several values in the table significantly disagree with the literature^[1] or predictions by online calculators.

Adiabatic flame temperature (constant pressure) of common fuels

Fuel	Oxidizer 1 bar 20 °C	${\displaystyle T_{\text{ad}}}$
		(°C)	(°F)
Acetylene (C2H2)	Air	2,500	4,532
	Oxygen	3,480	6,296
Butane (C4H10)	Air	2,231	4,074[2]
Cyanogen (C2N2)	Oxygen	4,525	8,177
Dicyanoacetylene (C4N2)	Oxygen	4,990	9,010
Ethane (C2H6)	Air	1,955	3,551
Ethanol (C2H5OH)	Air	2,082	3,779[3]
Gasoline	Air	2,138	3,880[3]
Hydrogen (H2)	Air	2,254	4,089[3]
Magnesium (Mg)	Air	1,982	3,600[4]
Methane (CH4)	Air	1,963	3,565[5]
Methanol (CH3OH)	Air	1,949	3,540[5]
Naphtha	Air	2,533	4,591[2]
Natural gas	Air	1,960	3,562[6]
Pentane (C5H12)	Air	1,977	3,591[5]
Propane (C3H8)	Air	1,980	3,596[7]
Methylacetylene (CH3CCH)	Air	2,010	3,650
	Oxygen	2,927	5,301
Toluene (C7H8)	Air	2,071	3,760[5]
Wood	Air	1,980	3,596
Kerosene	Air	2,093[8]	3,801
Light fuel oil	Air	2,104[8]	3,820
Medium fuel oil	Air	2,101[8]	3,815
Heavy fuel oil	Air	2,102[8]	3,817
Bituminous coal	Air	2,172[8]	3,943
Anthracite	Air	2,180[8]	3,957
	Oxygen	≈3,500[9]	≈6,332
Aluminium	Oxygen	3,732	6,750[5]
Lithium	Oxygen	2,438	4,420[5]
Phosphorus (white)	Oxygen	2,969	5,376[5]
Zirconium	Oxygen	4,005	7,241[5]

From thefirst law of thermodynamics for a closed reacting system we have

${\displaystyle {}_R{Q}_P-{}_R{W}_P=U_P-U_R}$

where,${\displaystyle {}_R{Q}_P}$ and${\displaystyle {}_R{W}_P}$ are the heat and work transferred from the system to the surroundings during the process, respectively, and${\displaystyle U_R}$ and${\displaystyle U_P}$ are the internal energy of the reactants and products, respectively. In the constant volume adiabatic flame temperature case, the volume of the system is held constant and hence there is no work occurring:

${\displaystyle {}_R{W}_P=\underset{R}{\overset{P}{\int }}pdV=0}$

There is also no heat transfer because the process is defined to be adiabatic:${\displaystyle {}_R{Q}_P=0}$. As a result, the internal energy of the products is equal to the internal energy of the reactants:${\displaystyle U_P=U_R}$. Because this is a closed system, the mass of the products and reactants is constant and the first law can be written on a mass basis,

${\displaystyle U_P=U_R\Rightarrow m_P{u}_P=m_R{u}_R\Rightarrow u_P=u_R}$.

In the case of the constant pressure adiabatic flame temperature, the pressure of the system is held constant, which results in the following equation for the work:

${\displaystyle {}_R{W}_P=\underset{R}{\overset{P}{\int }}pdV=p\left(V_P-V_R\right)}$

Again there is no heat transfer occurring because the process is defined to be adiabatic:${\displaystyle {}_R{Q}_P=0}$. From the first law, we find that,

${\displaystyle -p\left(V_P-V_R\right)=U_P-U_R\Rightarrow U_P+p{V}_P=U_R+p{V}_R}$

Recalling the definition ofenthalpy we obtain${\displaystyle H_P=H_R}$. Because this is a closed system, the mass of the products and reactants is the same and the first law can be written on a mass basis:

${\displaystyle H_P=H_R\Rightarrow m_P{h}_P=m_R{h}_R\Rightarrow h_P=h_R}$.

We see that the adiabatic flame temperature of the constant pressure process is lower than that of the constant volume process. This is because some of the energy released during combustion goes, as work, into changing the volume of the control system.

If we make the assumption that combustion goes to completion (i.e. forming onlyCO
₂ andH
₂O), we can calculate the adiabatic flame temperature by hand either atstoichiometric conditions or lean of stoichiometry (excess air). This is because there are enough variables and molar equations to balance the left and right hand sides,

${\displaystyle {\mathrm{C}}_{\alpha }{\mathrm{H}}_{\beta }{\mathrm{O}}_{\gamma }{\mathrm{N}}_{\delta }+\left(a{\mathrm{O}}_2+b{\mathrm{N}}_2\right)\to {\nu }_1{\mathrm{C}\mathrm{O}}_2+{\nu }_2{\mathrm{H}}_2\mathrm{O}+{\nu }_3{\mathrm{N}}_2+{\nu }_4{\mathrm{O}}_2}$

Rich of stoichiometry there are not enough variables because combustion cannot go to completion with at leastCO andH
₂ needed for the molar balance (these are the most common products of incomplete combustion),

${\displaystyle {\mathrm{C}}_{\alpha }{\mathrm{H}}_{\beta }{\mathrm{O}}_{\gamma }{\mathrm{N}}_{\delta }+\left(a{\mathrm{O}}_2+b{\mathrm{N}}_2\right)\to {\nu }_1{\mathrm{C}\mathrm{O}}_2+{\nu }_2{\mathrm{H}}_2\mathrm{O}+{\nu }_3{\mathrm{N}}_2+{\nu }_5\mathrm{C}\mathrm{O}+{\nu }_6{\mathrm{H}}_2}$

However, if we include thewater gas shift reaction,

${\displaystyle {\mathrm{C}\mathrm{O}}_2+H_2\iff \mathrm{C}\mathrm{O}+{\mathrm{H}}_2\mathrm{O}}$

and use the equilibrium constant for this reaction, we will have enough variables to complete the calculation.

Different fuels with different levels of energy and molar constituents will have different adiabatic flame temperatures.

We can see by the following figure whynitromethane (CH₃NO₂) is often used as a power boost for cars. Since each molecule of nitromethane contains an oxidant with relatively high-energy bonds between nitrogen and oxygen, it can burn much hotter than hydrocarbons or oxygen-containing methanol. This is analogous to adding pure oxygen, which also raises the adiabatic flame temperature. This in turn allows it to build up more pressure during a constant volume process. The higher the pressure, the more force upon the piston creating more work and more power in the engine. It stays relatively hot rich of stoichiometry because it contains its own oxidant. However, continual running of an engine on nitromethane will eventually melt the piston and/or cylinder because of this higher temperature.

In real world applications, complete combustion does not typically occur. Chemistry dictates thatdissociation andkinetics will change the composition of the products. There are a number of programs available that can calculate the adiabatic flame temperature taking into account dissociation through equilibrium constants (Stanjan, NASA CEA, AFTP). The following figure illustrates that the effects of dissociation tend to lower the adiabatic flame temperature. This result can be explained throughLe Chatelier's principle.

• Flame speed

• Babrauskas, Vytenis (2006-02-25)."Temperatures in flames and fires".Fire Science and Technology Inc. Archived fromthe original on 12 January 2008. Retrieved2008-01-27.
• Computation of adiabatic flame temperatureArchived 2019-02-27 at theWayback Machine
• Adiabatic flame temperature

• "Adiabatic Flame Temperature".The Engineering Toolbox.Archived from the original on 28 January 2008. Retrieved2008-01-27. adiabatic flame temperature of hydrogen, methane, propane and octane with oxygen or air as oxidizers
• "Flame Temperatures for some Common Gases".The Engineering Toolbox.Archived from the original on 7 January 2008. Retrieved2008-01-27.
• Temperature of a blue flame and common materials

• Online adiabatic flame temperature calculatorArchived 2012-12-26 at theWayback Machine usingCantera
• Adiabatic flame temperature program
• Gaseq, program for performing chemical equilibrium calculations.
• Flame Temperature Calculator - Constant pressure bipropellant adiabatic combustion
• Adiabatic Flame Temperature calculator

• Combustion
• Temperature
• Threshold temperatures

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