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Phys 160 Thermodynamics and Statistical Physics Lecture 4 Isothermal and Adiabatic Work Heat Capacities

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  • Phys 160 Thermodynamics and Statistical

    Physics

    Lecture 4 Isothermal and Adiabatic Work

    Heat Capacities

  • Heat and Work Much of thermodynamics deals with three closely -related concepts; temperature, energy, and heat.

    • Temperature, fundamentally, is a measure of an object's tendency to spontaneously give up energy. • Energy is the most fundamental

    dynamical concept in all of physics

  • • For this reason, how to express energy in terms of anything more fundamental?

    • We can only state what we know definitely. The law of conservation of energy.

    • There are many ways to put energy into a system or taken out.

  • • In Thermodynamics, we classify these mechanisms as Heat and Work

    • Heat is defined as spontaneous flow of energy from one object to another due to difference in temperature. • Work is defined as any other

    transfer of energy into or out of a system.

  • • Usually with work an agent is involved in putting in energy; it is not spontaneous

    • Both heat and work refers to energy in transit; there is no heat or work in a system. Heat enters a system; work is done on a system. .

  • • Define symbols: • U for the total energy inside a

    system.

    • Q and W represent the energy that enters and leave the system as heat and work. Q + W is the total energy that enters the system

    • By the conservation law, • U = Q + W . U is the change in energy.

  • • Can we say similarly change in Q and W? Q and W are infinitesimal quantities.

    • This statement U = Q + W is what is know as the first law of thermodynamics

    • The SI unit for energy is the Joule kg.m2/s2. Traditional unit is calorie. 1 cal = 4.186 J.

  • • Compression Work –important type of work done on a system (gas)

    • W = F. dr = F x =P.A. x (volume change should be very slow-quasistatic)

  • • Why negative sign in front of PdV?

    • The work done here is positive but the dV is negative, compression

    • Hence W = -PdV

  • • isothermal

    • For the isothermal (limits Vi to Vf) • W = - PdV =-NkT V/V

    • = NkT ln (Vi/Vf)

    • The work done here is positive.

  • • Because it is isothermal, heat must flow out of the system. How much? How to calculate?

    • From energy conservation, Q = U – W = (NfkT/2) – W There is no change in U; hence U = 0 and Q = 0 – W = NkTln(Vf/Vi) • The heat input here is just the

    negative of work done. expansion

  • • Because it is isothermal, heat must flow out of the system. How much? How to calculate?

    • From energy conservation, Q = U – W = (NfkT/2) – W There is no change in U; hence U = 0 and Q = 0 – W = NkTln(Vf/Vi) • The heat input here is just the

    negative of work done. expansion

  • • For isothermal compression, Q is nega-tive since heat leaves the gas. For iso-thermal expansion, Q is positive since heat enters the system. • Adiabatic Compression. We will assume

    quasistatic process, but no heat is allow-ed to escape. For this U = Q + W =W;

    • T will increase. • The curve in the PV diagram must con-

    nect a lower T isotherm with one of higher T, its slope higher than either.

  • • What is the shape of this curve?

    • From equipartition theorem • U =(f/2) NkT. Then the energy change

    along any infinitesimal segment of the curve is dU = (f/2)N k dT = - P dV

    • This differential equation relates dT to dV. To solve the equation use the ideal gas equation P = NkT/V to eliminate P

  • • The solution to this equation is (f/2) (dT/T) = - ( dV/V) Integrating (f/2) ln (Tf/Ti) = -ln (Vf /Vi)

    • Exponentiating we have • Vf Tf

    f/2 = ViTi f/2 = V T

    f/2 • Squaring we have V2 T

    f = constant. Eliminating T using PV = T* constant, we have V2 (PV)f =constant. Taking the fth root, P V (f+2)/f = constant = PV where is called the adiabatic exponent.

  • • An ideal gas is made to undergo the cyclic process as in Fig. For each step A, B and C: (a) Find the work done on the gas (b) the change in the energy content of the gas (c) the heat added to the gas. What does this process accomplish.

  • Phys 160 Thermodynamics and Statistical

    Physics

    Lecture 4 Isothermal and Adiabatic Work

    Heat Capacities

  • Heat and Work Much of thermodynamics deals with three closely -related concepts; temperature, energy, and heat.

    • Temperature, fundamentally, is a measure of an object's tendency to spontaneously give up energy. • Energy is the most fundamental

    dynamical concept in all of physics

  • • For this reason, how to express energy in terms of anything more fundamental?

    • We can only state what we know definitely. The law of conservation of energy.

    • There are many ways to put energy into a system or taken out.

  • • In Thermodynamics, we classify these mechanisms as Heat and Work

    • Heat is defined as spontaneous flow of energy from one object to another due to difference in temperature. • Work is defined as any other

    transfer of energy into or out of a system.

  • • Usually with work an agent is involved in putting in energy; it is not spontaneous

    • Both heat and work refers to energy in transit; there is no heat or work in a system. Heat enters a system; work is done on a system. .

  • • Define symbols: • U for the total energy inside a

    system.

    • Q and W represent the energy that enters and leave the system as heat and work. Q + W is the total energy that enters the system

    • By the conservation law, • U = Q + W . U is the change in energy.

  • • Can we say similarly change in Q and W? Q and W are infinitesimal quantities.

    • This statement U = Q + W is what is know as the first law of thermodynamics

    • The SI unit for energy is the Joule kg.m2/s2. Traditional unit is calorie. 1 cal = 4.186 J.

  • • Compression Work –important type of work done on a system (gas)

    • W = F. dr = F x =P.A. x (volume change should be very slow-quasistatic)

  • • Why negative sign in front of PdV?

    • The work done here is positive but the dV is negative, compression

    • Hence W = -PdV

  • • isothermal

    • For the isothermal (limits Vi to Vf) • W = - PdV =-NkT V/V

    • = NkT ln (Vi/Vf)

    • The work done here is positive.

  • • Because it is isothermal, heat must flow out of the system. How much? How to calculate?

    • From energy conservation, Q = U – W = (NfkT/2) – W There is no change in U; hence U = 0 and Q = 0 – W = NkTln(Vf/Vi) • The heat input here is just the

    negative of work done. expansion

  • • Because it is isothermal, heat must flow out of the system. How much? How to calculate?

    • From energy conservation, Q = U – W = (NfkT/2) – W There is no change in U; hence U = 0 and Q = 0 – W = NkTln(Vf/Vi) • The heat input here is just the

    negative of work done. expansion

  • • For isothermal compression, Q is nega-tive since heat leaves the gas. For iso-thermal expansion, Q is positive since heat enters the system. • Adiabatic Compression. We will assume

    quasistatic process, but no heat is allow-ed to escape. For this U = Q + W =W;

    • T will increase. • The curve in the PV diagram must con-

    nect a lower T isotherm with one of higher T, its slope higher than either.

  • • What is the shape of this curve?

    • From equipartition theorem • U =(f/2) NkT. Then the energy change

    along any infinitesimal segment of the curve is dU = (f/2)N k dT = - P dV

    • This differential equation relates dT to dV. To solve the equation use the ideal gas equation P = NkT/V to eliminate P

  • • The solution to this equation is (f/2) (dT/T) = - ( dV/V) Integrating (f/2) ln (Tf/Ti) = -ln (Vf /Vi)

    • Exponentiating we have • Vf Tf

    f/2 = ViTi f/2 = V T

    f/2 • Squaring we have V2 T

    f = constant. Eliminating T using PV = T* constant, we have V2 (PV)f =constant. Taking the fth root, P V (f+2)/f = constant = PV where is called the adiabatic exponent.

  • • An ideal gas is made to undergo the cyclic process as in Fig. For each step A, B and C: (a) Find the work done on the gas (b) the change in the energy content of the gas (c) the heat added to the gas. What does this process accomplish.