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8.3 Steady-State Energy Balances

Key Takeaways

  • The First Law of Thermodynamics for open systems under steady state simplifies to Q_dot - W_dot_s = Delta(H_dot) when kinetic and potential energy changes are negligible.

  • Enthalpy changes in non-reactive systems are calculated as Delta H = m * integral(Cp dT) for sensible heat, plus m * Delta H_v or m * Delta H_m for phase transitions.

  • Heats of reaction at standard reference conditions (298 K, 1 bar) are calculated from standard heats of formation: Delta H_rxn = sum(nu_i * Delta H_f,i).

  • To find the heat of reaction at temperatures other than standard reference conditions, Kirchhoff's Law is applied: Delta H_rxn(T) = Delta H_rxn(T_ref) + integral(Delta Cp dT).

  • Combustion calculations require determining the stoichiometric oxygen requirement, percent excess air, and accounting for the standard 79% N2 and 21% O2 composition of air on both a wet and dry basis.

Last updated: July 2026

Thermodynamic Principles and the First Law

Material balances track mass flows, whereas energy balances track the heat, work, and internal energy flows within a system. The thermodynamic foundation of energy balances is the First Law of Thermodynamics, which expresses the conservation of energy. For a closed system (no mass flow crossing the system boundary), the First Law is written as:

ΔU+ΔKE+ΔPE=Q−W\Delta U + \Delta \text{KE} + \Delta \text{PE} = Q - W

where ΔU\Delta U is the change in internal energy, ΔKE\Delta \text{KE} is the change in kinetic energy, ΔPE\Delta \text{PE} is the change in potential energy, QQ is the heat added to the system, and WW is the work done by the system. For most chemical process units, changes in kinetic and potential energy are negligible, simplifying the closed system balance to ΔU=Q−W\Delta U = Q - W.

For an open system (control volume) operating at steady state, mass enters and leaves the system continuously. In this case, we must account for the work required to push fluid into and out of the system (flow work). Enthalpy (H=U+PVH = U + PV) is defined to combine internal energy and flow work. The steady-state open-system energy balance is:

ΔH˙+ΔKE˙+ΔPE˙=Q˙−W˙s\Delta \dot{H} + \Delta \dot{\text{KE}} + \Delta \dot{\text{PE}} = \dot{Q} - \dot{W}_s

where Q˙\dot{Q} is the rate of heat input, W˙s\dot{W}_s is the shaft work rate (work associated with pumps, turbines, or compressors), and ΔH˙\Delta \dot{H} is the net rate of enthalpy flow leaving the system minus that entering. Neglecting kinetic and potential energy changes, the balance simplifies to the standard form found in the FE Reference Handbook:

Q˙−W˙s=∑m˙outH^out−∑m˙inH^in\dot{Q} - \dot{W}_s = \sum \dot{m}_{out} \hat{H}_{out} - \sum \dot{m}_{in} \hat{H}_{in}

where H^\hat{H} is the specific enthalpy (energy per unit mass). To evaluate these enthalpies, you must establish a reference state (e.g., liquid water at 0.01∘C0.01^\circ C and 1 bar1 \text{ bar}) where specific enthalpy is defined as zero.

Enthalpy Changes in Non-Reactive Systems

For systems without chemical reactions, enthalpy changes occur due to temperature changes (sensible heat) or phase changes (latent heat). The change in specific enthalpy for a substance heated from T1T_1 to T2T_2 without phase change is calculated using its constant-pressure heat capacity (CpC_p):

ΔH^=∫T1T2Cp(T)dT\Delta \hat{H} = \int_{T_1}^{T_2} C_p(T) dT

If the heat capacity is constant or an average value Cˉp\bar{C}_p is used, this simplifies to ΔH^=Cˉp(T2−T1)\Delta \hat{H} = \bar{C}_p(T_2 - T_1). When a phase change occurs (such as vaporization or melting), you must add the latent heat of vaporization (ΔHv\Delta H_v) or latent heat of fusion (ΔHm\Delta H_m) at the transition temperature:

ΔH^=∫T1TtransitionCp,phase1dT+ΔHphase_change+∫TtransitionT2Cp,phase2dT\Delta \hat{H} = \int_{T_1}^{T_{transition}} C_{p,phase1} dT + \Delta H_{phase\_change} + \int_{T_{transition}}^{T_2} C_{p,phase2} dT

Thermochemistry and Heats of Reaction

When chemical reactions occur, chemical bonds are broken and formed, releasing or absorbing energy. The heat of reaction (ΔHrxn\Delta H_{rxn}) is the enthalpy change when stoichiometric quantities of reactants react completely at a specified temperature and pressure. The standard heat of reaction at reference conditions (Tref=298.15 KT_{ref} = 298.15 \text{ K}, P=1 barP = 1 \text{ bar}) is calculated using standard heats of formation (ΔHf,i∘\Delta H_{f,i}^\circ):

ΔHrxn∘=∑νiΔHf,i∘=∑νjΔHf,j∘ (products)−∑νkΔHf,k∘ (reactants)\Delta H_{rxn}^\circ = \sum \nu_i \Delta H_{f,i}^\circ = \sum \nu_j \Delta H_{f,j}^\circ \text{ (products)} - \sum \nu_k \Delta H_{f,k}^\circ \text{ (reactants)}

where νi\nu_i is the stoichiometric coefficient of species ii (positive for products, negative for reactants). Standard heats of formation for common substances are tabulated in the chemistry and thermodynamics sections of the FE Reference Handbook. Note that the standard heat of formation of any elemental substance in its most stable physical state (e.g., O2(g)O_2(g), N2(g)N_2(g), C(s)C(s)) is zero.

To find the heat of reaction at a temperature TT other than the reference temperature, Kirchhoff's Law is applied:

ΔHrxn(T)=ΔHrxn∘(Tref)+∫TrefTΔCpdT\Delta H_{rxn}(T) = \Delta H_{rxn}^\circ(T_{ref}) + \int_{T_{ref}}^T \Delta C_p dT

where ΔCp=∑νiCp,i\Delta C_p = \sum \nu_i C_{p,i}. For a reactive system, the energy balance is evaluated by calculating the heat of reaction at a reference temperature and adding the sensible heat changes of the reactants and products relative to that reference temperature.

Combustion Calculations

Combustion is the rapid reaction of a fuel with oxygen to produce carbon dioxide, water, and heat. Combustion calculations are a major focus of the FE Chemical exam and require key definitions:

  • Theoretical Oxygen (Stoichiometric O2O_2): The exact amount of oxygen required for complete combustion of all carbon to CO2CO_2, hydrogen to H2OH_2 O, and sulfur to SO2SO_2.
  • Excess Air: The amount of air fed to the burner in excess of the theoretical requirement. It is calculated as:
% Excess Air=(O2)fed−(O2)stoich(O2)stoich×100%\% \text{ Excess Air} = \frac{(O_2)_{fed} - (O_2)_{stoich}}{(O_2)_{stoich}} \times 100\%

Since air is modeled as 21 mol% O221 \text{ mol\% } O_2 and 79 mol% N279 \text{ mol\% } N_2, the moles of nitrogen entering with air is N2=O2×(79/21)=3.76×O2N_2 = O_2 \times (79/21) = 3.76 \times O_2.

  • Wet-Basis vs. Dry-Basis: Dry-basis composition lists the mole fractions of the flue gas components excluding water vapor. Wet-basis composition includes all components, including water vapor. Be sure to convert between wet and dry bases as specified in the exam problem.

Worked Example: Combustion Energy Balance

Propane gas (C3H8C_3 H_8) is burned completely with 20.0%20.0\% excess air. Both the propane and the air enter the burner at 25∘C25^\circ C (298 K298 \text{ K}). The combustion products leave the chamber at 500∘C500^\circ C (773 K773 \text{ K}). Calculate the heat removed from the burner (Q˙\dot{Q}, in kJ\text{kJ}) per mole of propane burned. The standard heat of combustion of propane at 25∘C25^\circ C (with water as a gas) is ΔHc∘=−2,044 kJ/mol\Delta H_c^\circ = -2,044 \text{ kJ/mol}. The average heat capacities (CpC_p) between 25∘C25^\circ C and 500∘C500^\circ C are: Cp,CO2=0.045 kJ/(mol⋅∘C)C_{p, CO2} = 0.045 \text{ kJ/(mol}\cdot^\circ C), Cp,H2O=0.036 kJ/(mol⋅∘C)C_{p, H2O} = 0.036 \text{ kJ/(mol}\cdot^\circ C), Cp,O2=0.032 kJ/(mol⋅∘C)C_{p, O2} = 0.032 \text{ kJ/(mol}\cdot^\circ C), and Cp,N2=0.030 kJ/(mol⋅∘C)C_{p, N2} = 0.030 \text{ kJ/(mol}\cdot^\circ C).

Solution:

First, write the balanced stoichiometric equation for propane combustion:

C3H8(g)+5O2(g)→3CO2(g)+4H2O(g)C_3 H_8 (g) + 5 O_2 (g) \to 3 CO_2 (g) + 4 H_2 O (g)

Based on 1.0 mole1.0 \text{ mole} of propane burned:

  • Stoichiometric O2O_2 required = 5.0 mol5.0 \text{ mol}
  • Actual O2O_2 fed = 5.0×1.20=6.0 mol5.0 \times 1.20 = 6.0 \text{ mol} (representing 20%20\% excess)
  • Actual N2N_2 fed = 6.0×(79/21)=22.57 mol6.0 \times (79/21) = 22.57 \text{ mol}

The product stream composition is:

  • CO2=3.0 molCO_2 = 3.0 \text{ mol}
  • H2O=4.0 molH_2 O = 4.0 \text{ mol}
  • O2 remaining=6.0−5.0=1.0 molO_2 \text{ remaining} = 6.0 - 5.0 = 1.0 \text{ mol}
  • N2 remaining=22.57 molN_2 \text{ remaining} = 22.57 \text{ mol}

Since the reactants enter at the reference temperature (25∘C25^\circ C), their inlet enthalpy is zero. The heat removed Q˙\dot{Q} is the sum of the heat of reaction at 25∘C25^\circ C and the sensible heat change of the products as they are heated from 25∘C25^\circ C to 500∘C500^\circ C (ΔT=475∘C\Delta T = 475^\circ C):

Q˙=ΔHc∘+∑niCp,iΔT\dot{Q} = \Delta H_c^\circ + \sum n_i C_{p,i} \Delta T

Calculate the sum of niCp,in_i C_{p,i} for the products:

∑niCp,i=(3.0)(0.045)+(4.0)(0.036)+(1.0)(0.032)+(22.57)(0.030)\sum n_i C_{p,i} = (3.0)(0.045) + (4.0)(0.036) + (1.0)(0.032) + (22.57)(0.030) ∑niCp,i=0.135+0.144+0.032+0.6771=0.9881 kJ/∘C\sum n_i C_{p,i} = 0.135 + 0.144 + 0.032 + 0.6771 = 0.9881 \text{ kJ/}^\circ C

Now, calculate the sensible heat change:

ΔHsensible=(0.9881 kJ/∘C)(475∘C)=469.35 kJ\Delta H_{sensible} = (0.9881 \text{ kJ/}^\circ C)(475^\circ C) = 469.35 \text{ kJ}

Finally, calculate the heat removed:

Q˙=−2,044 kJ+469.35 kJ=−1,574.65 kJ\dot{Q} = -2,044 \text{ kJ} + 469.35 \text{ kJ} = -1,574.65 \text{ kJ}

Thus, approximately 1,575 kJ1,575 \text{ kJ} of heat is released (removed) per mole of propane burned.

Test Your Knowledge

Methane (CH_4) is burned completely with 50.0% excess air. What is the mole fraction of nitrogen (N_2) in the resulting flue gas on a dry basis?

A

79.0%

B

85.0%

C

73.8%

D

64.3%

Test Your Knowledge

The standard heat of reaction at 25°C for the hydrogenation of ethylene is: C_2H_4(g) + H_2(g) -> C_2H_6(g). If the standard heats of formation are: Delta H_f, C_2H_4 = 52.3 kJ/mol and Delta H_f, C_2H_6 = -84.7 kJ/mol, what is the standard heat of reaction at 25°C?

A

-32.4 kJ/mol

B

32.4 kJ/mol

C

137.0 kJ/mol

D

-137.0 kJ/mol

Test Your Knowledge

Air and fuel enter a steady-state burner at 25°C. If the combustion is adiabatic (no heat is removed from the burner, Q_dot = 0) and there is no shaft work (W_dot_s = 0), what is the relationship between the enthalpy of the product gas stream and the enthalpy of reaction?

A

The sensible enthalpy change of the product gas stream relative to 25°C must equal the negative of the standard heat of reaction

B

The sensible enthalpy change of the product gas stream relative to 25°C must equal the standard heat of reaction

C

The sensible enthalpy change of the product gas stream relative to 25°C must equal zero

D

The sensible enthalpy change of the product gas stream relative to 25°C is independent of the heat of reaction

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