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Flame resulting from the combustion (burning) of a fuel.

Combustion or burning is a complex sequence of exothermic chemical reactions between a fuel and an oxidant accompanied by the production of heat or both heat and light in the form of either a glow or flames. The most commonly used fuels are solid coal and hydrocarbon gases or liquids.

In complete combustion, a compound such as methane (CH₄) reacts with an oxidizing element such as oxygen (O₂) and the combustion products are compounds of each element in the fuel with the oxidizing element. For example:

methane + oxygen → carbon dioxide + water vapor
CH₄ + 2O₂ → CO₂ + 2H₂O

A simpler example is the combustion of hydrogen (H₂) and oxygen, which is a commonly used reaction in rocket engines:

hydrogen + oxygen → water vapor
2H₂ + O₂ → 2H₂O

In the large majority of the real world uses of combustion, the oxygen oxidant is obtained from the ambient air. Taking air to contain 79 volume percent of non-combustible nitrogen (N₂) and 21 volume percent oxygen, the resultant flue gas from the combustion of a fuel will contain nitrogen plus the products of combustion:

methane + oxygen + nitrogen → carbon dioxide + water vapor + nitrogen
CH₄ + 2O₂ + 7.52N₂ → CO₂ + 2H₂O + 7.52N₂

As can be seen, when air is the source of the oxygen, nitrogen is by far the largest part of the resultant flue gas.

In reality, combustion processes are never perfect or complete. In the flue gases from the combustion of carbon (as in coal combustion) or carbon compounds (as in combustion of hydrocarbons, wood, etc.) both unburned carbon (as soot) and carbon compounds other than carbon dioxide such as carbon monoxide (CO) and others will be present. Also, when air is the oxidant, some nitrogen will be oxidized to various nitrogen oxides (NO_x).

Types of combustion

Rapid

Rapid combustion is a form of combustion in which large amounts of heat and light energy are released, which often results in a fire. This is used in internal combustion engines and in thermobaric weapons. Sometimes, a large volume of gas is liberated in combustion besides the production of heat and light. The sudden evolution of large quantities of gas creates excessive pressure that produces a loud noise. Such a combustion is known as an explosion or detonation.

Slow

Slow combustion is a form of combustion which takes place at low temperatures. Cellular respiration is an example of slow combustion.

Turbulent

Turbulent combustion is a combustion characterized by turbulent flows. It is used for industrial applications such as gas turbines and diesel engines because the turbulence helps to mix the fuel and oxidizer.

Microgravity

Nearly every flame behaves differently in a microgravity environment. Microgravity combustion research contributes to understanding of spacecraft fire safety and diverse aspects of combustion physics.

Incomplete

Incomplete combustion occurs when there isn't enough oxygen to allow the fuel (usually a hydrocarbon) to react completely with the oxygen to produce carbon dioxide and water or when the combustion is quenched by a heat sink such as a solid surface or a flame trap.

The quality of combustion can be improved by the design of combustion devices such as furnace burners and internal combustion engines. Further improvements are achievable by catalytic after-burning devices or by the simple partial return of the exhaust gases into the combustion process. Such devices are required by environmental legislation for vehicles in most countries, and may be necessary in large combustion sources, such as the steam generating furnaces in thermal power plants, to reach legal emission standards.

(PD) Photo: Jens Buurgaard Nielsen
Smouldering embers of a solid barbecue fuel.

Smouldering

Smouldering is a flameless form of combustion. The fundamental difference between smouldering and flaming combustion is that in smouldering, the oxidation occurs on the surface of a solid fuel rather than in the gas phase. The characteristic temperature and heat released during smouldering are low compared to those in flaming combustion (i.e., ~ 600°C vs. ~ 1500°C). Smouldering propagates in a creeping fashion, around 0.1 mm/s, which is about ten times slower than flames spread over a solid. In spite of its weak combustion characteristics, smouldering is a significant fire hazard.

Combustion with other oxidants

Oxygen is usually assumed as the oxidant when talking about combustion, but other oxidants exist. Nitrous oxide (NO) is used in rockets and in race cars. Fluorine (F₂), another oxidizing element, can produce a combustion reaction that yields fluorinated products rather than oxides. For example, mixtures of gaseous fluorine and methane are explosive. Chlorine trifluoride is a strong fluorinating agent that ignites fuels more readily than oxygen.

Chemical equations

Generally, the chemical equation for stoichiometric burning of hydrocarbon in oxygen is as follows:

C_xH_y + ( x + 0.25 y ) O₂ → x CO₂ + ( 0.50 y ) H₂O

For example, the burning of propane is:

C₃H₈ + 5 O₂ → 3 CO₂ + 4 H₂O

The simple word equation for the combustion of a hydrocarbon in oxygen is:

fuel + oxygen → carbon dioxide + water vapor

If the combustion takes place using air as the oxygen source, the nitrogen can be added to the equation, although it does not react, to show the composition of the flue gas:

C_xH_y + ( x + 0.25 y ) O₂ + 3.76 ( x + 0.25 y ) N₂ → x CO₂ + ( 0.50 y ) H₂O + 3.76 ( x + 0.25 y ) N₂

For example, the burning of propane in air is:

C₃H₈ + 5 O₂ + 18.8 N₂ → 3 CO₂ + 4 H₂O + 18.8 N₂

The simple word equation for the combustion of a hydrocarbon in air is:

fuel + air → carbon dioxide + water + nitrogen

Nitrogen may also oxidize when there is an excess of oxygen. The reaction is thermodynamically favored only at high temperatures. Diesel engines are run with an excess of oxygen to combust small particles that tend to form with only a stoichiometric amount of oxygen, necessarily producing nitrogen oxide emissions.

Fuels

Liquid fuels

Combustion of a liquid fuel in an oxidizing atmosphere actually happens in the gas phase. It is the vapour that burns, not the liquid. Therefore, a liquid will normally catch fire only above a certain temperature, its flash point. The flash point of a liquid fuel is the lowest temperature at which it can form an ignitable mix with air. It is also the minimum temperature at which there is enough evaporated fuel in the air to start combustion.

Solid fuels

The act of combustion consists of three relatively distinct but overlapping phases:

Preheating phase, when the unburned fuel is heated up to its flash point and then fire point. Flammable gases start being evolved in a process similar to dry distillation.
Distillation phase or gaseous phase, when the mix of evolved flammable gases with oxygen is ignited. Energy is produced in the form of heat and light. Flames are often visible. Heat transfer from the combustion to the solid maintains the evolution of flammable vapors.
Charcoal phase or solid phase, when the output of flammable gases from the material is too low for persistent presence of flame and the charred fuel does not burn rapidly anymore but just glows and later only smoulders.

Adiabatic Flame Temperatures
Gas	Formula	°C
Hydrogen	H₂	2,181
Methane	CH₄	2,014
Ethane	C₂H₆	2,063
Ethylene	C₂H₄	2,231
Propane	C₃H₈	2,076
Propylene	C₃H₆	2,171
Butane	C₄H₁₀	2,078
Pentane	C₅H₁₂	2,083
Hexane	C₆H₁₄	2,087
Notes: Gas temperature = 25 °C Combustion air temperature = 25 °C Air relative humidity = 60% Excess combustion air = 0 %

Adiabatic flame temperature

Assuming complete combustion under adiabatic conditions (i.e., no heat loss or gain), the adiabatic flame temperature can be calculated. The calculation is based on the first law of thermodynamics (i.e., the conservation of energy) and on the fact that the heat of combustion is used entirely for heating the fuel, the combustion air or oxygen, and the combustion product gases.^[1]^[2]

In the case of fossil fuels burnt in air, the combustion temperature depends on:

the heat of combustion (also referred to as the heating value)
the stoichiometric air-fuel ratio ${\lambda }$
the specific heat capacity of the fuel and the air
the air and fuel inlet temperatures, as well as the relative humidity of the air

The adiabatic flame temperature increases for higher heating values and for higher inlet air and fuel temperatures and for stoichiometric air-fuel ratios approaching one.

Most commonly, the approximate adiabatic flame temperatures for coals are 2200 °C, 2150 °C for fuel oils and 2000 °C for natural gases. The adjacent table lists some calculated adiabatic flame temperatures for hydrogen and for various hydrocarbon gases, all at the conditions stated in the notes at the bottom of the table.

In industrial fired heaters, power plant steam generators, and large gas-fired turbines, the more common way of expressing the usage of more than the stoichiometric combustion air is percent excess combustion air. For example, excess combustion air of 15 percent means that 15 percent more than the required stoichiometric air is being used.

References

↑ Milton R.Beychok (2005). Fundamentals of Stack Gas Dispersion, 4th Edition. author-published, pp. 173-177. ISBN 0-9644588-0-2.
↑ Flame Temperature Professor Hsin Chu, National Cheng Kung University, Taiwan

General:

Merle C. Potter and Craig W. Somerton (2006). Schaum's Outline of Thermodynamics for Engineers, 2nd Edition. McGraw-Hill. ISBN 0-07-146306-2.
Steven S. Zumdahl (2003). Introductory Chemistry: A Foundation, 5th Edition. Brooks Cole. ISBN 0-618-30499-1.
Warren C. Strahle (1993). An Introduction to Combustion, 1st Edition. ISBN 2-88124-608-7.

[1] Milton R.Beychok (2005). Fundamentals of Stack Gas Dispersion, 4th Edition. author-published, pp. 173-177. ISBN 0-9644588-0-2.

[2] Flame Temperature Professor Hsin Chu, National Cheng Kung University, Taiwan

[1]

[2]

@@ Line 1: / Line 1: @@
 {{subpages}}
 [[Image:Combustion flame.jpg|thumb|200px|Flame resulting from the combustion (burning) of a fuel.]]
-'''Combustion''' or '''burning''' is a complex sequence of [[exothermic]] [[chemical reaction]]s between a [[fuel]] and an [[oxidant]] accompanied by the production of [[heat]] or both heat  and [[light]] in the form of either a glow or [[flame]]s.
+'''Combustion''' or '''burning''' is a complex sequence of [[exothermic]] [[chemical reaction]]s between a [[fuel]] and an [[Oxidation|oxidant]] accompanied by the production of [[heat]] or both [[heat]] and [[light]] in the form of either a glow or [[flame]]s. The most commonly used fuels are solid [[coal]] and [[hydrocarbon]] [[gas]]es or [[liquid]]s.
-<!-- Commenting this section out, because it is a bit of esoteric information which really is not needed and may confuse many readers. If many others disagree, it can always be added back in.:
-"Direct combustion by atmospheric oxygen is a reaction mediated by [[Radical (chemistry)|radical]] intermediates. The conditions for radical production are naturally produced by [[thermal runaway]], where the heat generated by combustion is necessary to maintain the high temperature necessary for radical production."-->
+In complete combustion, a compound such as [[methane]] (CH<sub>4</sub>) reacts with an [[Oxidation|oxidizing]] element such as [[oxygen]] (O<sub>2</sub>) and the combustion products are compounds of each element in the fuel with the oxidizing element. For example:
+<center>'''methane + oxygen → carbon dioxide + water vapor'''<br/>
+'''CH<sub>4</sub> + 2O<sub>2</sub> → CO<sub>2</sub> + 2H<sub>2</sub>O'''</center>
-In a complete combustion reaction, a compound reacts with an oxidizing element, such as [[oxygen]] or [[fluorine]], and the products are compounds of each element in the fuel with the oxidizing element. For example:
+A simpler example is the combustion of [[hydrogen]] (H<sub>2</sub>) and oxygen, which is a commonly used reaction in [[rocket]] engines:
+<center>'''hydrogen + oxygen → water vapor'''<br/>
-:'''CH<sub>4</sub>  + 2O<sub>4</sub> → CO<sub>2</sub>  + 2H<sub>2</sub>O'''
+'''2H<sub>2</sub> + O<sub>2</sub> → 2H<sub>2</sub>O'''</center>
-:'''CH<sub>2</sub>S + 6F<sub>2</sub> → CF<sub>2</sub> + 2HF + SF<sub>6</sub> '''
-A simpler example can be seen in the combustion of hydrogen and oxygen, which is a commonly used reaction in rocket engines:
-:'''2H<sub>2</sub> + O<sub>2</sub> → 2H<sub>2</sub>O + heat'''
-The result is water vapor.
+In the large majority of the real world uses of combustion, the oxygen oxidant is obtained from the ambient [[air]]. Taking air to contain 79 volume percent of non-combustible [[nitrogen]] (N<sub>2</sub>) and 21 volume percent oxygen, the resultant [[flue gas]] from the combustion  of a fuel will contain nitrogen plus the products of combustion:
+<center>'''methane + oxygen + nitrogen → carbon dioxide + water vapor + nitrogen'''<br/>
-In the large majority of the real world uses of combustion, the oxygen (O<sub>2</sub>) oxidant is obtained from the ambient air and the resultant [[flue gas]] from the combustion will contain [[nitrogen]]:
+'''CH<sub>4</sub> + 2O<sub>2</sub> + 7.52N<sub>2</sub> → CO<sub>2</sub> + 2H<sub>2</sub>O + 7.52N<sub>2</sub>'''</center>
-:'''CH<sub>4</sub> + 2O<sub>2</sub> + 7.52N<sub>2</sub> → CO<sub>2</sub> + 2H<sub>2</sub>O + 7.52N<sub>2</sub> + heat
 As can be seen, when air is the source of the oxygen, nitrogen is by far the largest part of the resultant flue gas.
-In reality, combustion processes are never perfect or complete. In the flue gases from the combustion of [[carbon]] (as in [[coal]] combustion) or carbon [[compound]]s (as in combustion of [[hydrocarbons]], [[wood]], etc.) both unburned carbon (as [[soot]]) and carbon compounds ([[carbon monoxide|CO]] and others) will be present. Also, when air is the oxidant, some nitrogen will be oxidized to various [[nitrogen oxides]] (NO<sub>x</sub>).
+In reality, combustion processes are never perfect or complete. In the flue gases from the combustion of [[carbon]] (as in [[coal]] combustion) or carbon [[compound]]s (as in combustion of [[hydrocarbons]], [[wood]], etc.) both unburned carbon (as [[soot]]) and carbon compounds other than carbon dioxide such as [[carbon monoxide]] (CO) and  others will be present. Also, when air is the oxidant, some nitrogen will be oxidized to various [[nitrogen oxides]] (NO<sub>x</sub>).
-==Types==
+==Types of combustion==
 ===Rapid===
-Rapid combustion is a form of combustion in which large amounts of heat and [[light]] energy are released, which often results in a [[fire]]. This is used in a form of machinery such as [[internal combustion engine]]s and in [[thermobaric weapon]]s. Sometimes, a large volume of gas is liberated in combustion besides the production of heat and light.The sudden evolution of large quantities of gas creates excessive [[pressure]] that produces a loud noise. Such a combustion is known as an [[explosion]] or [[detonation]].
+Rapid combustion is a form of combustion in which large amounts of heat and [[light]] energy are released, which often results in a [[fire]]. This is used in [[internal combustion engine]]s and in [[thermobaric weapon]]s. Sometimes, a large volume of gas is liberated in combustion besides the production of heat and light. The sudden evolution of large quantities of gas creates excessive [[pressure]] that produces a loud noise. Such a combustion is known as an [[explosion]] or [[detonation]].
 ===Slow===
 Slow combustion is a form of combustion which takes place at low [[temperature]]s. [[Cellular respiration]] is an example of slow combustion.
-===Complete===
-In complete combustion, the reactant will burn in oxygen, producing a limited number of products. When a hydrocarbon burns in oxygen, the reaction will only yield [[carbon dioxide]] and water. When a hydrocarbon or any fuel burns in air, the combustion products will also include nitrogen. When elements such as carbon, nitrogen, [[sulfur]], and [[iron]] are burned, they will yield the most common oxides. Carbon will yield carbon dioxide. Nitrogen will yield [[nitrogen dioxide]]. Sulfur will yield [[sulfur dioxide]]. Iron will yield [[iron(III) oxide]]. It should be noted that complete combustion is almost impossible to achieve.  In reality, as actual combustion reactions come to [[Chemical equilibrium|equilibrium]], a wide variety of major and minor species will be present.  For example, the combustion of [[methane]] in air will yield, in addition to the major products of carbon dioxide and water, the minor product carbon monoxide and nitrogen oxides.
 ===Turbulent===
-Turbulent combustion is a combustion characterized by turbulent flows. It is the most used for industrial application (e.g. [[gas turbine]]s, [[diesel engine]]s, etc.) because the turbulence helps the mixing process between the fuel and oxidizer.
+Turbulent combustion is a combustion characterized by turbulent flows. It is used for industrial applications such as [[gas turbine]]s and [[diesel engine]]s because the turbulence helps to mix the fuel and oxidizer.
 ===Microgravity===
-Nearly every flame behaves differently in a [[Microgravity| microgravity environment]]. Microgravity  combustion research contributes to understanding of spacecraft fire safety and diverse aspects of combustion physics.
+Nearly every flame behaves differently in a [[Microgravity| microgravity environment]]. Microgravity  combustion research contributes to understanding of [[spacecraft]] fire safety and diverse aspects of combustion physics.
 ===Incomplete===
-Incomplete combustion occurs when there isn't enough oxygen to allow the fuel (usually a hydrocarbon) to react completely with the oxygen to produce carbon dioxide and water, also when the combustion is quenched by a heat sink such as a solid surface or flame trap. When a hydrocarbon burns in air, the reaction will yield carbon dioxide, water, carbon monoxide, pure carbon (soot or ash) and various other compounds such as nitrogen oxides.
+Incomplete combustion occurs when there isn't enough oxygen to allow the fuel (usually a hydrocarbon) to react completely with the oxygen to produce carbon dioxide and water or when the combustion is quenched by a heat sink such as a solid surface or a flame trap.
-The quality of combustion can be improved by the design of combustion devices, such as furnace [[burner]]s and [[internal combustion engine]]s. Further improvements are achievable by [[catalytic]] after-burning devices (such as [[catalytic converter]]s) or by the simple partial return of the exhaust gases into the combustion process. Such devices are required by [[environmental legislation]] for vehicles in most countries, and may be necessary in large combustion sources, such as [[thermal power plants]], to reach legal [[emission standard]]s.
+The quality of combustion can be improved by the design of combustion devices such as furnace [[burner]]s and [[internal combustion engine]]s. Further improvements are achievable by [[catalytic]] after-burning devices or by the simple partial return of the exhaust gases into the combustion process. Such devices are required by [[environmental legislation]] for vehicles in most countries, and may be necessary in large combustion sources, such as the [[Steam generator|steam generating furnaces]] in [[thermal power plants]], to reach legal [[emission standard]]s.
+{{Image|Smouldering.jpg|right|175px|Smouldering embers of a solid barbecue fuel.}}
 ===Smouldering===
+[[Smouldering]] is a flameless form of combustion. The fundamental difference between smouldering and flaming combustion is that in smouldering, the oxidation occurs on the surface of a solid fuel rather than in the gas phase. The characteristic [[temperature]] and [[heat]] released during smouldering are low compared to those in flaming combustion (i.e., ~ 600°C vs. ~&thinsp;1500°C). Smouldering propagates in a creeping fashion, around 0.1 mm/s, which is about ten times slower than flames spread over a solid. In spite of its weak combustion characteristics, smouldering is a significant fire hazard.
-[[Smoulder|Smouldering combustion]] is a flameless form of combustion, deriving its heat from heterogeneous reactions occurring on the surface of a solid fuel when heated in an ''oxidizing'' environment. The fundamental difference between smouldering and flaming combustion is that in smouldering, the oxidation of the reactant species occurs on the surface of the solid rather than in the gas phase. The characteristic temperature and heat released during smouldering are low compared to those in the flaming combustion of a solid. Typical values in smouldering are around 600 °C for the peak temperature and 5 kJ/g-O<sub>2</sub> for the heat released; typical values during flaming are around 1500 °C and 13 kJ/g-O<sub>2</sub> respectively. These characteristics cause smoulder to propagate at low velocities, typically around 0.1 mm/s, which is about two orders of magnitude lower than the velocity of flame spread over a solid. In spite of its weak combustion characteristics, smouldering is a significant fire hazard.
+==Combustion with other oxidants==
-==Combustion with other oxidants==
+Oxygen is usually assumed as the oxidant when talking about combustion, but other oxidants exist. [[Nitrous oxide]] (NO) is used in rockets and in race cars. [[Fluorine]] (F<sub>2</sub>), another oxidizing element, can produce a combustion reaction that yields fluorinated products rather than oxides. For example, mixtures of gaseous fluorine and methane are explosive. [[Chlorine trifluoride]] is a strong fluorinating agent that ignites fuels more readily than oxygen.
-Oxygen can be assumed as the oxidant when talking about combustion, but other oxidants exist. [[Nitrous oxide]] is used in rockets and in motorsport; it produces oxygen at over 1300 C. Fluorine, another oxidizing element, can produce a combustion reaction, to produce fluorinated products (rather than oxides). For example, mixtures of gaseous [[fluorine]] and [[methane]] are explosive, just like mixtures of oxygen and methane. [[Chlorine trifluoride]] is a strong fluorinating agent that ignites fuels more readily than oxygen.
-==Chemical equation==
+==Chemical equations==
 Generally, the [[chemical equation]] for [[Stoichiometry|stoichiometric]] burning of hydrocarbon in oxygen is as follows:
+:'''C<sub>x</sub>H<sub>y</sub> + (&thinsp;x + 0.25 y&thinsp;)&thinsp;O<sub>2</sub> → x&thinsp;CO<sub>2</sub> + (&thinsp;0.50 y&thinsp;)&thinsp;H<sub>2</sub>O'''
-:<math>C_xH_y + \left( x + \frac{y}{4} \right) O_2 \rightarrow \; xCO_2 + \left( \frac{y}{2} \right) H_2O</math>
 For example, the burning of [[propane]] is:
+:'''C<sub>3</sub>H<sub>8</sub> + 5&thinsp;O<sub>2</sub> → 3&thinsp;CO<sub>2</sub> + 4&thinsp;H<sub>2</sub>O
-:<math>C_3H_8 + 5O_2 \rightarrow \; 3CO_2 + 4H_2O</math>
 The simple word equation for the combustion of a hydrocarbon in oxygen is:
+:'''fuel + oxygen → carbon dioxide + water vapor
-:<math>\textrm{Fuel} + \textrm{Oxygen} \rightarrow \; \textrm{Heat} + \textrm{Water} + \textrm{Carbon\ dioxide}</math>
 If the combustion takes place using air as the oxygen source, the nitrogen can be added to the equation, although it does not react, to show the composition of the flue gas:
+:'''C<sub>x</sub>H<sub>y</sub> + (&thinsp;x + 0.25&thinsp;y&thinsp;)&thinsp;O<sub>2</sub> + 3.76&thinsp;(&thinsp;x + 0.25&thinsp;y&thinsp;)&thinsp;N<sub>2</sub> → x&thinsp;CO<sub>2</sub> + (&thinsp;0.50&thinsp;y&thinsp;)&thinsp;H<sub>2</sub>O + 3.76&thinsp;(&thinsp;x + 0.25&thinsp;y&thinsp;)&thinsp;N<sub>2</sub>'''
-:<math>C_xH_y +  \left( x+ \frac{y}{4} \right) O_2 + 3.76 \left( x+ \frac{y}{4} \right) N_2 \rightarrow \; xCO_2 +  \left( \frac{y}{2} \right) H_2O + 3.76 \left( x + \frac{y}{4} \right) N_2</math>
 For example, the burning of propane in air is:
+:'''C<sub>3</sub>H<sub>8</sub> + 5&thinsp;O<sub>2</sub> + 18.8&thinsp;N<sub>2</sub> → 3&thinsp;CO<sub>2</sub> + 4&thinsp;H<sub>2</sub>O + 18.8&thinsp;N<sub>2</sub>
-:<math>C_3H_8 + 5O_2 + 18.8N_2 \rightarrow \; 3CO_2 + 4H_2O + 18.8N_2</math>
+The simple word equation for the combustion of a hydrocarbon in air is:
-The simple word equation for the combustion of a hydrocarbon in air  is:
+:'''fuel + air → carbon dioxide + water + nitrogen
-:<math>\textrm{Fuel} + \textrm{Air} \rightarrow \; \textrm{Heat} + \textrm{Water} + \textrm{Carbon\ dioxide} + \textrm{Nitrogen}</math>
+Nitrogen may also oxidize when there is an excess of oxygen. The reaction is thermodynamically favored only at high temperatures. Diesel engines are run with an excess of oxygen to combust small particles that tend to form with only a stoichiometric amount of oxygen, necessarily producing nitrogen oxide emissions.
-Nitrogen may also oxidize when there is an excess of oxygen. The reaction is thermodynamically favored only at high temperatures. Diesel engines are run with an excess of oxygen to combust small particles that tend to form with only a stoichiometric amount of oxygen, necessarily producing nitrogen oxide emissions.
 ==Fuels==
@@ Line 91: / Line 77: @@
 ===Liquid fuels===
-Combustion of a liquid fuel in an oxidizing atmosphere actually happens in the gas phase. It is the vapour that burns, not the liquid. Therefore, a liquid will normally catch fire only above a certain temperature, its [[flash point]]. The flash point of a liquid fuel is the lowest temperature at which it can form an ignitable mix with air. It is also the minimum temperature at which there is enough evaporated fuel in the air to start combustion.
+Combustion of a liquid fuel in an oxidizing atmosphere actually happens in the gas phase. It is the vapour that burns, not the liquid. Therefore, a liquid will normally catch fire only above a certain temperature, its [[Flash point (science)|flash point]]. The flash point of a liquid fuel is the lowest temperature at which it can form an ignitable mix with air. It is also the minimum temperature at which there is enough evaporated fuel in the air to start combustion.
 ===Solid fuels===
@@ Line 97: / Line 83: @@
 The act of combustion consists of three relatively distinct but overlapping phases:
 * '''Preheating phase''', when the unburned fuel is heated up to its flash point and then [[fire point]]. Flammable gases start being evolved in a process similar to [[dry distillation]].
-* '''Distillation phase''' or '''gaseous phase''', when the mix of evolved flammable gases with oxygen is ignited. Energy is produced in the form of heat and light.   Flames are often visible. Heat transfer from the combustion to the solid maintains the evolution of flammable vapours.
+* '''Distillation phase''' or '''gaseous phase''', when the mix of evolved flammable gases with oxygen is ignited. Energy is produced in the form of heat and light.   Flames are often visible. Heat transfer from the combustion to the solid maintains the evolution of flammable vapors.
 * '''Charcoal phase''' or '''solid phase''', when the output of flammable gases from the material is too low for persistent presence of flame and the charred fuel does not burn rapidly anymore but just glows and later only smoulders.
-==Reaction mechanism==
+{| border="0" width="215" align="right" cellpadding="0" cellspacing="0" style="wrap=no"
+|
-Combustion in oxygen is a radical chain reaction where many distinct radical intermediates participate.
+{| class = "wikitable" align="right"
+|+ Adiabatic Flame Temperatures
-The high energy required for initiation is explained by the unusual structure of the [[dioxygen]] [[molecule]]. The lowest-energy configuration of the dioxygen molecule is a stable, relatively unreactive [[diradical]] in a [[triplet oxygen|triplet spin state]]. [[Bonding]] can be described with three bonding electron pairs and two antibonding [[electrons]], whose [[Spin (physics)|spin]]s are aligned, such that the molecule has nonzero total angular momentum. Most fuels, on the other hand, are in a singlet state, with paired spins and zero total angular momentum. Interaction between the two is quantum mechanically a "[[forbidden transition]]", i.e. possible with a very low probability. To initiate combustion, energy is required to force dioxygen into a spin-paired state, or [[singlet oxygen]]. This intermediate is extremely reactive. The energy is supplied as heat. The reaction produces heat, which keeps it going.
+!Gas!!Formula!!°C
+|-
-Combustion of hydrocarbons is thought to be initiated by the abstraction of a [[hydride radical]] (H) from the fuel to oxygen, to give a [[hydroperoxide radical]] (HOO). This reacts further to give [[hydroperoxide]]s, which break up to give [[hydroxyl]] radicals. There are a great variety of these processes that produce fuel radicals and oxidizing radicals. Oxidizing species include singlet oxygen, hydroperoxide, hydroxyl, monatomic oxygen, and hydroperoxyl (OH<sub>2</sub>). Such intermediates are short-lived and cannot be isolated. However, non-radical intermediates are stable and are produced in incomplete combustion. An example is [[acetaldehyde]] produced in the combustion of [[ethanol]]. An intermediate in the combustion of carbon and hydrocarbons, carbon monoxide, is of special importance because it is a [[Poison|poisonous gas]].
+|Hydrogen||H<sub>2</sub>||2,181
+|-
-Solid fuels also undergo a great number of [[pyrolysis]] reactions that give more easily oxidized, gaseous fuels. These reactions are [[endothermic]] and require constant energy input from the combustion reactions. A lack of oxygen or other poorly designed conditions result in these noxious and [[carcinogenic]] pyrolysis products being emitted as thick, black smoke.
+|Methane||CH<sub>4</sub>||2,014
+|-
-==Temperature==
+|Ethane||C<sub>2</sub>H<sub>6</sub>||2,063
+|-
+|Ethylene||C<sub>2</sub>H<sub>4</sub>||2,231
+|-
+|Propane||C<sub>3</sub>H<sub>8</sub>||2,076
+|-
+|Propylene||C<sub>3</sub>H<sub>6</sub>||2,171
+|-
+|Butane||C<sub>4</sub>H<sub>10</sub>||2,078
+|-
+|Pentane||C<sub>5</sub>H<sub>12</sub>||2,083
+|-
+|Hexane||C<sub>6</sub>H<sub>14</sub>||2,087
+|-
+|colspan=3|<span style="font-size:0.85em;">Notes:<br/>Gas temperature = 25 °C<br/>Combustion air temperature = 25 °C<br/>Air relative humidity = 60%<br/>Excess combustion air = 0 %</span>
+|}
+|}
+==Adiabatic flame temperature==
+Assuming complete combustion under [[adiabatic]] conditions (i.e., no heat loss or gain), the ''adiabatic flame temperature'' can be calculated. The calculation is based on the [[Laws of thermodynamics|first law of thermodynamics]] (i.e., the ''conservation of energy'') and on the fact that the [[heat of combustion]] is used entirely for heating the fuel, the combustion air or oxygen, and the combustion product gases.<ref name>{{cite book|author=Milton R.Beychok|title=[[Fundamentals of Stack Gas Dispersion]]|edition=4th Edition|publisher=author-published|year=2005|pages=pp. 173-177|id=ISBN 0-9644588-0-2}}</ref><ref>[http://myweb.ncku.edu.tw/~chuhsin/ppt/combustion%20principles%20and%20control/04-Flame%20Temperature.ppt Flame Temperature] Professor Hsin Chu, [[National Cheng Kung University]], [[Taiwan]]</ref>
-Assuming perfect combustion conditions, such as complete combustion under [[adiabatic]] conditions (i.e., no heat loss or gain), the adiabatic combustion temperature can be determined. The formula that yields this temperature is based on the [[first law of thermodynamics]] and takes note of the fact that the [[heat of combustion]] is used entirely for heating the fuel, the combustion air or oxygen, and the combustion product gases.
+In the case of fossil fuels burnt in air, the combustion temperature depends on:
+* the heat of combustion (also referred to as the ''heating value'')
-In the case of fossil fuels burnt in air, the combustion temperature depends on
-* the heat of combustion (also referred to as ''heating value'')
 * the stoichiometric [[air-fuel ratio]] <math>{\lambda}</math>
-* the [[specific heat capacity]] of fuel and air
+* the [[Specific heat|specific heat capacity]] of the fuel and the air
-* the air and fuel inlet temperatures
+* the air and fuel inlet temperatures, as well as the relative humidity of the air
-The adiabatic combustion temperature (also known as the ''[[adiabatic flame temperature]]'') increases for higher heating values and inlet air and fuel temperatures and for stoichiometric air ratios approaching one.
+The adiabatic flame temperature increases for higher heating values and for higher inlet air and fuel temperatures and for stoichiometric air-fuel ratios approaching one.
-Most commonly, the adiabatic combustion temperatures for coals are around 2200 °C ( for inlet air and fuel at ambient temperatures and for <math>\lambda = 1.0</math> ), around 2150 °C for oil and 2000 °C for natural gas.
+Most commonly, the approximate adiabatic flame temperatures for coals are 2200 °C, 2150 °C for [[fuel oil]]s and 2000 °C for [[natural gas]]es. The adjacent table lists some calculated adiabatic flame temperatures for hydrogen and for various hydrocarbon gases, all at the conditions stated in the notes at the bottom of the table.
 In industrial [[furnace|fired heaters]], [[power plant]] steam generators, and large [[gas turbine|gas-fired turbines]], the more common way of expressing the usage of more than the stoichiometric combustion air is ''percent excess combustion air''.  For example, excess combustion air of 15 percent means that 15 percent more than the required stoichiometric air is being used.
-==Instabilities==
+==References==
+{{reflist}}
-Combustion instabilities are typically violent pressure oscillations in a combustion chamber.  These pressure oscillations can be as high as 180 dB, and long term exposure to these cyclic pressure and thermal loads reduces the life of engine components.  In [[rocket]]s, such as the F1 used in the Saturn V program, instabilities led to massive damage of the combustion chamber and surrounding components. This problem was solved by re-designing the fuel injector.  In liquid [[jet engine]]s the droplet size and distribution can be used to attenuate the instabilities.  Combustion instabilities are a major concern in ground-based gas turbine engines because of NOx emissions. The tendency is to run lean, an equivalence ratio less than 1, to reduce the combustion temperature and thus reduce the NOx emissions; however, running the combustor lean makes it very susceptible to combustion instabilities.
+'''General:'''<br/>
+*{{cite book|author=Merle C. Potter and Craig W. Somerton|title=Schaum's Outline of Thermodynamics for Engineers|edition=2nd Edition|publisher=McGraw-Hill|year=2006|id=ISBN 0-07-146306-2}}<br/>
-The [[Rayleigh Criterion]] is the basis for analysis of thermoacoustic combustion instabilities and is evaluated using the Rayleigh Index over one cycle of instability.
+*{{cite book|author=Steven S. Zumdahl|title=Introductory Chemistry: A Foundation|edition=5th Edition|publisher=Brooks Cole|year=2003|id=ISBN 0-618-30499-1}}<br/>
+*{{cite book|author=Warren C. Strahle|title=An Introduction to Combustion|edition=1st Edition|Publisher=CRC Press|year=1993 |id=ISBN 2-88124-608-7}}[[Category:Suggestion Bot Tag]]
-:<math>G(x)=\frac{1}{T}\int_{T}q'(x,t)p'(x,t)dt</math>
-When the heat release oscillations are in phase with the pressure oscillations the Rayleigh Index is positive and the magnitude of the thermoacoustic instability increases.  Consecutively if the Rayleigh Index is negative then thermoacoustic damping occurs.  The Rayleigh Criterion implies that a thermoacoustic instability can be optimally controlled by having heat release oscillations 180 degrees out of phase with pressure oscillations at the same frequency.  This minimizes the Rayleigh Index.

Combustion: Difference between revisions

Latest revision as of 16:01, 30 July 2024

Contents

Types of combustion

Rapid

Slow

Turbulent

Microgravity

Incomplete

Smouldering

Combustion with other oxidants

Chemical equations

Fuels

Liquid fuels

Solid fuels

Adiabatic flame temperature

References

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Combustion: Difference between revisions

Latest revision as of 16:01, 30 July 2024

Types of combustion

Rapid

Slow

Turbulent

Microgravity

Incomplete

Smouldering

Combustion with other oxidants

Chemical equations

Fuels

Liquid fuels

Solid fuels

Adiabatic flame temperature

References

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