1) The document discusses different types of thermodynamic processes including reversible, irreversible, isobaric, isochoric, isothermal, and adiabatic processes.
2) It provides examples of an ideal gas cycle consisting of isobaric, isochoric, and isothermal processes and calculates the work, internal energy change, heat, and efficiency for each process.
3) The heat capacities of ideal monoatomic and diatomic gases are derived from their internal energy changes, showing the relationship between heat capacity at constant volume and constant pressure.
Types of processes
Reversible
•must be slow (quasistatic: system has time to go to
equilibrium after each change)
• system is in equilibrium at all points along the process
• corresponds to a line in pV diagram
• can be run in reverse
eg: He balloon shrink in liquid N and expands.
Irreversible
• often fast (but not always)
• is not a line in pV diagram (you can only mark initial and
final states)
• cannot run in reverse
DEMO:
eg. explosion
Reversible and
irreversible
processes
3.
Basic thermodynamic processes
•Isobaric: Constant p
W = p ∆V
• Isochoric: Constant V
W =0
• Isothermal: Constant T
∆U = 0 for ideal gases
• Adiabatic: No heat exchange
Q =0
• An infinite number of other processes without any special
name!
4.
Example: Ideal gascycle
An ideal monoatomic gas is trapped in a cylindrical container whose
cap is a piston of negligible mass that can slide up and down the
cylinder. The gas is initially at room temperature (298K) and
occupies a volume of 1.0 m3. The piston is in its equilibrium position.
(1) A mild heat source is then applied at the base of the container, and
the gas is then slowly warmed up to 350K while the piston moves up
to allow the gas to expand. Once the new temperature is reached,
the volume of the gas is 2.0 m3. Isobaric expansion
(2) The piston is locked in the new position and the gas is allowed to
cool down to room temperature. Isochoric cooling
(3) Finally, when room temperature is reached, the piston is pushed
back manually but very slowly, so that the gas is allowed to remain
in thermal equilibrium with the air in the room at all times. At the
end, the piston is back in its initial position. Isothermal compression
p
1
A
1 atm
Work foreach process:
B
2
350 K
3
pC
C
278 K
2.0 m3
1.0 m3
(
V
)(
)
W1 = pA (VB −VA ) = 1.01 × 105 Pa 1.0 m3 = 1.0 × 105 J
W2 = 0
VA
W3 = ∫ pdV
VC
=
VA
∫
VC
n from state A: n =
VA
nRTA
dV = nRTA ln
VC
V
nRT
Ideal gas: p =
V
(
pAVA
RTA
V
= pAVA ln A
VC
)(
)
= 1.01 × 105 Pa 1.0 m3 ln
Wcycle = W1 +W2 +W3 = 3.1 × 10 4 J
1
= −7.0 × 10 4 J
2
7.
p
1
A
1 atm
Change ininternal energy
for each process:
B
350 K
2
3
pC
C
1.0 m3
∆U1 =
278 K
V
2.0 m3
3
3
T −T
nRTB − nRTA = 3 pAVA B A = 3.9 × 10 4 J
2
2
2
TA
n from state A: n =
∆U2 =
3
3
nRTC − nRTB = −∆U1
2
2
∆U3 = 0 (isothermal)
∆Ucycle = 0
pAVA
RTA
since TC =TA
8.
p
1 atm
1
A
2
pC
Heat foreach process:
B
350 K
3
C
1.0 m3
2.0 m3
278 K
V
Q1 = ∆U1 +W1 = 1.4 × 105 J
Q2 = ∆U2 +W2= −3.9 × 10 4 J
Q3 = ∆U3 +W3 = −7.0 × 10 4 J
Qcycle = Q1 + Q2 + Q3 = 3.1 × 10 4 J
( =W
cycle
good!
)
9.
Heat capacities
Take anyprocess with a change in temperature, find heat Q. Their
relation is the definition of heat capacity!
Process at constant
volume:
dQ = nCV dT
p
V
Process at constant pressure:
p
dQ = nC P dT
V
p
Process X!
dQ = nC X dT
V
10.
Heat capacities (idealgas)
Process at constant
volume:
dU = dQ = nCV dT
W =0
Process at constant pressure: dW = pdV
dU = dQ − dW
= nC P dT − pdV
= nC P dT − nRdT
pV = nRT
pdV = nRdT
But: For the same change in
temperature, the change in
internal energy must be the
same!
nCV dT = nC P dT − nRdT
C P = CV + R
Also, good news: we can use dU = nCV dT for any process!
11.
Ratio of heatcapacities
Ideal gas:
Monoatomic
3
J
R = 12.47
2
mol K
5
J
C P = CV + R = R = 20.78
2
mol K
CV =
Diatomic
J
CV = 5R / 2 = 20.78
mol K
7
J
C P = CV + R = R = 29.09
2
mol K
CP
γ =
CV
5
CP 2 R 5
γ =
=
= = 1.67
CV
3
3
R
2
7
R
CP
7
γ =
= 2 = = 1.4
CV
5
5
R
2
ACT: Different heatingprocesses
Two containers have each 1 mole of monoatomic ideal gas inside. Heat
is transferred into both, causing a 50°C rise in temperature. For
container A, this happens at constant volume. For container B, this
happens at constant pressure. Which of the following is correct?
A. More heat is transferred into sample A
B. More heat is transferred into sample B
C. Both samples absorb the same heat.
QA = nCv ∆T
QB = nC P ∆T
C P = Cv + R > Cv
QA < QB
How much more?
J
QB − QA = n C p − Cv ∆T = nR ∆T = ( 1 mole ) 8.31
÷( 50 K ) = 415 J
mol K
(
)
14.
Compression Stroke ofEngines
If piston and cylinder are
thermally insulated, no heat is
transferred during compression,
Q = 0 (adiabatic process)
In this stroke of an engine
• Gas is compressed → it does
negative work
• Internal energy increases
• Temperature increases
15.
Adiabatic Gas Expansion
Pistonis insulated so that, as gas expands, Q = 0
∆U = Q −W = −
W
with W > 0 (expansion), so ΔU < 0
ΔT < 0
Temperature
decrease
16.
Adiabatic curve forideal gases: T and V
If Q = 0, dU = −dW
nCV dT = − pdV
nRT
nCV dT = −
dV
V
dT
R dV
=−
=0
T
CV V
R C P − CV
=
= γ −1
CV
CV
dT
dV
= − ( γ − 1)
=0
T
V
lnT + ( γ − 1 ) lnV = constant
TV γ −1 = constant
γ −1 > 0
DEMO:
Adiabatic
compression
For expansion, T decreases
For compression, T increases
17.
Adiabatic curve forideal gases: p and V
TV γ −1 = constant
pV γ −1
V
= constant
nR
pV γ = constant
18.
Work in adiabaticprocesses
If Q = 0, W = −∆U
W = −nCV ∆T
W = −nCV ∆T = −nCV
∆ ( pV
W =−
nR
)
∆ ( pV
γ −1
=−
)
∆ ( pV
γ −1
)