Video summary
The video explores the concept of adiabatic flame temperature, focusing on combustion as one of the most significant types of reaction enthalpy. Combustion is essential for various daily processes such as cooking with natural gas or propane, generating energy, and powering vehicles like gasoline cars. While these different fuels—ranging from methane to octane—all undergo a similar chemical process where carbon converts to CO2 and hydrogen turns into water vapor when reacting with oxygen, the resulting flame temperatures vary significantly. To understand this variation, thermodynamics is used to calculate how much heat remains within the system after combustion occurs, specifically under adiabatic conditions where no heat escapes to the surroundings before heating up the reaction products.
To illustrate this calculation, the speaker uses methane as a simple example, noting that burning one mole of methane releases approximately 890 kJ of energy (a negative enthalpy change). In an idealized scenario where all released heat stays within the system, this energy is used entirely to raise the temperature of the products. The equation balances the total heat generated against the sum of the heats required to warm each product molecule: one mole of CO2 and two moles of H2O vapor. However, in real-world scenarios like burning natural gas on a stove, air provides the oxygen for combustion. Since air is roughly 78% nitrogen and only 21% oxygen, significant amounts of inert nitrogen diffuse into the flame alongside the necessary oxygen. Consequently, this large quantity of nitrogen must also be heated up by the reaction's energy output, which acts as an additional thermal load that lowers the final temperature compared to a pure oxygen environment.
By plugging in average heat capacity values for CO2, water vapor, and nitrogen over the high-temperature range typical of flames, the video demonstrates how to solve for the resulting temperature increase. For methane burning in air, this calculation yields an approximate rise of 2300 Kelvin from room temperature, leading to a final flame temperature around 2600 K or roughly 2300°C. The speaker highlights several factors influencing these results: flames burn hotter in pure oxygen because the energy isn't wasted heating nitrogen; different fuels produce different temperatures due to their unique stoichiometry and carbon-to-hydrogen ratios; and while assuming constant heat capacities simplifies the math, a more accurate approach would involve integrating variable heat capacities over temperature. Ultimately, this thermodynamic procedure allows for reasonable estimates of how hot various fuels will burn under specific conditions like air versus pure oxygen environments.
Read the full video transcript
[Music]
all right so among all the different
flavors or types of uh enthalpies
reaction enthalpies that we've seen uh
one of the most important is the
enthalpy of combustion so combustion of
course is a process that's important for
a lot of different processes we use
combustion uh to cook with we use it to
generate a lot of our energy we use it
in many cases to drive uh our cars so
combustion as a process is very
important and we can use thermodynamics
to understand the details of combustion
at a slightly deeper level in particular
we can learn using what we know about
thermodynamics uh to understand the
temperature at which Flames burn when uh
combustion takes place so to illustrate
what I mean by that and why that's an
interesting question you're familiar
most likely with uh burning a number of
different types of fuels you might burn
um you know if you if you cook on a gas
stove the natural gas is is mostly
methane if you use a bunson burner in a
chemistry lab those most likely are
burning
propane uh if you uh weld with an
acetylene torch then you're burning
acetylene if you drive a gasoline
powered car you're using a mix of
hydrocarbons that might be uh include
some octane for example but a range of
different hydrocarbons we can burn all
of those those combustion in every one
of those cases we combine those with
oxygen the carbon turns into CO2 the
hydrogen turns into steam or water so
combustion is the same chemical process
in each of those cases just the
stochiometry of the reaction works out
to be different and yet the Flames the
temperature at which these burn the
temperature of the Flames that are
generated when uh these different
hydrocarbons uh combust in a flame turn
out to be very different so so uh to
understand why that would be
true let's take the the simplest of
these as an example just to keep the
stochiometry relatively easy for the
first example if we
burn methane so again maybe we're
cooking on a gas stove and burning
natural gas or or uh primarily methane
if we burn methane and
oxygen this will generate
CO2 and H2O
uh if I burn one mole of methane one
carbon becomes one carbon so I've got
one mole of CO2 uh four hydrogens need
two molecules of
water or two moles of water so I've got
a total of 2 plus two is four oxygen so
that means two o2 molecules on the
reactant side of the reaction so there's
my balanced reaction that's the
combustion reaction for methane the
enthalpy of
combustion for methane so the enthalpy
change associated with that reaction eny
of combustion for methane
isus
89.3 K per mole a number we can get by
looking it up in a table or by
calculating it from the Heats of
formation of products minus reactants or
by doing in the lab and measuring the
the enthalpy In a calorimetry experiment
we can get that number a number of of
different ways that's the enthalpy
change for this combustion
reaction that's enough information that
plus one additional assumption I'll
mention in a minute is enough to let us
calculate the temperature at which
methane will burn uh so that assumption
let's say let me draw a picture of
what's going on in so I'll draw a flame
which I've drawn as a as a candle but
any in any of these examples if I'm
burning methane I've got some source of
methane my natural gas line on my stove
or whatever the oxygen that's required
to burn the methane that's just in the
air so methane and oxygen both enter
this flame and then this chemical
reaction takes place the thing I need to
um understand about the the flame what I
eventually use this flame for if I'm
burning methane on my stove I'm going to
use it to heat a pot of water or
whatever it is I'm cooking so there's
some heat that's going to get
transferred to something else at some
point that process is relatively slow
the the process of getting the heat from
the flame to something else takes a
significant amount of of time what's
going to happen very quickly when this
reaction liberates some heat so this
enthalpy changes negative which means
the enthalpy of the products is less
than the enthalpy of the
reactants so if I just do this
reaction uh it has a negative enthalpy
change so that would normally generate
heat that gets given off to the
environment and that's what heats my pot
of
water that process like I've said is
relatively slow the first place that
heat goes that energy in the form of
enthalpy goes is to heating up the
products of the reaction themselves so
the first thing that gets heated up is
the CO2 and the
H2O so uh in fact those atoms that make
up the molecules of CO2 and H2O those
are the same atoms that started in my
methane and O2 so it's the same um atoms
that were there originally so in that
sense the heat has not left the system
and we can
assume at least under some conditions if
the reaction is fast enough that the
reaction is adiabatic
meaning that the heat in the reaction uh
no heat was transferred to the
surroundings in the reaction all of the
energy stayed within all of the enthalpy
stayed within the system which means
that the enthalpy change of the products
that energy was used to heat up the
products and at least initially didn't
transfer to anything outside of those
individual uh atoms or molecules so if
we do this process at constant pressure
if it's open to the environment
we know that heat and enthalpy change
are the same thing at constant pressure
that's why we Define the enthalpy is to
be able to make statements like this one
so if we do this at constant pressure
enthalpy and heat are both equal to zero
for this tic process so the thing that's
zero the enthalpy that's equal to zero
is the full enthalpy change for the
reaction not
just the enthalpy of combustion not that
just the enthalpy change when the mo
when the reactants get converted to
products but
also the enthalpy change that occurs
when these products are heated up so the
way physically to understand what's
going on is I generate 890 kles every
time I burn a mole of methane and then I
spend all 890 KJ of that energy in
heating up the CO2 and H2O to a much
higher temperature than where they
started that's why a flame Burns hot is
because that energy is used to heat up
the products so in this thermodynamic
equation the total enthalpy is the
enthalpy change of the reaction heat of
combustion plus since I've got a mole of
CO2 the if my ANL be if I'm sorry if my
heat capacity is constant which is a big
assumption we'll come back to that
statement in just a second second but as
a um an initial guess if I say CO2 has
some heat capacity the total enthalpy
change of the CO2 is its heat capacity
times uh the change in temperature so
for each mole of CO2 I have I've got one
mole participating in this reaction I've
got heat capacity times delta T if I've
raised the temperature by some amount
delta T I've also got two moles of H2O
so I also need to include twice the heat
capacity of water vapor
times the same increase in temperature
the whole system all of the products are
going to be heated to the same
temperature of this flame so this delta
T and this delta T are the same number
I've I've raised the temperature of the
CO2 and the H2O by the same amount so if
I rearrange this equation what I'm
interested in I know that en of
combustion I know I can look up the uh
heat capacity of CO2 and H2O what I
don't know is is the amount by which
this reaction will have increased the
temperature of the products so I want to
solve for delta T so let's rearrange
this equation first and
say move the um enthalpy of combustion
over the other side negative enthalpy of
combustion is equal to these heat
capacities so and heat capacity of CO2
and heat capacity of
H2O twice
and all times delta
T then if I want to solve for delta T
that's going to
be negative eny of combustion divided by
my heat
capacities so these are numbers that I
can look up and plug in to calculate the
temperature change we're going to do
that in just a
second and this would be exactly how to
proceed with the calculation if the
chemical reaction occurred as I've drawn
it if we're burning methane in
oxygen and of course we are there's
oxygen in the air that's the uh oxygen
that's used in this combustion reaction
but of course air is composed not just
of oxygen but also of
nitrogen nitrogen doesn't participate in
the chemical reaction so normally we
would avoid it when avoid thinking about
it when talking about the chemistry of
this reaction but once we start talking
about the fact that the enthalpy gets
transferred to the products uh and and
heats them up it's unavoidable that if
oxygen diffuses into this flame nitrogen
is diffusing Into The Flame as well so
uh in the immediate environment of the
flame uh which is at several thousand
degrees I've not only heating up the CO2
and H2O that I generate by burning the
methane but I'm also going to need to
heat up the nitrogen as well so for a
more accurate um estimate of the flame
temperature in air we're going to need
to include the the effects of the
nitrogen as well so remembering that air
is 21 Parts oxygen so the O2 to N2 ratio
is 21 Parts oxygen for every 78 Parts
nitrogen and the other 1% is is argon
and other Trace uh components so I need
to know that ratio because for every two
moles of oxygen that I need to diffuse
into the flame and burn uh with the
methane or help burn the methane I'm
going to have so for every two
moles of
o2 there's 21 parts of o2 in air that
ratio needs to be the same as 78 parts
of N2 in the air so some number of moles
of of N2 so roughly not exactly roughly
four times as much N2 as O2 in the air
if I work this ratio out it turns out to
be that in instead of two moles of
oxygen this will work out to
be 7.4 moles of nitrogen are the
stochiometric amount uh to the two moles
of oxygen so if I go back and say the
things I need to heat up in this flame
include not only one mole of CO2 and two
moles of H2O every time I burn a mole of
methane but I'm also going to need to
heat up 7 7.4
moles of
N2 so again in this parentheses I've got
7.4 times the heat capacity of N2 and
also in the denominator of this fraction
I've got 7.4
times the heat capacity of N2 so that's
accounting for the fact that I need to
heat up the N2 that's a passive
participant in this reaction just
because it's in the same vicinity as the
oxygen so now we're in a position where
we'll get a reasonable answer if we plug
the numbers into this expression we know
that enthalpy of
combustion 89.3 kles per
mole let's pay attention to the units so
that's 890 with a negative sign becomes
positive in the
numerator heat capacities of CO2 and H2O
and N2 the heat capacities I'm going to
need to use there are not the heat
capacities at room temperature but the
average heat capacity over the range of
temperatures so this temperature
increase is going to be on the order of
thousands of degrees Flames are are
relatively hot so we need the average
heat capacity over the range from room
temperature up to the temperature of the
flame so I'll just let you know what
those numbers
are a reasonable number to use for the
average heat capacity of of CO2 between
room temperature and Flame temperature
is about 55 Jew per mole
Kelvin for water it's about
42 and for nitrogen it's about 33 Jew
per mole
Kelvin so a few things to notice about
that as we've seen heat capacities are
larger for these triatomic molecules
than for diatomic molecules for reasons
um related to the equip partition
theorem um
also um yeah that's enough information
about the heat capacity so if we plug
these numbers
in notice that the units Jews per mole
Kelvin in the denominator I've got kles
per mole in the numerator so to keep the
unit straight let's
multiply the enthalpy of combustion by a
th000 so that we've got units of Jews
per mole that'll cancel the units of
Jewel per mole in the
denominator and what we
get when we do that math 890,000
300 divided by the quantity 55 + 2 * 42
+ 33 when I do that math with a couple
of
sigfigs oops that's not correct one step
ahead of myself
that number works out to be
2300
Kelvin is the increase in temperature so
what that tells us is when I burn
methane whatever the initial temperature
was the temperature is going to increase
by 2300 Kelvin so the actual flame
temperature if I start out near room
temperature that's where my 2600 kvin
comes from so start out near room
temperature increase the temperature by
2300 and I find out that the the
temperature of this
flame is going to be around 2600
Kelvin so or 2300 Celsius roughly if you
prefer so a few comments about that
number that that's a reasonable estimate
in purely ideal conditions so the notes
I'll make will be this calculation
is for having made the assumption that
this flame burns adiabatically the heat
generated in this reaction immediately
goes to raise the temperature of the
products and the nitrogen in the air
before any of it gets transferred to
other things like um the the pot that's
sitting on the flame and things like
that so it's under relatively ideal tic
conditions if the the reaction is not
completely adiabetic
then uh the temperature increase will be
less so uh
so if it's
nonadiabatic a
diabetic the flame temperature will will
decrease another thing to notice is that
we've done this calculation for Burning
uh methane in air a 21 to 78 mixture of
oxygen and nitrogen uh the calculation
would be different if I were burning in
pure oxygen if you take the effort to
burn a flame in pure oxygen rather than
oxygen with nitrogen then the flame
temperature will be different and you
can just leave out the
nitrogen to do
that so in oxygen I'll point out that
the flame temperature will be
considerably higher in oxygen because we
don't have to go to the effort of the
thermodynamic effort of heating up the
N2 I'll also point out that with the
same type of
calculation we've done the ex Le for
methane we could do it for propane we
could do it for acetylene the only
difference in those cases is the
stochiometry of this reaction works out
differently we combine it with a
different number of moles of oxygen
which bring with them a different number
of moles of N2 and we generate a
stochiometrically different number of
moles of CO2 and H2O so every molecule
every fuel Burns at a different flame
temperature because the ratio of carbons
to hydrogens is different in that
particular fuel so the stochiometry of
the reaction is a little bit different
and then
lastly I'll remind us
that we used a constant just a single
number for the heat capacity assuming
that the heat capacity was a relatively
constant number between room temperature
and this flame temperature which is
certainly not true or assuming that this
average heat capacity is a reasonably
good estimate in fact we know that the
heat capacity depends on the temperature
sometimes relatively strongly at these
high temperatures so the more accurate
way of doing the calculation if we want
just a couple more than just a couple of
sigfigs worth of uh accuracy out of this
flame temperature would be to treat the
the dependence of the heat capacity on
the temperature so in other words
instead of saying heat capacity times
delt T we would replace this with
something like an integral of the heat
capacity over the temperature from some
initial to some final temperature that
makes the math of doing the calculation
quite a bit more calc
complicated but of course it gives you a
much better uh more accurate estimate
for the flame temperature but this uh
overall procedure depending on whether
you want to burn uh your fuel in oxygen
or in air what your fuel is how
accurately you want to treat the heat
capacities can give you uh a pretty good
estimate of the temperature at which
different fuels will burn