First Law of Thermodynamics
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Transcript of First Law of Thermodynamics
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Essential UNIVERSITY PHYSICS, Volume 1 Richard Wolfson
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18.1 The First Law of Thermodynamics
First Law of Thermodynamics The change in the internal energy of asystem depends only on the net heat transferred to the system and thenet work done by the system, independent of the particular processesinvolved.
Mathematically, the first law is
U = Q - W
Change in Intenalenergy
Heat addedto thesystem
Work done by thesystem
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18.1 The First Law of Thermodynamics
Heat addedto thesystem
Work done bythe system
U U
U = (U-U) Change in internal energy
Q
Example: Heat a gas, it expands against a weight. Force (pressure times area) is applied over a distance, work is done.
U = Q - W
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18.1 The First Law of Thermodynamics
We are frequently concerned with rates of energy flow.
Differentiating the first law with respect to time gives a
statement about rates:
dU/dt is the rate of change of a systems internal energy.
dQ/dt is the rate of heat transfer to the system.
dW/dt is the rate at which the system does work.
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The First Law of Thermodynamics: Thermal PollutionEXAMPLE 18.1
The reactor in a nuclear power plant supplies energy at the rate of3.0 GW, boiling water to produce steam that turns a turbine-generator.The spent steam is then condensed through thermal contact with watertaken from a river. If the power plant produces electrical energy atthe rate of 1.0 GW, at what rate is heat transferred to the river?
The entire power plant is our system, comprising the nuclear reactor,including its fuel, and the turbine-generator.We identify U as the internal energy stored in the fuel, W as themechanical work that ends up as electrical energy, and Q as the heattransferred to the river.
We know that: dU/dt = dQ/dt dW/dt. The reactor extracts internalenergy from its fuel, so the rate dU/dt is negative; the power plantdelivers electrical energy to the outside world, so dW/dt is positive.We need to solve for dQ/dt.
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GIVEN: dU/dt = 3.0GW and dW/dt = 1.0 GW
-3.0 GW 1.0 GW
-3.0 GW + 1.0 GW
-2.0 GW
The First Law of Thermodynamics: Thermal PollutionEXAMPLE 18.1
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18.2 Thermodynamic Processes
Although the 1st law applies to any system, its easiest to understandwhen applied to an ideal gas. The ideal gas law relates thetemperature, pressure, and volume of a given gas sample:
pV = nRt
The thermodynamic state is completely determined by any two of thisquantities p, V, or T.
p,V,T
p,V,T
V
p
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18.2 Thermodynamic Processes
Reversible and Irreversible Processes
Water Gas
T T
Temperature control
These temperatures stay the same as the water temperature increasesslowly
If we raise thereservoirtemperature veryslowly, both thewater and gas temperatures willrise in unison, and the gas willremain in
equilibrium.
Quasi-staticprocessA system is alwaysin thermodynamicequilibrium.
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18.2 Thermodynamic Processes
Reversible and Irreversible Processes
Water Gas
T T
Temperature control
These temperatures stay the same as the water temperature increasesslowly
Reversible Process:
We could reverse this heatingprocess by slowlylowering thereservoirtemperatur; the gas would cool, reversing its pathin the pV diagram.
Irreversible Process:If we suddenlyplunging a cool gas sample into hotwater, then itbecomes and irreversible process.The system is notin equilibrium.
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18.2 Thermodynamic Processes
Work and Volume Changes
The work done by the system is related to the changes in pressure and volume:
(work done during volume change)
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18.2 Thermodynamic Processes
Isothermal Processes
An isothermal process occurs at constant temperature.
To find work, we relate pressure and volume through the ideal gas law: p = (nRT)/V. Then it becomes:
For an isothermal process, the temperature T is constant, giving
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18.2 Thermodynamic Processes
Isothermal Processes
The first law of thermodynamics then gives U = 0 = Q W, so
T = constant
Q = W
W = nRT*ln(V/V)
pV = constant
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18.2 Thermodynamic Processes
Constant-Volume Processes and Specific Heat
A constant-volume process occurs in a rigid closed container whosevolume cant change.To express U = Q in terms of a temperature change T, we introduce the molar specific heat at constant volume Cv defined by:
V
p
V = constant
Q = U
W = 0
Q = nCvT
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18.2 Thermodynamic Processes
Isobaric Processes and Specific HeatIsobaric means constant pressure. Processes occurring in systemsexposed to the atmosphere are essentially isoberic. The work done asthe volume changes from V to V, is the area under the isobar, or
W = p(V-V) = pV
(isobaric process)
Cp is the molar specific heat at constant pressure.
(molar specific heats)
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18.2 Thermodynamic Processes
Isobaric Processes and Specific Heat
p = constant
Q = U + W
W = p(V-V)
Q = nCpT
Cp = Cv + R
V
p
W
T
T
isobar
VV
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18.2 Thermodynamic Processes
Adiabatic Processes
In an adiabatic process, no heat flows between a system and itsenvironment. The way to achieve this is to surround the system withperfect thermal insulation.
Since the heat Q is zero in an adiabatic process, the 1st law becomessimply
U = -W (adiabatic process)
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18.2 Thermodynamic Processes
Adiabatic Processes
As a gas expands adiabatically, its volume increases while itsinternal energy and temperature decrease. The ideal-gas law,pV=nRT, then requires that the pressure decrease as well and bymore than it would in an isothermal process where T remainsconstant.
(adiabatic process)
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18.2 Thermodynamic Processes
Adiabatic Processes
Q = 0
U = -W
W = (pV-pV)/(-1)
pV = constant
TV(-1) = constant
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An Adiabatic Process: Diesel PowerEXAMPLE 18.3
Fuel ignites in a diesel engine from the heat of compression as thepiston moves toward the top of the cylinder; theres no spark plug asin a gasoline engine. Compression is fast enough that the process isessentially adiabatic. If the ignition temperature is 500C, WHATCOMPRESSION RATIO Vmax/Vmin is needed? Airs specific-heat ratio is=1.4, and before compression the air is at 20C.
The problem involves temperature and volume, we apply the formulaTminVmin(-1) = TmaxVmax(-1).
Solving for the compression ratio Vmax/Vmin gives
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18.3 Specific Heats of an Ideal Gas
The specific heats of an ideal gas follow from the degrees offreedom of each molecule:
Monatomic
3 degrees of freedom
Cv = (3/2)R
Diatomic
5 degrees of freedom
Cv = (5/2)R