Chapter 2 First Law “The first law of thermodynamics is nothing more than the principle of the conservation of energy applied to phenomena involving the production or absorbtion of heat.” - Max Planck. In this discussion Q is heat and W is work and the bold d is used to indicate that the differential is inexact. (In class I will “bar” the “d” to distinguish it from an exact differential.) By modern convention, dQ is heat added “to” and 2.1 dW is work done “on”. The Internal Energy 2.1.1 2. Heat is the energy transfer in response to T differences. A better description would be that Q is the energy transfer which is not work. Begging the question? Not if we have a good definition of work. Components 1. Translational kinetic energy 2. Rotational kinetic energy 3. Vibrational kinetic and potential energy 4. Association energies (a) atom-atom (chemical energy) (b) nucleus - electron and electron-electron (c) nucleon(n/p)-nucleon (nuclear energy) Any associations that do not change (∆ = −) can be literally “swept under the rug” as whatever the association energy is for this sector, it does not change. For example, chemical reactions do not change the nuclei [all the nuclei on reactants (R) side are on the products (P) side], therefore we can neglect the “nucleon association” sector. 2.1.2 History Many contributed (Julius Robert Mayer, James Prescott Joule and Hermann von Helmholtz) [∼1842]. 2.1.3 Statement = d + d (2.1) 1. d = [] = d 22 3. Work is the means of energy transfer which changes the Hamiltonian (or boundary conditions) and whereby eigen solutions of the system. For example, consider a particle in a box. Push on the box and the energy levels move up and separate. If there is an Auf-bau and particles occupy levels up to some point, the energy clearly goes up due to the application of this “work”. The addition of heat is then a process by which the eigen solutions stay the same but the “particles” (on average) occupy higher energy levels. 2.4 4. Cases: (a) General: = d + d P = d − + ( F · x ) H P (b) Always: = = 0 As the internal energy is a state function, and has an exact differential, it has a unique value at any point in thermospace (specified values of the thermodynamic variables.) Heat Capacities 1. ≡ lim∆ →0 ( ∆ ) ≡ ( ) Definition 1 The symbol “” is used to indicate an experimental infinitesimal. 2. Heat capacities are defined for each phase. The input or output of heat during a phase change is not associated with a heat capacity. (c) No heat flow (adiabatic): ∆ = (d) No Work done: = d + d = or ∆ = Again, you should think of “no work done” as the same as fixing the levels. The work can take many forms, but for d to be non-zero there must be a change (motion) in the conjugate variable to the applied generalized force. X d = F · x (2.2) 3. Heat capacities are (within a phase) smooth functions of T [i.e. C(T)]. The functions are often expressed as polynomials as these functions are easy in integrate. (Now you know what is coming don’t you, see item below.) 4. Example of C for H2 O. Fig. Cp (H2 O) 2.2 Work P d = (“applied forces”)·(“displacement”) Examples Generalized “Force” Displacement dW Mechanical F [N= ] x [m] Fdx 2 Linear tension 1 [J/m] L -1 dL surface ten. 2 [J/m2 ] A -2 dA pressure p3 [Pa=J/m3 ] V [m3 ] -PdV gravitational mg [N] h [m] mgdh electromotive pot. [V] q-charge [Coul.] M-magnitization HdM magnetic H [Tesla= ] chemical [J/mole] n-quantity dn In trying to remember the signs, just appreciate that +ve work increases the energy of the system. 5. The heat required to transform ice into steam, from T= -10 C to T= 110 C at 1 bar is R0 = ( ) + + −10 R 100 R 110 ( ) + + 100 ( ) . 0 6. The heat capacity under constant volume is: ≡ ( ) = ( ) (2.3) 7. The heat capacity under constant pressure is: 2.3 Heat 1. Leads to altered population of QL (most often translational levels) 2. Energy transfer in response to a Temp. imbalance ≡ ( ) = ( ) (2.4) The enthalpy is defined to have this quality. 8. = + the work required to heat and expand the system against an external P [per mole·K]. 3. Energy transfer that is not work Exercise 2.3.1 Book example 2.2: Heat H2 O in an adiabatic enclosure → 24 Most of the energy goes into the vaporization of the water (association sector). Only 1.7 kJ into expansion. FOLLOW THE ENERGY! 23 (a) W [mole·K] = R = 8.13 [ ]. (b) W [mole·K] ∼ 0 for liquids and solids as dV ∼ 0 (“No movey, no worky!”) 2.5 State Functions Fig. Indicator diagram (See 2.12, pg 29.) For any state function R 1. ∆ = = − H 2. = 0 3. On the other hand, work and heat are not state functions and depend on path. R = − R = = − = − ∆ 2.8 Designer fxn Enthalpy H 1. Define ≡ + But this work (between these end points) is only one of an infinite number of possible values. R = d = value depends on the path R = d = value depends on the path ( ) is the result of a Legendre transformation on to swap out as an independent variable and replace it with = [ ] + ( ) = [ − ] + + 4. Consider loading a remote pallet onto a pickup truck with a hoist on the end of a swingable boom. = + Note the sign change of the “PV” term. Recall that = −( ) (a) drag the pallet to near the truck and then use the hoist to pick it almost straight up and onto truck. 2. (b) Pick the pallet up where it is, at the end of a boom, and rotate it into the truck. 1 = = d − + + = d + = 2.6 Reversibility [d + d ] + + = the heat transfer at constant P. This is “bench-top” chemistry. 3. Integrate to get: ∆ = Consider the two following changes in volume: 4. This justifies the previously stated result 1. Quasi static and reversible. The piston moves up slowly as the water evaporates. ≡ ( ) = ( ) 2. Sudden and irreversible - jank off the cup of water. 2.9 Fig. reversible vs irreversible 2.7 W dU vs dH Consider the internal energy and enthalpy differences between two stationary thermodynamic states. Labeling these states and we are asking for the difference in the heat required to convert a fixed amount of material from one equilibrium state at to another at The heat required is more in the constant pressure case as one must commit enough energy to push back the retaining walls. If one did not do this the pressure would (almost always) increase. W vs W 1. As = ( ) ⇒ ∆ = –—+–––+–––—+––—+–––-+–– W W 0 W W down the slide up the slide below above R ( ) = = 2. As = ( ) ⇒ ∆ = = = 24 ∆ R ( ) ∆ 3. = + ( ) = + Therefore the magnitudes of the heat transfer at constant and the heat transfer at constant required (to convert into ) are related via, ln = ( ) −1 = ( )−1 = ( ) 1∴0 5. As 1 and 0 and change in opposite directions, i.e. 4. Cases (a) Condensed Phases: ≈ as these phases have small coefficients of thermal expansion [ ≡ 1 ( ) ∼ 0] thus is very small. (b) When the # of moles of gas changes: ≈ +(∆) = − ln Remark 2 What is ? It is the energy required to heat one mole of an ideal gas by one degree. Later we will have fun with which is 0 little brother = Clearly between the three ( ) we only need two! History has saddled us with all three. (The truth is worse than that. If we decided to measure in energy units we could dump both and ) Remark 3 What are the units of the IGL? ENERGY. The ideal gas law says if you measure the internal energy content via the product or via the average kinetic energy per mole (times 2/3rds - see SM) you get the same answer. Adiabatic Expansion Compression of an IG and Under adiabatic (“no through passage”) conditions 1. = 0 ∴ = = − = − = − R R 3. = − 4. If C 6= ( ) = − ln (b) adiabatic expansions cool. ( ) ( ) = ( ) −1 = ( ) = ( ) = 0 Remark 1 I will use small letters (v, u, h, g, and s) to denote molar quantities. Heat capacities will always be molar so refers to the molar heat capacity with units of While I am on the subject, note that the entropy also has the units of = 8314[ ] 2. (a) adiabatic compressions heat and 6. Again assuming IG, (c) For isothermal processes (rxns) when the # of moles of gas is fixed and the gases are close to ideal, R R R = − = − = − ln = ln( ) = ln( )( − ) with ≡ = + 2.10 = ln 25 See Fig. 2.13, pg 35. isothermal compressions squeeze out heat expansions suck in heat adiabatic heat cool