Midterm 1 : 1st Law of Thermodynamics

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14 Terms

1
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Distinguish between intensive and extensive properties. Distinguish between open, isolated and closed systems.

Thermodynamic vocabulary

  • System: the portion of the universe under study. Surroundings: everything else. Together they make the universe.

  • The boundary (real or imaginary) determines what can cross between system and surroundings.

Intensive vs. extensive properties

  • Extensive property: depends on the amount of matter (extent) present. If you double the sample, the value doubles.

    • Examples: mass (mm), volume (VV), moles (nn), energy (EE), enthalpy (HH), entropy (SS), Gibbs energy (GG), heat capacity (CC), length, weight.

  • Intensive property: independent of the amount present. Mnemonic: INTensive = INDependent.

    • Examples: temperature (TT), pressure (PP), density (ρ=m/V\rho = m/V), voltage (VV = J/C), color, hardness, luster, odor, melting/boiling/freezing point, conductivity, malleability, ductility, specific heat (csc_s), molar heat capacity (cmolarc_{molar}).

  • Shortcut rule: the ratio of two extensive properties is intensive. ρ=m/V\rho = m/V, cs=C/mc_s = C/m, and cmolar=C/nc_{molar} = C/n all follow this rule. Doubling the sample doubles both numerator and denominator, so the ratio is unchanged.

  • Molecular meaning:

    • Temperature measures average kinetic energy per particle, so it does not scale with NN.

    • Total energy sums over all particles, so it scales with NN.

  • Common pitfalls:

    • Weight vs. mass: both are extensive (weight depends on amount and gravity).

    • Concentration is intensive, but amount of solute is extensive. This matters for heterogeneous equilibria later: the “concentration” of a pure solid is constant regardless of how much solid is present.

    • Thermodynamic functions of the form ΔH\Delta H, ΔE\Delta E and ΔG\Delta G for a reaction are extensive: doubling the balanced equation doubles ΔH\Delta H. This is why 2 C2H2+5 O22\,\text{C}_2\text{H}_2 + 5\,\text{O}_2 gives twice the ΔH\Delta H of C2H2+52O2\text{C}_2\text{H}_2 + \tfrac52\text{O}_2.

Classifying systems by what crosses the boundary

System

Matter exchange

Energy exchange (heat/work)

Example

Open

Yes

Yes

Living plant, gasoline burning in a car engine, open beaker of boiling water

Closed

No

Yes

Coolant in a refrigerator coil, mercury in a thermometer, sealed flask in a water bath

Isolated

No

No

Ideal thermos of coffee, the universe

  • Pitfall: “closed” does not mean fully sealed from energy. It is closed to matter only. The fully sealed case is isolated.

  • The bomb calorimeter is treated as isolated: the sample burns inside a rigid sealed steel bomb (constant VV, no matter exchange), and the insulated water jacket is assumed to prevent heat leaving. Strictly, heat flows from the bomb to the water inside the calorimeter, which is why we measure it.

  • Related process labels (a constraint on a process, not on the system type):

    • Isothermal: ΔT=0\Delta T = 0

    • Isobaric: ΔP=0\Delta P = 0

    • Isochoric: ΔV=0\Delta V = 0

    • Adiabatic: q=0q = 0

Worked classification (from your slide exercise)

  1. Coffee in a very-high-quality thermos → isolated (no matter or energy exchange, ideal case).

  2. Coolant in refrigerator coil → closed (sealed fluid, but it absorbs and releases heat and is worked on by the compressor).

  3. Benzene burned in bomb calorimeter → isolated (sealed, insulated).

  4. Gasoline burning in an automobile engine → open (fuel and air in, exhaust out, heat and work out).

  5. Mercury in thermometer → closed (mercury cannot escape, but it exchanges heat).

  6. A living plant → open (takes in CO₂, H₂O, light; releases O₂, water vapor).


2
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Applying E=32RTE = \tfrac32 RT to isothermal changes.

Where the equation comes from

  • For 1 mole of an ideal monatomic gas (He, Ne, Ar, Kr), the only energy is translational kinetic energy. There are 3 translational degrees of freedom (x,y,zx, y, z), each carrying 12kT\tfrac12 kT per atom (12RT\tfrac12 RT per mole). This is the equipartition theorem.

    • E=3×12RT=32RTE = 3 \times \tfrac12 RT = \tfrac32 RT (J/mol), where R=8.314 J K−1mol−1R = 8.314\ \text{J K}^{-1}\text{mol}^{-1} and TT is in kelvin.

  • Key assumptions (the ideal gas model):

    • Particles have no intermolecular attractions or repulsions, so there is no potential energy contribution.

    • Particles are point masses, so there is no rotation or vibration (true for monatomic gases at ordinary temperatures).

    • Electronic excitation is negligible.

Consequence: EE depends only on temperature

  • ΔE=32R ΔT\Delta E = \tfrac32 R\,\Delta T (per mole), or ΔE=32nR ΔT\Delta E = \tfrac32 nR\,\Delta T for nn moles. The 32\tfrac32 and RR are constants, so they factor out of the Δ\Delta.

  • Isothermal process: ΔT=0\Delta T = 0, therefore ΔE=0\Delta E = 0.

    • Molecular picture: if the average kinetic energy per particle does not change and there are no interparticle forces, the total energy cannot change. Compression or expansion changes how much space the particles have, not how fast they move.

  • Since EE is a state function, ΔE=0\Delta E = 0 for any path between two states at the same TT, whether sudden or gradual, one step or many.

Pitfalls and edge cases

  • ΔE=0\Delta E = 0 for an isothermal process is exact only for ideal gases. For real gases, liquids and solids, EE also depends on volume (through intermolecular forces).

  • Phase changes are isothermal but ΔE≠0\Delta E \neq 0. Melting or boiling absorbs heat at constant TT because that energy goes into potential energy (breaking intermolecular attractions), not kinetic energy.

  • ΔE=0\Delta E = 0 does not mean q=0q = 0 or w=0w = 0. Both can be nonzero, but they must cancel (see Card 4).

  • For polyatomic ideal gases, EE is larger (52RT\tfrac52RT or 3RT3RT, see Card 12), but it still depends only on TT, so isothermal ΔE=0\Delta E = 0 still holds.

Worked example
Q: How much does the internal energy change when 2.00 mol of He is heated from 300 K to 400 K? What if the same gas is compressed isothermally at 300 K?

  1. Heating: ΔE=32nR ΔT=32(2.00 mol)(8.314 J K−1mol−1)(100 K)\Delta E = \tfrac32 nR\,\Delta T = \tfrac32 (2.00\ \text{mol})(8.314\ \text{J K}^{-1}\text{mol}^{-1})(100\ \text{K})

  2. Units: mol × J K⁻¹ mol⁻¹ × K = J

  3. ΔE=2494 J≈\Delta E = 2494\ \text{J} \approx +2.49 kJ

  4. Isothermal compression: ΔT=0⇒\Delta T = 0 \Rightarrow ΔE=0\Delta E = 0


3
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First law of thermodynamics (in words and in equation form).

Statement in words

  • Energy cannot be created or destroyed; it can only be converted from one form to another or transferred. The energy of the universe is constant.

  • For a closed system, the change in internal energy equals the heat added to it plus the work done on it.

Equation

  • ΔE=q+w\Delta E = q + w

    • ΔE\Delta E = change in internal energy of the system (J), the total of all kinetic and potential energy of the particles. It is a state function.

    • qq = heat transferred across the boundary (J), driven by a temperature difference. It is a path function.

    • ww = work done on or by the system (J). It is a path function.

  • Sign convention (system’s point of view): ++ means energy enters the system, −- means energy leaves (see Card 4).

Conceptual background

  • Heat is not a substance (the old “caloric” theory is wrong). It is a mechanism of energy transfer driven by a temperature gradient, flowing hot → cold until thermal equilibrium.

  • Joule’s experiment (1840s): a falling weight turned a paddle wheel in water, and the water warmed without contact with any hotter body. This showed mechanical work converts to heat. 1 cal = 4.184 J (mechanical equivalent of heat).

  • Analogy to other “potential” differences:

    • Electrical current flows with a difference in electrical potential.

    • Heat flows with a difference in temperature.

    • Chemical reactions proceed with a difference in chemical potential (ΔG\Delta G).

Why EE is a state function but qq and ww are not

  • State function: depends only on the current state (P, V, T, n), not on how it was reached. Examples: E,H,S,G,P,V,TE, H, S, G, P, V, T.

  • Path function: depends on the route. Only the sum q+wq + w is path-independent.

  • Analogy: the elevation difference between two towns is fixed, but the distance walked depends on the road.

Pitfalls

  • Writing Δq\Delta q or Δw\Delta w: these are not changes in state functions, so write qq and ww.

  • Using the opposite sign convention. Some textbooks define ww as work done by the system, giving ΔE=q−w\Delta E = q - w. Your course uses ΔE=q+w\Delta E = q + w.

  • The first law says nothing about direction or spontaneity. That requires the second law.

Worked example
*Q: A system’s internal energy increases by 80 J while 50 J of work is done on it. What is qq?*

  1. ΔE=q+w⇒80 J=q+50 J\Delta E = q + w \Rightarrow 80\ \text{J} = q + 50\ \text{J}

  2. q=80−50=q = 80 - 50 = +30 J

  3. The positive sign means 30 J of heat flowed into the system.


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Application of the first law to isothermal conditions and sign convention for heat and work.

Sign convention (system’s perspective)

  • q>0q > 0: heat flows into the system (endothermic).

  • q<0q < 0: heat flows out of the system (exothermic).

  • w>0w > 0: work done on the system (e.g., compression, ΔV<0\Delta V < 0).

  • w<0w < 0: work done by the system on the surroundings (e.g., expansion, ΔV>0\Delta V > 0).

  • Mnemonic: think of a bank account. Whatever enters the system is ++.

Isothermal ideal-gas process

  1. For an ideal gas, E=32RTE = \tfrac32RT (monatomic), so ΔE=32R ΔT\Delta E = \tfrac32R\,\Delta T.

  2. Isothermal: ΔT=0⇒ΔE=0\Delta T = 0 \Rightarrow \Delta E = 0.

  3. First law: ΔE=q+w⇒0=q+w\Delta E = q + w \Rightarrow 0 = q + w.

  4. Therefore q=−wq = -w.

Interpretation in words

  • Heat absorbed by the system equals work done by the system on the surroundings. (And vice versa for compression.)

  • Expansion (w<0w<0): the gas does work and would cool, but heat flows in from the surroundings (q>0q>0) to keep TT constant.

  • Compression (w>0w>0): work is put in, and the same amount of energy leaves as heat (q<0q<0) so TT stays constant.

  • Molecular picture: during expansion, molecules colliding with a receding piston lose kinetic energy. The thermal reservoir resupplies it.

Pitfalls

  • q=−wq = -w holds only when ΔE=0\Delta E = 0 (isothermal ideal gas). In general, ΔE≠0\Delta E \neq 0.

  • Isothermal does not mean no heat flow. Isothermal means constant TT. No heat flow is adiabatic.

  • qq and ww depend on the path (reversible vs. irreversible) even though q=−wq = -w always holds on each path.

Worked example (from your slides): bicycle pump
*Q: Air is compressed in a pump of inner diameter 3.0 cm, depressed 20. cm against 2.00 atm. Find ww and its sign.*

  1. w=−PextΔVw = -P_{ext}\Delta V, and ΔV=−(πr2⋅ℓ)\Delta V = -(\pi r^2 \cdot \ell) (volume decreases).

  2. r=1.5 cmr = 1.5\ \text{cm}, so V=π(1.5)2(20.) cm3=141 cm3=0.141 LV = \pi(1.5)^2(20.)\ \text{cm}^3 = 141\ \text{cm}^3 = 0.141\ \text{L} (using 1 L=1000 cm31\ \text{L} = 1000\ \text{cm}^3).

  3. w=−(2.00 atm)(−0.141 L)=w = -(2.00\ \text{atm})(-0.141\ \text{L}) = +0.28 atm·L

  4. In joules: 0.283 atm⋅L×101.3 J/(atm⋅L)≈0.283\ \text{atm·L} \times 101.3\ \text{J/(atm·L)} \approx +28.7 J

  5. Positive: work is done on the air.


5
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Derivation of work for irreversible and reversible expansions.

Step 1: general expression for pressure-volume work

  • Work = force × distance. For a gas pushing a piston of area AA against an external force FextF_{ext} through a displacement dzdz:

    • dw=−Fext dzdw = -F_{ext}\,dz (minus sign: the system expands against a force, so it loses energy).

  • Pressure = force/area, so Fext=PextAF_{ext} = P_{ext}A:

    • dw=−PextA dzdw = -P_{ext}A\,dz

  • Area × distance = volume: dV=A dzdV = A\,dz

    • dw=−Pext dVdw = -P_{ext}\,dV

  • Integrate:

    • w=−∫ViVfPext dVw = -\displaystyle\int_{V_i}^{V_f} P_{ext}\,dV (i)

  • Note: the work depends on PextP_{ext}, the pressure the surroundings exert. This is not necessarily the pressure of the gas.

Step 2: irreversible (sudden) expansion at constant PextP_{ext}

  • PextP_{ext} is constant, so it comes out of the integral:

    • wirr=−Pext(Vf−Vi)=−Pext ΔVw_{irr} = -P_{ext}(V_f - V_i) = -P_{ext}\,\Delta V

  • Variables: PextP_{ext} (Pa, atm or bar), ΔV\Delta V (m³ or L).

  • Units: Pa·m³ = J. With atm and L, 1 L·atm = 101.325 J (equivalently 8.314/0.08206=101.38.314/0.08206 = 101.3).

  • This is “irreversible” because the system is not in equilibrium during the process (gas pressure > PextP_{ext} throughout expansion).

Step 3: reversible (gradual) isothermal expansion of an ideal gas

  • Reversible means infinitely slow change in which the system is always in equilibrium with its surroundings: Pext=PsysP_{ext} = P_{sys} at every instant.

  • Substitute into (i) and use PV=nRTPV = nRT, so P=nRT/VP = nRT/V:

    • w=−∫ViVfnRTV dVw = -\displaystyle\int_{V_i}^{V_f}\frac{nRT}{V}\,dV

  • nn, RR and TT are constant (isothermal), so pull them out:

    • w=−nRT∫ViVf1V dVw = -nRT\displaystyle\int_{V_i}^{V_f}\frac{1}{V}\,dV

  • Use ∫1xdx=ln⁡x\int \frac1x dx = \ln x:

    • w=−nRT [ln⁡V]ViVf=−nRT(ln⁡Vf−ln⁡Vi)w = -nRT\,[\ln V]_{V_i}^{V_f} = -nRT(\ln V_f - \ln V_i)

  • Use ln⁡A−ln⁡B=ln⁡(A/B)\ln A - \ln B = \ln(A/B):

    • wrev=−nRTln⁡VfViw_{rev} = -nRT\ln\dfrac{V_f}{V_i}

  • Since PiVi=PfVfP_iV_i = P_fV_f for an isothermal ideal gas, this can also be written wrev=−nRTln⁡PiPfw_{rev} = -nRT\ln\dfrac{P_i}{P_f}.

Corresponding heat

  • For an isothermal ideal gas, q=−wq = -w, so qrev=nRTln⁡VfViq_{rev} = nRT\ln\dfrac{V_f}{V_i} and qirr=+PextΔVq_{irr} = +P_{ext}\Delta V. Heat is also path-dependent.

  • Dividing by TT gives ΔS=qrev/T=nRln⁡(Vf/Vi)\Delta S = q_{rev}/T = nR\ln(V_f/V_i), the macroscopic entropy definition, which is a state function.

Assumptions and pitfalls

  • The reversible formula requires an ideal gas and constant TT.

  • Reversibility is a theoretical limit. No real expansion is truly reversible, but it defines the maximum work.

  • Sign check: expansion has Vf>ViV_f > V_i, so ln⁡(Vf/Vi)>0\ln(V_f/V_i) > 0 and w<0w < 0. Compression gives w>0w > 0.

  • Do not use w=−PΔVw = -P\Delta V with the gas pressure unless the process is irreversible.

Worked example (from your slides)
*Q: 1.00 mol ideal gas at 298 K expands isothermally from 1.00 m³ to 11.0 m³. Find ww for (a) one-step irreversible expansion against the final pressure and (b) reversible expansion.*

  1. nRT=(1.00)(8.314)(298)=2478 JnRT = (1.00)(8.314)(298) = 2478\ \text{J}

  2. (a) Final pressure Pf=nRT/Vf=2478/11.0=225 PaP_f = nRT/V_f = 2478/11.0 = 225\ \text{Pa} (1 Pa = 1 J/m³)

    • wirr=−PextΔV=−(225 J/m3)(10.0 m3)=w_{irr} = -P_{ext}\Delta V = -(225\ \text{J/m}^3)(10.0\ \text{m}^3) = −2.25 × 10³ J

  3. (b) wrev=−(2478 J)ln⁡(11.0/1.00)=−(2478)(2.398)=w_{rev} = -(2478\ \text{J})\ln(11.0/1.00) = -(2478)(2.398) = −5.94 × 10³ J (your slide: −5941 J)

  4. The reversible path extracts more than twice the work.

⚠ Slide correction: the 5-step expansion total on your slide reads −4325 J with steps “−1625, −982…”. Recomputing each step (2 m3×P2\ \text{m}^3 \times P) gives −1652, −991, −708, −551, −450 J, totaling ≈ −4352 J. The slide has transposed digits. The trend (more steps → closer to −5941 J) is unaffected.


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Work done under reversible conditions is greater than when done irreversibly.

Statement

  • For a given initial and final state, the maximum work that a system can do on its surroundings is obtained when the process is carried out reversibly.

    • Expansion: ∣wrev∣>∣wirr∣|w_{rev}| > |w_{irr}| (the reversible path gives the most negative ww).

    • Compression: the reversible path requires the least work input (wrevw_{rev} is the smallest positive value).

  • Your slide’s shorthand “wrev>wirrw_{rev} > w_{irr}” refers to the magnitude of work done by the system.

Why: the physical argument

  • Work of expansion = −∫Pext dV-\int P_{ext}\,dV. Magnitude = area under the PextP_{ext} vs. VV curve.

  • During expansion, Pext≤PsysP_{ext} \leq P_{sys} (otherwise the gas wouldn’t expand).

  • The reversible process sets PextP_{ext} as large as possible at every step, equal to PsysP_{sys}. Any irreversible path has PextP_{ext} lower somewhere, so it traces less area.

  • Graphical picture (your slides): with 1 step, the rectangle is small. As steps increase (5 → 40 → ∞), the rectangles approach the curve and the area approaches the maximum.

Numerical illustration (1 mol, 298 K, 1 → 11 m³)

Path

Work done by gas

1 sudden step

≈ 2250 J

5 steps

≈ 4350 J

40 steps

≈ 5672 J

Infinite steps (reversible)

5941 J (maximum)

Connection to entropy and the second law

  • ΔS\Delta S is a state function, equal to qrev/Tq_{rev}/T for any path.

  • Because ∣q∣=∣w∣|q| = |w| at constant TT and ∣wirr∣<∣wrev∣|w_{irr}| < |w_{rev}|, we get ∣qirr∣<∣qrev∣|q_{irr}| < |q_{rev}|, so:

    • ΔS>qirrT\Delta S > \dfrac{q_{irr}}{T} for an irreversible process.

  • Interpretation: the “missing” work is dissipated as increased disorder in the universe, which is why ΔSuniv>0\Delta S_{univ} > 0 for irreversible processes.

Pitfalls

  • A reversible process is not one that merely “can go backward.” It is one that proceeds through a continuous sequence of equilibrium states, infinitely slowly.

  • Phase changes at the transition temperature (melting ice at 0 °C, 1 atm) are naturally reversible equilibrium processes. Gas expansions are not.

  • ΔE\Delta E, ΔH\Delta H and ΔS\Delta S are the same for both paths. Only qq and ww differ.

Worked example
*Q: 1.00 mol ideal gas at 298 K expands from 1.00 L to 10.0 L. Compare ∣w∣|w| for a single step against PextP_{ext} = final pressure vs. reversible.*

  1. nRT=2478 JnRT = 2478\ \text{J}

  2. Pf=nRT/Vf=2478 J/(10.0 L)=247.8 J/LP_f = nRT/V_f = 2478\ \text{J}/(10.0\ \text{L}) = 247.8\ \text{J/L}

  3. ∣wirr∣=PfΔV=(247.8 J/L)(9.00 L)=2230 J|w_{irr}| = P_f\Delta V = (247.8\ \text{J/L})(9.00\ \text{L}) = 2230\ \text{J}

  4. ∣wrev∣=nRTln⁡(10.0)=(2478)(2.303)=5706 J|w_{rev}| = nRT\ln(10.0) = (2478)(2.303) = 5706\ \text{J}

  5. Ratio ≈ 2.6: the reversible path does about 2.6× more work.


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Calculate the work done by a gas due to expansion (not necessarily isothermal). Calculate the change in internal energy due to heat and work.

Choosing the right work formula

  • Constant external pressure (irreversible): w=−PextΔVw = -P_{ext}\Delta V

  • Reversible isothermal ideal gas: w=−nRTln⁡(Vf/Vi)w = -nRT\ln(V_f/V_i)

  • Free expansion into vacuum (Pext=0P_{ext} = 0): w=0w = 0

  • Reaction producing or consuming gas at constant PP and TT: using PΔV=ΔngasRTP\Delta V = \Delta n_{gas}RT:

    • w=−Δngas RTw = -\Delta n_{gas}\,RT

    • Δngas\Delta n_{gas} = (moles gas products) − (moles gas reactants). Solids and liquids contribute negligible volume.

Calculating ΔE\Delta E

  • ΔE=q+w\Delta E = q + w, with each term in joules.

  • Heat from an electric heater: q=Ppower×tq = P_{power}\times t, where 1 W = 1 J/s.

Unit management (the most common source of error)

  • 1 L⋅atm=101.325 J1\ \text{L·atm} = 101.325\ \text{J}; also R=8.314 J K−1mol−1=0.08206 L atm K−1mol−1R = 8.314\ \text{J K}^{-1}\text{mol}^{-1} = 0.08206\ \text{L atm K}^{-1}\text{mol}^{-1}.

  • Convert kJ ↔ J before adding. Temperatures in K for RTRT terms. 1 mL=10−3 L1\ \text{mL} = 10^{-3}\ \text{L}.

  • Sign check: expansion → ww negative; compression → ww positive.

Worked example 1: heater and expansion (your slide)
*Q: A 100. W heater runs for 10.0 min heating a gas that expands from 2.00 L to 10.0 L against a constant 0.975 atm. Find ΔE\Delta E.*

  1. q=(100. J/s)(10.0×60 s)=6.00×104 J=+60.0 kJq = (100.\ \text{J/s})(10.0 \times 60\ \text{s}) = 6.00 \times 10^4\ \text{J} = +60.0\ \text{kJ}

  2. ΔV=10.0−2.00=8.00 L\Delta V = 10.0 - 2.00 = 8.00\ \text{L}

  3. w=−PextΔV=−(0.975 atm)(8.00 L)(101.33 J/L⋅atm)=−790 J=−0.790 kJw = -P_{ext}\Delta V = -(0.975\ \text{atm})(8.00\ \text{L})(101.33\ \text{J/L·atm}) = -790\ \text{J} = -0.790\ \text{kJ}

  4. ΔE=q+w=60.0−0.790=\Delta E = q + w = 60.0 - 0.790 = +59.2 kJ

Worked example 2: simple expansion
*Q: A gas expands by 500. mL against 1.20 atm. Find ww in J.*

  1. w=−(1.20 atm)(0.500 L)=−0.600 L⋅atmw = -(1.20\ \text{atm})(0.500\ \text{L}) = -0.600\ \text{L·atm}

  2. −0.600 L⋅atm×101.3 J/(L⋅atm)=-0.600\ \text{L·atm} \times 101.3\ \text{J/(L·atm)} = −60.8 J

Worked example 3: work from a chemical reaction
*Q: Ni(s) + 4 CO(g) → Ni(CO)₄(g) for 1.00 mol Ni at 75 °C. Find ww.*

  1. Δngas=1−4=−3 mol\Delta n_{gas} = 1 - 4 = -3\ \text{mol} (solid Ni is ignored)

  2. T=75+273=348 KT = 75 + 273 = 348\ \text{K}

  3. w=−ΔngasRT=−(−3.00 mol)(8.31 J K−1mol−1)(348 K)=w = -\Delta n_{gas}RT = -(-3.00\ \text{mol})(8.31\ \text{J K}^{-1}\text{mol}^{-1})(348\ \text{K}) = +8.68 × 10³ J

  4. Positive: the gas volume shrinks, so surroundings do work on the system.


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Calorimetry. Use the heat capacity of a substance to calculate the heat required to raise its temperature by a given amount.

Core concept

  • Calorimetry measures heat flow by monitoring a temperature change in a known mass of a known substance (often water).

  • Heat capacity (CC): the heat needed to raise the whole sample’s temperature by 1 K (or 1 °C). Units: J/K (extensive).

    • q=C ΔTq = C\,\Delta T

  • Specific heat capacity (csc_s): heat per gram per kelvin. Units: J g⁻¹ K⁻¹ (intensive).

    • q=m cs ΔTq = m\,c_s\,\Delta T

  • Molar heat capacity (cmolarc_{molar}): heat per mole per kelvin. Units: J mol⁻¹ K⁻¹ (intensive).

    • q=n cmolar ΔTq = n\,c_{molar}\,\Delta T

  • ΔT=Tfinal−Tinitial\Delta T = T_{final} - T_{initial}. A temperature difference in °C equals that in K, so no conversion is needed for ΔT\Delta T.

Molecular meaning

  • Substances with many ways to store energy (rotation, vibration, hydrogen bonds) have large heat capacities. Water has a high csc_s (4.184 J g⁻¹ °C⁻¹) due to extensive hydrogen bonding, which absorbs energy.

Calorimetry principle (isolated system)

  • Energy conservation: heat lost by the hot object = heat gained by the cold object.

    • −qhot=+qcold-q_{hot} = +q_{cold}, or equivalently ∑q=0\sum q = 0.

  • Assumptions: no heat exchange with the surroundings or the container (or the container’s heat capacity is included explicitly), and no phase changes.

  • Coffee-cup calorimeter: include the calorimeter heat capacity: qtotal=CcalΔT+mcsΔTq_{total} = C_{cal}\Delta T + m c_s \Delta T.

Pitfalls

  • Using TT in the wrong units in RTRT but not here. For ΔT\Delta T alone, °C and K are interchangeable.

  • Sign errors: the metal’s ΔT\Delta T is negative (cooling), so qmetal<0q_{metal} < 0.

  • ⚠ Your slide has a typo in its first example, writing 4.148 instead of 4.184 for water’s csc_s. The final answer (0.434) uses the correct value.

Worked example 1: heat required
*Q: How much energy is needed to raise an 8.50 × 10² g aluminum block from 22.8 °C to 94.6 °C? (csc_s = 0.900 J g⁻¹ °C⁻¹)*

  1. ΔT=94.6−22.8=71.8 °C\Delta T = 94.6 - 22.8 = 71.8\ °\text{C}

  2. q=(8.50×102 g)(0.900 J g−1°C−1)(71.8 °C)q = (8.50 \times 10^2\ \text{g})(0.900\ \text{J g}^{-1}\text{°C}^{-1})(71.8\ \text{°C})

  3. Units: g × J g⁻¹ °C⁻¹ × °C = J

  4. q=5.49×104 J=q = 5.49 \times 10^4\ \text{J} = 54.9 kJ (3 sig. figs.)

Worked example 2: final temperature
*Q: 840 J is absorbed by 10.0 g of water at 25.0 °C. Find TfT_f.*

  1. ΔT=q/(mcs)=840/(10.0×4.18)=20.1 °C\Delta T = q/(m c_s) = 840/(10.0 \times 4.18) = 20.1\ °\text{C}

  2. Tf=25.0+20.1=T_f = 25.0 + 20.1 = 45.1 °C


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Calculate energy changes from calorimetry data. Difference between cmolarc_{molar} and cspecificc_{specific}. How CC is related to cc. Relation between CPC_P and CVC_V.

Three related quantities

Symbol

Name

Units

Extensive?

CC

Heat capacity

J K⁻¹

Extensive

csc_s

Specific heat capacity

J g⁻¹ K⁻¹

Intensive

cmolarc_{molar}

Molar heat capacity

J mol⁻¹ K⁻¹

Intensive

  • Relationships: C=m cs=n cmolarC = m\,c_s = n\,c_{molar}

  • Conversion between the intensive forms: cmolar=cs×Mc_{molar} = c_s \times M (molar mass, g/mol).

  • Rule: lowercase cc = intensive; uppercase CC = extensive.

CVC_V vs. CPC_P

  • CVC_V (constant volume): CV=ΔEΔTC_V = \dfrac{\Delta E}{\Delta T}, since ΔE=qV=CVΔT\Delta E = q_V = C_V\Delta T.

  • CPC_P (constant pressure): CP=ΔHΔTC_P = \dfrac{\Delta H}{\Delta T}, since ΔH=qP=CPΔT\Delta H = q_P = C_P\Delta T.

  • Derivation of the ideal-gas relation:

    1. H=E+PVH = E + PV and PV=nRTPV = nRT gives H=E+nRTH = E + nRT.

    2. ΔH=ΔE+nR ΔT\Delta H = \Delta E + nR\,\Delta T

    3. Divide by ΔT\Delta T: ΔHΔT=ΔEΔT+nR\dfrac{\Delta H}{\Delta T} = \dfrac{\Delta E}{\Delta T} + nR

    4. CP=CV+nRC_P = C_V + nR (extensive form) and cP=cV+Rc_P = c_V + R (per mole).

  • Why CP>CVC_P > C_V: at constant PP, part of the heat supplied goes into expansion work against the surroundings (PΔV=nRΔTP\Delta V = nR\Delta T), so more heat is needed for the same ΔT\Delta T. At constant VV, all heat raises internal energy.

  • This relation is exact for ideal gases. For solids and liquids CP≈CVC_P \approx C_V because they barely expand.

Energy changes from calorimetry data

  1. Identify what absorbs heat (water, solution, calorimeter hardware).

  2. Compute q=CΔTq = C\Delta T or mcsΔTmc_s\Delta T for each, and add them.

  3. Apply energy conservation: qrxn=−(qwater+qcal)q_{rxn} = -(q_{water} + q_{cal}).

  4. Divide by moles for kJ/mol.

Worked example (from your slides): unknown metal
*Q: 18.0 g metal at 100 °C is placed in 50.2 g water at 22.0 °C. Final T = 24.8 °C. Find csc_s of the metal.*

  1. −qmetal=+qwater-q_{metal} = +q_{water}

  2. −[18.0 g cmetal(24.8−100)]=+[50.2 g (4.184)(24.8−22.0)]-[18.0\ \text{g}\ c_{metal}(24.8 - 100)] = +[50.2\ \text{g}\,(4.184)(24.8 - 22.0)]

  3. cmetal(18.0)(75.2)=(50.2)(4.184)(2.8)c_{metal}(18.0)(75.2) = (50.2)(4.184)(2.8)

  4. cmetal=5881354=c_{metal} = \dfrac{588}{1354} = 0.434 J g⁻¹ °C⁻¹


10
New cards

From internal energy to enthalpy. Why do we need enthalpy? Relation to calorimetry.

The problem with ΔE\Delta E

  • First law at constant pressure for expansion work only: ΔE=q−PΔV\Delta E = q - P\Delta V.

  • If volume is constant (ΔV=0\Delta V = 0), ΔE=qV\Delta E = q_V, so heat measures ΔE\Delta E directly (bomb calorimeter).

  • But most laboratory and biological chemistry occurs at constant pressure (open beakers, 1 atm). Constant volume is experimentally difficult to maintain.

  • At constant PP, the heat flow qPq_P equals ΔE\Delta E plus the expansion work term, so qP≠ΔEq_P \neq \Delta E. We need a state function whose change equals qPq_P.

Definition of enthalpy

  • H=E+PVH = E + PV (state function, extensive, J). Since EE, PP and VV are state functions, so is HH.

  • At constant PP: ΔH=ΔE+PΔV\Delta H = \Delta E + P\Delta V.

  • Substitute ΔE=q−PΔV\Delta E = q - P\Delta V: ΔH=q−PΔV+PΔV\Delta H = q - P\Delta V + P\Delta V

    • ΔH=qP\Delta H = q_P

  • Meaning: ΔH\Delta H is the heat absorbed or released at constant pressure. ΔH<0\Delta H < 0 is exothermic; ΔH>0\Delta H > 0 is endothermic.

  • PVPV term physically: the energy needed to “make room” for the system by pushing back the atmosphere.

Relating ΔH\Delta H and ΔE\Delta E for reactions

  • For ideal gases, PΔV=ΔngasRTP\Delta V = \Delta n_{gas}RT:

    • ΔH=ΔE+ΔngasRT\Delta H = \Delta E + \Delta n_{gas}RT

  • If Δngas=0\Delta n_{gas} = 0 (or only solids/liquids), ΔH≈ΔE\Delta H \approx \Delta E.

Relation to calorimetry

  • Constant volume (bomb): qV=ncVΔT=mcs,VΔT=ΔEq_V = nc_V\Delta T = mc_{s,V}\Delta T = \Delta E

  • Constant pressure (coffee cup): qP=ncPΔT=mcs,PΔT=ΔHq_P = nc_P\Delta T = mc_{s,P}\Delta T = \Delta H

Absolute vs. relative values

  • Absolute EE and HH can’t be measured, only differences. We choose a reference: ΔHf∘=0\Delta H_f^\circ = 0 for elements in their standard state (298 K, 1 atm). For hydrogen the standard state is H₂(g), not H(g).

Pitfall: ΔH=qP\Delta H = q_P is valid only at constant pressure with only expansion work.

Worked example
*Q: For ½H₂(g) + ½I₂(s) → HI(g), ΔH=+39.7\Delta H = +39.7 kJ at 298 K. Find ΔE\Delta E.*

  1. Δngas=1−12=+12\Delta n_{gas} = 1 - \tfrac12 = +\tfrac12 mol (I₂(s) not counted)

  2. ΔH=ΔE+ΔngasRT⇒ΔE=ΔH−ΔngasRT\Delta H = \Delta E + \Delta n_{gas}RT \Rightarrow \Delta E = \Delta H - \Delta n_{gas}RT

  3. ΔngasRT=(0.5)(8.314)(298)=1239 J=1.24 kJ\Delta n_{gas}RT = (0.5)(8.314)(298) = 1239\ \text{J} = 1.24\ \text{kJ}

  4. ΔE=39.7−1.24=\Delta E = 39.7 - 1.24 = 38.5 kJ


11
New cards

Distinguish between the internal energy and the enthalpy of a process and describe how each is measured.

Comparison


Internal energy ΔE\Delta E

Enthalpy ΔH\Delta H

Definition

Total kinetic + potential energy change of the system

ΔH=ΔE+Δ(PV)\Delta H = \Delta E + \Delta(PV)

Equals heat at…

Constant volume: ΔE=qV\Delta E = q_V

Constant pressure: ΔH=qP\Delta H = q_P

Instrument

Bomb calorimeter (rigid sealed steel vessel)

Coffee-cup (constant-pressure) calorimeter

Heat capacity used

CVC_V

CPC_P

State function?

Yes

Yes

Includes expansion work?

No (wPV=0w_{PV}=0 at constant VV)

Accounts for it automatically

Measuring ΔE\Delta E: bomb calorimeter

  • The sample burns in a sealed rigid “bomb” (constant VV) surrounded by water in an insulated container. An ignition wire triggers the reaction.

  • qrxn=−(qwater+qbomb)=−(mwcw+Ccal)ΔTq_{rxn} = -(q_{water} + q_{bomb}) = -(m_{w}c_{w} + C_{cal})\Delta T, and ΔE=qV=qrxn\Delta E = q_V = q_{rxn}.

Measuring ΔH\Delta H: constant-pressure calorimeter

  • A reaction occurs in solution in an insulated cup with a loosely fitting lid (open to atmosphere at ~1 atm).

  • qrxn=−(msolncs+Ccal)ΔTq_{rxn} = -(m_{soln}c_s + C_{cal})\Delta T, and ΔH=qP=qrxn\Delta H = q_P = q_{rxn}.

  • ΔH\Delta H per mole = qrxn/nlimiting reagentq_{rxn}/n_{\text{limiting reagent}}.

Pitfalls

  • Sign: if the temperature of the solution rises, the reaction is exothermic, so ΔH\Delta H is negative.

  • Limiting reagent: divide by moles of the limiting reactant, not by moles of “solution.”

  • ⚠ Slide correction: your KOH(s) + HCl(aq) calorimetry example computes q=6762q = 6762 J correctly but (1) divides by 0.08 mol labeled “moles of solution” (it is the limiting reagent HCl: 0.800 L × 0.100 M), and (2) reports +84.5 kJ/mol, but since TT rose, the correct answer is ΔH = −84.5 kJ/mol.

Worked example 1: constant-pressure (coffee cup)
*Q: 0.0300 mol NaOH(s) is added to 1000 mL of 0.0300 M HNO₃ at 23.000 °C. TfT_f = 23.639 °C. CcalC_{cal} = 451 J/°C; csc_s = 4.18 J g⁻¹ °C⁻¹; density = 1.00 g/mL. Find ΔH\Delta H per mole.*

  1. ΔT=0.639 °C\Delta T = 0.639\ °\text{C}

  2. qcal=(451)(0.639)=288 Jq_{cal} = (451)(0.639) = 288\ \text{J}

  3. qsoln=(1000 g)(4.18)(0.639)=2671 Jq_{soln} = (1000\ \text{g})(4.18)(0.639) = 2671\ \text{J}

  4. qtotal gained=2959 Jq_{total\ gained} = 2959\ \text{J}, so qrxn=−2959 Jq_{rxn} = -2959\ \text{J}

  5. ΔH=−2959 J/0.0300 mol=−98,600 J/mol=\Delta H = -2959\ \text{J}/0.0300\ \text{mol} = -98{,}600\ \text{J/mol} = −98.6 kJ/mol

Worked example 2: constant-volume (bomb)
*Q: 5.000 g methanol (32.04 g/mol) burns in a bomb with 4000 g water (TT: 24.000 → 29.765 °C); CcalC_{cal} = 2657 J/°C. Find ΔE\Delta E per mole.*

  1. ΔT=5.765 °C\Delta T = 5.765\ °\text{C}

  2. qcal=2657(5.765)=15,318 Jq_{cal} = 2657(5.765) = 15{,}318\ \text{J}; qwater=4000(4.184)(5.765)=96,486 Jq_{water} = 4000(4.184)(5.765) = 96{,}486\ \text{J}

  3. Total heat released by reaction = 111.8 kJ per 5.000 g

  4. Per mole: 111.8×(32.04/5.000)=716 kJ/mol111.8 \times (32.04/5.000) = 716\ \text{kJ/mol}

  5. Exothermic: ΔE=−716 kJ/mol\Delta E = -716\ \text{kJ/mol}


12
New cards

Contributions to internal energy in the case of monoatomic, polyatomic (linear), polyatomic (non-linear) species.

Foundation: equipartition

  • Each quadratic degree of freedom contributes 12kT\tfrac12 kT per molecule, i.e., 12RT\tfrac12RT per mole.

    • k=1.381×10−23 J K−1k = 1.381\times10^{-23}\ \text{J K}^{-1} (Boltzmann’s constant); NAk=RN_A k = R.

  • Ideal gas assumption: no intermolecular potential energy, so EE is purely the sum of molecular motions.

Types of motion

  • Translation: 3 degrees of freedom for any gas particle (movement along xx, yy, zz).

  • Rotation: present for molecules, not atoms (point masses have negligible moment of inertia).

  • Vibration: only significantly excited at high temperatures, ignored at room temperature (the energy spacing is large compared to kTkT; quantum mechanically the mode is “frozen out”).

Results

Species

Translational

Rotational

Total EE (per mol)

CVC_V

CP=CV+RC_P = C_V + R

Monoatomic (He, Ar)

3 × ½RT

0

32RT\tfrac32RT

32R\tfrac32R

52R\tfrac52R

Linear polyatomic (H₂, N₂, CO₂)

3 × ½RT

2 × ½RT

52RT\tfrac52RT

52R\tfrac52R

72R\tfrac72R

Non-linear polyatomic (H₂O, NH₃, CH₄)

3 × ½RT

3 × ½RT

3RT3RT (= 62RT\tfrac62RT)

3R3R

4R4R

Why linear molecules have only 2 rotations

  • A linear molecule can tumble about two axes perpendicular to the molecular axis. Rotation about the bond axis involves essentially no change in the positions of the atomic nuclei (point-like masses on the axis), so its moment of inertia is negligibly small.

  • Quantized rotational energy ∝1/I\propto 1/I, so the first excited level of this mode is enormously high, so it is never populated at accessible temperatures. Your slide expresses this as requiring energies so large that the molecule would dissociate first.

  • Non-linear molecules have atoms off any single axis, so all 3 rotational axes have appreciable moments of inertia.

Pitfalls

  • These values hold at moderate temperatures. At high TT, vibrations contribute (each vibrational mode adds kTkT: ½ kinetic + ½ potential), so measured CVC_V rises above these values.

  • The CP=CV+RC_P = C_V + R shortcut applies to 1 mole of ideal gas.

  • In liquids and solids, intermolecular potential energy matters, so these formulas do not apply.

Worked example
*Q: Estimate the molar internal energy of N₂(g) and CO₂(g) at 298 K, and ΔE\Delta E for heating 1.00 mol of H₂O vapor by 50.0 K (ideal, no vibration).*

  1. N₂ and CO₂ are both linear: E=52RT=2.5(8.314)(298)=6194 J/mol≈E = \tfrac52RT = 2.5(8.314)(298) = 6194\ \text{J/mol} \approx 6.19 kJ/mol

  2. H₂O is non-linear: CV=3R=24.94 J K−1mol−1C_V = 3R = 24.94\ \text{J K}^{-1}\text{mol}^{-1}

  3. ΔE=nCVΔT=(1.00)(24.94)(50.0)=\Delta E = nC_V\Delta T = (1.00)(24.94)(50.0) = 1247 J ≈ 1.25 kJ


13
New cards

Use standard enthalpies of formation to calculate the standard enthalpy of a reaction.

Definitions

  • Standard enthalpy of formation (ΔHf∘\Delta H_f^\circ): the enthalpy change when 1 mole of a compound forms from its elements in their standard states at 1 bar/1 atm (and usually 298 K). Units: kJ/mol.

  • Elements in their standard states have ΔHf∘=0\Delta H_f^\circ = 0: O₂(g), H₂(g), N₂(g), C(graphite), Fe(s), Hg(l), Br₂(l). Not H(g), O(g) or C(diamond).

  • Formation of a compound is written with a coefficient of 1 on the product, e.g. C(s) + 2H₂(g) → CH₄(g).

Formula

  • ΔHrxn∘=∑np ΔHf∘(products)−∑nr ΔHf∘(reactants)\Delta H^\circ_{rxn} = \sum n_p\,\Delta H_f^\circ(\text{products}) - \sum n_r\,\Delta H_f^\circ(\text{reactants})

    • np,nrn_p, n_r = stoichiometric coefficients (mol) from the balanced equation.

  • Explicitly, for aA+bB→cC+dDaA + bB \to cC + dD:

    • ΔHrxn∘=cΔHf∘(C)+dΔHf∘(D)−[aΔHf∘(A)+bΔHf∘(B)]\Delta H^\circ_{rxn} = c\Delta H_f^\circ(C) + d\Delta H_f^\circ(D) - [a\Delta H_f^\circ(A) + b\Delta H_f^\circ(B)]

Why it works

  • HH is a state function. Imagine decomposing all reactants into elements (enthalpy change =−ΔHf∘= -\Delta H_f^\circ of reactants) and then forming all products from elements (+ΔHf∘+\Delta H_f^\circ of products). The elements cancel, and the net change equals the formula above (a special case of Hess’s law).

  • Bond picture: breaking bonds is endothermic (ΔH>0\Delta H > 0), forming bonds is exothermic (ΔH<0\Delta H < 0). Products − reactants = final − initial.

Pitfalls

  • Multiply each ΔHf∘\Delta H_f^\circ by its coefficient.

  • Phase matters: ΔHf∘\Delta H_f^\circ[H₂O(l)] = −285.8 vs. ΔHf∘\Delta H_f^\circ[H₂O(g)] = −241.8 kJ/mol. The difference is the enthalpy of vaporization (≈44 kJ/mol).

  • Order: products minus reactants (not the reverse).

  • Units: “kJ/mol” in this context means kJ per mole of reaction as written.

  • Extensive: doubling the equation doubles ΔHrxn∘\Delta H^\circ_{rxn}.

  • ⚠ Slide corrections (acetylene examples): C₂H₂ is acetylene (ethylene is C₂H₄). The accepted ΔHf∘\Delta H_f^\circ[C₂H₂(g)] is +226.7 kJ/mol (consistent with your own Hess’s-law question, 226.7), not +277. With H₂O(g) at −241.8, the correct combustion enthalpy is 2(−393.5)+(−241.8)−226.7=−1255.52(-393.5) + (-241.8) - 226.7 = -1255.5 kJ/mol.

Worked example (from your slides)
*Q: Calculate ΔH∘\Delta H^\circ for CH₄(g) + 2O₂(g) → CO₂(g) + 2H₂O(l). Given ΔHf∘\Delta H_f^\circ: CH₄ = −74.8, CO₂ = −393.5, H₂O(l) = −285.8 kJ/mol.*

  1. Products: (1)(−393.5)+(2)(−285.8)=−393.5−571.6=−965.1 kJ(1)(-393.5) + (2)(-285.8) = -393.5 - 571.6 = -965.1\ \text{kJ}

  2. Reactants: (1)(−74.8)+(2)(0)=−74.8 kJ(1)(-74.8) + (2)(0) = -74.8\ \text{kJ} (O₂ is an element)

  3. ΔHrxn∘=−965.1−(−74.8)=\Delta H^\circ_{rxn} = -965.1 - (-74.8) = −890.3 kJ/mol (exothermic)


14
New cards

Calculate an overall reaction enthalpy from the enthalpies of the reactions in a reaction sequence by using Hess’s law.

Hess’s law

  • The enthalpy change for a reaction is the same whether it occurs in one step or through a series of steps; the overall ΔH\Delta H is the sum of the ΔH\Delta H values of the individual steps.

  • Basis: HH is a state function, so ΔH\Delta H depends only on initial and final states: ΔHRP=ΔHRI+ΔHIP\Delta H_{RP} = \Delta H_{RI} + \Delta H_{IP} (reactants → intermediates → products).

  • Utility: lets us find ΔH\Delta H for reactions that are hard to measure directly (e.g., C → CH₄, diamond → graphite) from combustion or other easily measured reactions.

Three manipulation rules

  1. Reverse a reaction → change the sign of ΔH\Delta H.

  2. Multiply a reaction by a factor kk → multiply ΔH\Delta H by kk (ΔH\Delta H is extensive).

  3. Add equations → add their ΔH\Delta H values. Species that appear on both sides cancel.

Problem-solving strategy

  1. Write the target equation clearly.

  2. Locate each target reactant/product in exactly one given equation, and orient and scale that equation to match.

  3. Add the modified equations. Check that all intermediates cancel and the result equals the target.

  4. Sum the modified ΔH\Delta H values. Keep track of signs and units (kJ).

Pitfalls

  • Forgetting to flip the sign when reversing.

  • Forgetting to multiply ΔH\Delta H when scaling coefficients.

  • Mismatched phases (H₂O(l) vs. H₂O(g)).

  • The same ΔG\Delta G logic also follows Hess’s law, which is why coupled biochemical reactions (e.g., ATP hydrolysis driving glucose phosphorylation) simply add their ΔG\Delta G values.

Worked example 1 (from your slides): ΔH_f of propane
Target: 3C(gr) + 4H₂(g) → C₃H₈(g)
Given:
(a) C₃H₈ + 5O₂ → 3CO₂ + 4H₂O(l)   ΔH=−2220\Delta H = -2220 kJ
(b) C(gr) + O₂ → CO₂   ΔH=−394\Delta H = -394 kJ
(c) H₂ + ½O₂ → H₂O(l)   ΔH=−286\Delta H = -286 kJ

  1. Reverse (a) (propane must be a product): 3CO₂ + 4H₂O → C₃H₈ + 5O₂   ΔH=+2220\Delta H = +2220 kJ

  2. Multiply (b) by 3 (need 3 C): 3C + 3O₂ → 3CO₂   ΔH=3(−394)=−1182\Delta H = 3(-394) = -1182 kJ

  3. Multiply (c) by 4 (need 4 H₂): 4H₂ + 2O₂ → 4H₂O   ΔH=4(−286)=−1144\Delta H = 4(-286) = -1144 kJ

  4. Add: CO₂, H₂O and O₂ cancel (5 O₂ produced on the right; 3 + 2 = 5 O₂ consumed on the left).

  5. ΔH=+2220−1182−1144=\Delta H = +2220 - 1182 - 1144 = −106 kJ

Worked example 2: diamond → graphite (from your slides)

  1. C(diamond) + O₂ → CO₂   −395.4-395.4 kJ (as given)

  2. 2CO₂ → 2CO + O₂   +566.0+566.0 kJ (as given)

  3. 2CO → C(graphite) + CO₂   −172.5-172.5 kJ (as given)

  4. Adding: C(diamond) → C(graphite), ΔH=−395.4+566.0−172.5=\Delta H = -395.4 + 566.0 - 172.5 = −1.9 kJ

  5. Slightly exothermic, so graphite is the more stable form.