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2
Introductory remarks:
work to heat:- no tax heat to work:- tax
work and heat are not forms of energy:- they are names for methods of transferring energy
Heat is not a noun! (nor an adjective)Heat converted to work means that energy was transferred
from a source by heating and then transferred by doing work.{To avoid circumlocutions we will often, in fact, use heat as a noun or an adjective!}We often wish to know how one quantity varies with a variation in another quantity under certain conditions. Tabulations are available for certain of these variations that are easily measurable. We can then often derive expressions for other variations that are not tabulated in terms of these tabulated quantities.
3
Heat CapacityWe consider a situation in which there is no change of phase. The heat capacity is defined as: C = (đQ /dT)
This is not a derivative of Q with respect to T as Q cannot be written as a function of T. (Misleading?)
The heat capacity is extensive. The intensive equivalent is called the specific heat capacity
c = đQ/(mdT) heat capacity per unit mass.c = đQ/(ndT) heat capacity per mole.
Since đQ depends upon the process, c is not specified until the process is specified. For a given dT, đQ could be +, - or 0.
4
Some minor comments:
Heat capacity is a misnomer because “heat’ is not “contained” in a body. It should be called an energy capacity.
When reference is made to a specific heat, keep in mind that it can be /mole or /kilomole or /mass or /volume.
5
The most common specific heats are for constant pressure and for constant volume.
cv =( đQ/ndT)v c at constant V
cp = (đQ/ndT)p c at constant P
cp is usually measured as cv is difficult experimentally.
There are many relationships between thermodynamic quantifies which can be obtained by combining the definitions, laws and rules for partial derivatives. Here we will consider P,V,T systems (hydrostatic systems),
but there are similar relationships for other systems.
In a P,V,T system certain quantities are readily measured directly: P,V,T, volume expansivity β, and the isothermal compressibility κ.
6
Let us take T and V as independent variables.
VTU
VdTQ
V
TVU
VTU
TVU
VTU
C
)3(dVPdTQ
)2(VddTdU
)1(VPddUQ
VV T
UC
đ
đ
Cv can be determined
experimentally
This equation is true for any reversible process
If one has a model of a substance one can calculate from this model and compare with the experimentally
determined CV.
VT
U
đ
7
Let us consider Cp:
Equation (3): dVPV
UdT
T
UQ
TV
đ
At constant pressure:
PTVP T
VP
V
U
T
U
dT
Q
đ
VPV
UCC
T
VP
P
V
CC
V
U VP
T
This is an example of an equation that relates the quantity on the left, which is usually not measured, to state functions which can be measured and are often tabulated.If we have a model of a substance, we can calculate the quantity on the left and compare the result with the experimentally determined quantities on the right hand side.
8
EXAMPLE: Chapter 4The molar specific heat capacity of most substances (except at very low temperatures) can be satisfactorily expressed by the empirical formula 22 cTbTacP
(a) Find the heat required to raise the temperature of n moles of the substance at constant pressure from 21 TtoT
(b) Determine the specific heat capacity for Mg at 300K given
)(1027.313.3107.25 83
Kkmole
Jinccba P
(a) dTT
cbT2aqdTcq
dT
qc
2
1
T
T
2PP
12
21
2212
11)()(
TTcTTbTTaq
12
21
2212
11)()(
TTcTTbTTanQ
đ đ
9
(b)
28
23
)300(1
1027.3)300()13.3(2107.25Kkmole
KJK
Kkmole
J
Kkmole
JcP
Kkmole
JcP
41039.2 Mg at 300K
10
EXAMPLE: Chapter 4From figure 4.1 (textbook) estimate the energy to heat one gram of Cu from 300K to 600K:(a) At constant volume(b) At constant pressure(c) Determine the change in internal energy of the Cu in each case.
(a) Constant V )constantV(dTncQdT
Q
n
1c V
V
V
For the specific heat take the midpoint (450K) Kkmole
JcV
31025
đ
kmolenkmolekg
kgnamuM 5
3
1057.1/5.63
105.63
)300(/
10251057.1
)(
35
0
KKkmole
JkmoleQ
TTncQdTncdQ ifV
T
T
V
Q f
i
Q=118J
constant V
đ
11
(b) Constant PKkmole
JcP
31026
)constantP(dTncQdT
Q
n
1c P
P
P
)300(10261057.1)( 35 KKkmole
JkmoleTTncQ ifP
Q=122J constant P
(c) At constant volume W=0 so JUQU 118
For constant P
)constantP(VdTdVT
V
V
1dVPW
P
V
V
f
i
f
i
f
i
f
i
V
V
T
T
T
T
TVVdTVVdTdV
Look up values for Cu 3315 1092.8102.5m
kgK
constant V
đđ
12
3733
3
1012.1/1092.8
10mV
mkg
kgmV
V
m
393715 1075.1)300(1012.1102.5 mVKmKTVV
JWmPaW 4395 1077.1)1075.1)(1001.1(
JUJJWQU 1221077.1122 4
constant P
(d) When heat enters a system at constant V, all the energy goes into increasing the internal energy. When heat enters at constant pressure, some of the energy is expended in doing work against the surroundings and there is a smaller temperature rise.
VP
P
P
V
V CCT
QC
T
QC
smaller
13
Free (Joule) expansion of a real gas. (System isolated)
In this process Q=0, W=0 so U=constant. Does T change during this process? The Joule coefficient is introduced. Is it zero?
UV
T
This coefficient is extremely difficult to measure directly, so indirect methods are used to answer the question.Considering U=U(T,P):
dPP
UdT
T
UdU
TP
If, in a free expansion, dT=0 and since dU=0 then 0
TP
U
Experiments by Rossini and Framdsen found that 0)(
TfP
U
T
Hence, for real gases, in a Joule expansion. 0dT
14
Ideal Gas:We now refine our definition of an ideal gas as one that satisfies the relationship PV=nRT and U=U(T) only. For a quasi-static process of a hydrostatic system: đQ=dU+PdVWe have and since, for an ideal gas, U=U(T) only,
this gives so (ideal gas)
V
V T
UC
dT
dUCV PdVdTCQ V
Using the equation of state: PdV+VdP=nRdT and so
)1(VdPnRdTdTCQ V Dividing by dT and considering processes at constant P,
nRCCornRCdT
QVPV
P
(Mayer’s Equation)
Substituting into (1) gives (ideal gas)VdPdTCQ P đ
đ
đ
đ
15
Continuing with an ideal gas:
Starting with U(T,V) dVV
UdT
T
UdU
TV
dT
dV
V
U
T
U
dT
dU
TV
PTVP T
V
V
U
T
U
T
U
But, for an ideal gas (only!), 0V
U
T
VVP
CT
U
T
U
Hence, for an ideal gas (only!) we can write irrespective of the process under consideration dT
dUCV
16
We introduce a very useful ratio:
V
P
c
c
Although the molar specific heats vary somewhat with temperature, at temperatures not too far from ordinary temperatures, experimental results give:
Monatomic gases:
Diatomic gases :
67.125
soRcP
40.127
soRcP
For a phase change:VaporLiquidSolid
System gives off heat
System absorbs heat
17
We are now ready to introduce the concept of enthalpy and I would like to provide a reason for doing so.
It is not always convenient, and may even be dangerous, to carry out a process at constant volume. (This is particularly true in chemistry!) It is often preferable to carry out experiments at constant pressure (perhaps atmospheric). For these latter processes, the concept of enthalpy is useful.
As an example consider a liquid at its BP in a cylinder and the piston is held in place by atmospheric pressure. Now consider energy supplied to vaporize the liquid, the pressure remaining atmospheric. The result will be an increase in the volume and an increase in internal energy. But to achieve this transformation we must supply not only the internal energy increase, but also the energy required for the gas to push the piston and since the pressure is constant ΔW=PΔV and so the energy that must be supplied is
ΔU+PΔV and we then write ΔU+PΔV =ΔH
18
The quantity H is called the enthalpy.
Even absent the piston this energy must be supplied as the atmosphere must be pushed aside.
Such a situation is very common in chemical processes.Hence there exist extensive tabulations of ΔH.
19
Enthalpy and heats of transformation:
Isobaric processes often occur, such as in a change of phase (isothermal and isobaric). Keeping track of the work can be annoying.We can sidestep this problem by considering the enthalpy, rather than the energy in these processes. In a phase change )vv(PW 12 From the first law: vPdqddu Consider a finite change and introduce , the latent heat of transformation per kilomole.
q
)Pvu()Pvu(or)vv(P)uu( 11221212
We introduce the specific enthalpy h=u+Pv
Hence 12 hh
We now consider the possible phase changes. Notation:1=solid 2=liquid 3=vapor
1 prime(′) =solid 2 primes(″)=liquid 3 primes(′′′)=vapor
is the heat involved in a phase change
(for a kilomole)
20
We can now write, in terms of this notation:hh 12hh 23hh 13
solid liquid (fusion)liquid vapor (vaporization)
solid vapor (sublimation)
h is a state function! Hence 0dh
We consider a small cycle that encloses the triple point. (see next slide)We assume that the circle is so small that the enthalpy changes appreciably only during a change of phase. The cycle is
solid vapor liquid solid
solid vapor (heat flows in) vapor liquid (heat flows out) liquid solid (heat flows out)
131 h23322 h12213 h
1223133210 hhhdh
This gives 231213 (all positive quantities)
22
The enthalpy of a system is then H=U+PVIf we could annihilate the system we could, in principle, not only extract the energy, but also the work done (PV) by the atmosphere as it fills in the vacuum left when the system disappears.
For an isobaric process dH=dU+PdVand the enthalpy can increase for two reasons:
• the energy of the system increases• the system expands
23
Relationships involving enthalpy:Pdvduq
vdPPdvdudhPvuh Hence vdPdhq
But we can write dPP
hdT
T
hdh)P,T(hh
TP
dPvP
hdT
T
hq
TP
Now for P constant dTT
hq
P
P
P
PP T
hcso
T
h
dT
q
Vc Pc is an “energy capacity”, while is an “enthalpy capacity”
đ
đ
đ
đ
đ
24
It should be mentioned that there does not have to be any heat involved as energy or enthalpy can be changed by other means, such as in a microwave oven.
In first order phase transitions (melting, boiling, sublimation)the change in enthalpy is called “latent heat”. This term is used because there is no change in temperature.
Extensive tables of enthalpy changes exist. For example we can find that the change in enthalpy when 1 mole of water at 1 atmosphere and 373K is converted to steam is 40,660J. Since a mole is about 18 grams the change in enthalpy per kilogram is 2.26MJ/kg, which is the latent heat of vaporization of water. Not all of the energy ends up in the vapor. Some work must be performed to push the atmosphere away.
Neglecting the volume of the liquid and treating the vapor as ideal and for 1 mole of water, PVvapor= RT
PVvapor= (8.31J/K)(373K)=3100J
This is about 8% of the 40,660J
25
Note on enthalpy and review:As a result of the Joule-Thomson experiment (discussed later), it can be shown that, for an ideal gas: 0
TP
H
PdVdTCQsodT
dUCgasidealPdVdUQ VV
Consider H=H(T,P) dPP
HdT
T
HdH
TP
=0 for an ideal gas
Hence dTCdHCT
H
dT
dHdT
T
HdH PP
PP
VdPPdVPdVQVdPPdVdUdHPVUH
VdPdTCQVdPQdTC PP (ideal gas)
We will soon use these two expressions for an ideal gas.
đ đ
đ
đ đ
26
For an ideal gas f
i
P
f
i
P dTCdHdTCdH
f
i
Pif dTCHH for all processes involving an ideal gas
u h
reversible process vdPqdhPdvqdu
PP
VV T
hc
T
uc
ideal gas vdPdTcqPdvdTcq PV
0P
h0
V
u
TT
f
i
Pif
f
i
Vif dTchhdTcuu
đđ
đđ
27
Quasi-static adiabatic processes (ideal gas):
We had vdPdTcqandPdvdTcq PV
In an adiabatic process q=0 and so, upon division of the two equations, we obtain
v
dv
P
dP
For modest temperature changes, is constant, and upon integrating we obtain:
constantPv (adiabatic)
This is for an ideal gas!
đ đ
đ
28
Example: Adiabatic expansion of an ideal gas. (The hard way.)?,, UVPVP ffii
f
i
f
i
V
V
ii
V
V
iiV
dVVPWPVVPPdVW
111
111
11
1
if
ii
V
V
iiVV
VP
VVPW
f
i
)1(11
111
1
11
1
f
iii
if
iii
V
VVP
VV
VVPW
To find ratio of volumes )2(fi
if
f
i
TP
TP
V
VnRTPV
i
f
f
i
f
i
f
i
f
i
f
i
i
fffii T
T
V
Vor
T
T
V
V
V
Vinso
V
V
P
PVPVP
1
)2(
29
Placing this in (1)
][1
11
11 if
i
fi
i
fii TTnR
WT
TnRT
T
TVPW
Since the gas is ideal
VVVVVP CnR
CCCnRnRCC
1
)1(
][ ifV TTCW ][ ifV TTCUWWQU
or, since for an ideal gas U=U(T) only dT
dUCV
][ ifVV TTCUdTCdU
(The first approach was just to show how much fun algebra can be and to practice some techniques.)
30
EXAMPLE:
Q
000 ,,, TVPn 000 ,,, TVPn
0827, Pn
LTn, RT
Ideal gas5.1
adiabatic piston adiabatic walls
A cylinder with thermally insulated walls contains a moveable frictionless thermally insulated piston. On each side of the piston are n moles of an ideal gas. The initial state variables are the same on both sides. By means of a heating coil in the gas on the left side, heat is slowly supplied. The gas on the left expands and compresses the gas on the right hand side until its pressure has increased toIn terms of determine: (a) How much work is done on the gas on the right side.(b) The final temperature of the gas on the right side.(c) The final temperature of the gas on the left side.(d) How much heat flows into the gas on the left side.
0)8/27( P0,, Tcn V
31
(a) On the right side no heat enters so we have an adiabatic compression.
0
/1
R0RR000 V27
8VV
27
8VVP
8
27VPconstantPV
000
3/2
914
94
278
VVsoVVVV LRR
3/23/2
8
27
8
2700027
808
271
nR
VPVP
nRRT
RnRT
RVRP
WUWQUTTTT RR
00
3/1
23
827
Ideal gas so dTncdTCdU VV
0000 21
21
23
TncWTncTTncU VVV
(b) From above 023TTR
32
(c)
OLLLLLL VPnR
TnRTVPVVPP914
8271
914
827
000
025.5 TTL
(d) For the left side the gas expands so, from part (a) 02
1TncW VL
000 25.4)125.5()( TncUTncTTncU VLVLVL
00 5.025.4 TncTncWUQWQU VVLLLLLL
075.4 TncQ VL
33
Example: Problem 4-4
Consider u=u(T,P) dPP
udT
T
udu
TP
dT
dP
P
u
T
u
dT
du
TP
VTPV T
P
P
u
T
u
T
u
)1(VTP
V T
P
P
u
T
uc
1P
v
v
TPV
T
T
P
v-
v
PvTv
T
P
VT
P
In equation (1) )2(
TPV P
u
T
uc
?
34
From problem 4-3: vPcT
uP
P
In equation (2)
TPV P
uPcc
v
TVP P
uPcc
vT
VP P
uPcc
v)(
)(-v VPT
ccPP
u
Hence we have shown that this partial can be calculated in terms of easily measurable or tabulated quantities.
{To derive, start with definition of cP and use h=u+Pv}
35
Recapitulation:The key concept is that adiabatic work is independent of path.U=internal energy function or adiabatic work function.
Q and W are methods for changing the internal energyW=mechanical method of energy transferQ=non-mechanical method of energy transfer
When the transfer is over, heat and work are no longer useful or meaningful.
Heat is not a noun! It is wrong to make a statement such as “the ocean holds a lot of heat.”Using heat as a verb can be confusing:
to heat : add energy to or raise the temperature of
36
Avoid using the term “thermal energy”. This is obscure or ambiguous. Sometimes it is used to mean “heat” and at other timesinternal energy. Often it is not clear what is meant.
Consider the adiabatic compression of a gas. It is often said that there is no flow of thermal energy into the gas, but then we are told that the “thermal energy” has increased.
In Chapter 2 we introduced the work PdvWIn Chapter 3 we introduced the 1st Law Pdvduq In this Chapter we introduced the specific heat (often tabulated)which permits us to now calculate đq and so du can be obtained.
The specific heat is a very important property of systems andso extensive tabulations exist and much theoretical work has also been done. It will be considered throughout the course.
đ
đ
37
For an adiabatic process undergone by an ideal gas,
constantPv
Along the way, we introduced another state variable, the enthalpy.This is very convenient when the pressure is held constant and also processes involving a change of phase. h=u+Pv
Also, for any reversible process, VV T
UC
For an ideal gas, we added the condition that U=U(T) only!
38
Comments on a thin wire.
The linear expansivity α and Young’s Modulus Y are introduced.Young’s Modulus is always positive.The linear expansivity is almost always positive. (The few exceptions include rubber.)
In an assignment, you showed:
dYA
1dL
L
1dT
If there is no change in the tension, a slight increase in L will result in an increase of T. On the other hand, if the length is held fixed and the tension increases, T will decrease. If both the length and tension change, the T change can be positive or negative.