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Intermediate chemical engineering: 50 equations and principles

The core chemical engineering courses: energy balances, phase equilibrium, distillation, fluid flow, heat transfer, kinetics, reactor design and control.

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Steady-state energy balance on an open system

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  1. 1
    Steady-state energy balance on an open system
    Q˙−W˙s=ΔH˙+ΔE˙k+ΔE˙p\dot{Q} - \dot{W}_s = \Delta\dot{H} + \Delta\dot{E}_k + \Delta\dot{E}_p
    Q˙\dot{Q} is heat added to the system, W˙s\dot{W}_s shaft work done by it, and Δ\Delta means outlet minus inlet. The kinetic and potential energy terms are often negligible.
  2. 2
    Enthalpy change for heating without a phase change
    ΔH^=∫T1T2Cp(T) dT\Delta\hat{H} = \displaystyle\int_{T_1}^{T_2} C_p(T)\,dT
    Exact for ideal gases and close for liquids and solids. With constant CpC_p, ΔH^=Cp ΔT\Delta\hat{H} = C_p\,\Delta T.
  3. 3
    Heat of vaporization of water at 100 °C
    About 2257 kJ/kg2257\ \mathrm{kJ/kg}, or 40.7 kJ/mol40.7\ \mathrm{kJ/mol}
    A latent heat: it is absorbed at constant temperature and pressure while the phase changes.
  4. 4
    Standard heat of reaction from heats of formation
    ΔHr∘=∑iνi ΔHf,i∘\Delta H_r^\circ = \displaystyle\sum_i \nu_i\,\Delta H_{f,i}^\circ
    νi\nu_i is positive for products and negative for reactants. The heat of formation of an element in its standard state is zero.
  5. 5
    Mechanical energy balance
    ΔPρ+Δv22+g Δz+F^=−W˙sm˙\dfrac{\Delta P}{\rho} + \dfrac{\Delta v^2}{2} + g\,\Delta z + \hat{F} = -\dfrac{\dot{W}_s}{\dot{m}}
    For an incompressible fluid at steady state; F^\hat{F} is the friction loss per unit mass. With no friction or shaft work it becomes Bernoulli’s equation.
  6. 6
    Why use recycle?
    To send unreacted feed back to the reactor, raising overall conversion and cutting raw material use and waste
    Recycle also recovers solvents and catalysts.
  7. 7
    Single-pass vs overall conversion
    Single-pass: the fraction of reactant entering the reactor that reacts in it. Overall: the fraction of reactant fed to the whole process that reacts
    With unreacted feed recycled, overall conversion can be far higher than single-pass conversion.
  8. 8
    Purge stream
    A small stream drawn off a recycle loop to stop inert gases or impurities from building up
    Example: argon and methane purged from the ammonia synthesis loop. Some reactant is lost with them.
  9. 9
    Bypass stream
    Part of a feed that skips a process unit and rejoins its outlet, used to control the final composition or temperature
  10. 10
    Raoult’s law
    yiP=xiPisat(T)y_i P = x_i P_i^{\text{sat}}(T)
    For ideal liquid solutions with an ideal vapor; most accurate when a component is nearly pure (xix_i close to 1).
  11. 11
    Henry’s law
    yiP=xiHi(T)y_i P = x_i H_i(T)
    For a dilute solute (xix_i close to 0), such as a sparingly soluble gas. HiH_i is the Henry’s law constant, in pressure units in this form.
  12. 12
    Antoine equation
    log⁡10Psat=A−BT+C\log_{10} P^{\text{sat}} = A - \dfrac{B}{T + C}
    An empirical vapor pressure fit. AA, BB and CC are tabulated for each substance, for specific units and a temperature range.
  13. 13
    Relative volatility
    αij=yi/xiyj/xj\alpha_{ij} = \dfrac{y_i/x_i}{y_j/x_j}
    Under Raoult’s law, αij=Pisat/Pjsat\alpha_{ij} = P_i^{\text{sat}}/P_j^{\text{sat}}. The closer it is to 1, the harder the separation by distillation.
  14. 14
    Bubble-point temperature
    The temperature at which a liquid heated at constant pressure forms its first bubble of vapor
    For an ideal solution, solve ∑ixiPisat(T)=P\sum_i x_i P_i^{\text{sat}}(T) = P for TT.
  15. 15
    Dew-point temperature
    The temperature at which a vapor cooled at constant pressure forms its first drop of liquid
    For an ideal solution, solve ∑iyiPPisat(T)=1\sum_i \dfrac{y_i P}{P_i^{\text{sat}}(T)} = 1 for TT.
  16. 16
    Azeotrope
    A mixture whose equilibrium vapor has the same composition as the liquid, so ordinary distillation can’t separate it further
    Ethanol and water form one at about 95.6 wt% ethanol at 1 atm.
  17. 17
    Reflux ratio
    R=LDR = \dfrac{L}{D}: the liquid returned to the column per unit of distillate withdrawn
  18. 18
    Effect of raising the reflux ratio
    Fewer stages are needed for the same separation, but reboiler and condenser duties, and so energy costs, rise
    The optimum balances the column’s capital cost against its energy cost.
  19. 19
    Constant molar overflow
    The McCabe–Thiele assumption that the liquid and vapor molar flows are constant within each section of the column
    It holds when the components have similar molar heats of vaporization and heat losses are small.
  20. 20
    Rectifying-section operating line
    yn+1=RR+1 xn+xDR+1y_{n+1} = \dfrac{R}{R + 1}\,x_n + \dfrac{x_D}{R + 1}
    It crosses the diagonal y=xy = x at xDx_D, the distillate composition.
  21. 21
    Feed line (q-line)
    y=qq−1 x−zFq−1y = \dfrac{q}{q - 1}\,x - \dfrac{z_F}{q - 1}
    For a two-phase feed, qq is its liquid fraction. A saturated liquid feed (q=1q = 1) gives a vertical line; a saturated vapor (q=0q = 0), a horizontal one.
  22. 22
    Counting stages in a McCabe–Thiele diagram
    Step between the equilibrium curve and the operating lines from one end of the column to the other; each step is one equilibrium stage
    A partial reboiler counts as one equilibrium stage.
  23. 23
    Gas absorption vs stripping
    Absorption transfers a component from a gas into a liquid solvent; stripping (desorption) transfers it from a liquid into a gas
    Example: removing CO2\mathrm{CO_2} from natural gas with an amine solution.
  24. 24
    Absorption factor
    A=LmVA = \dfrac{L}{mV}
    LL and VV are the liquid and gas molar flows, mm the slope of the equilibrium line. With A>1A > 1, enough stages can absorb nearly all of the solute.
  25. 25
    Liquid–liquid extraction
    Moves a solute from one liquid into an immiscible solvent in which it is more soluble
    The solvent-rich product is the extract; the treated feed left behind is the raffinate.
  26. 26
    Distribution coefficient in extraction
    KD=yxK_D = \dfrac{y}{x} at equilibrium
    yy is the solute concentration in the extract phase and xx in the raffinate phase. A larger KDK_D means less solvent is needed.
  27. 27
    Reynolds number for pipe flow
    Re=ρvDμRe = \dfrac{\rho v D}{\mu}
    Flow is laminar below about 2100, turbulent above about 4000, and transitional in between.
  28. 28
    Darcy–Weisbach equation
    hf=fD LD v22gh_f = f_D\,\dfrac{L}{D}\,\dfrac{v^2}{2g}
    fDf_D is the Darcy friction factor, read from the Moody chart or the Colebrook equation. The Fanning factor is fF=fD/4f_F = f_D/4.
  29. 29
    Friction factor in laminar pipe flow
    fD=64Ref_D = \dfrac{64}{Re}, or in Fanning form fF=16Ref_F = \dfrac{16}{Re}
    In laminar flow it doesn’t depend on pipe roughness.
  30. 30
    Pump operating point
    Where the pump curve (head delivered vs flow) crosses the system curve (head the piping needs vs flow)
    Closing a valve steepens the system curve and moves the operating point to a lower flow.
  31. 31
    Net positive suction head (NPSH)
    The NPSH available at the pump suction must exceed the NPSH the pump requires, or the liquid boils and the pump cavitates
    NPSH available is the absolute suction head above the liquid’s vapor pressure head. Cavitation erodes the impeller.
  32. 32
    Pump affinity laws for a change in speed
    Q∝NQ \propto N,   H∝N2\;H \propto N^2,   P∝N3\;P \propto N^3
    Flow, head and power against rotational speed NN, for the same impeller.
  33. 33
    Minor loss through a valve or fitting
    hL=K v22gh_L = K\,\dfrac{v^2}{2g}
    KK is the fitting’s loss coefficient. Losses can also be given as an equivalent length of straight pipe.
  34. 34
    Log mean temperature difference (LMTD)
    ΔTlm=ΔT1−ΔT2ln⁡(ΔT1/ΔT2)\Delta T_{\text{lm}} = \dfrac{\Delta T_1 - \Delta T_2}{\ln(\Delta T_1/\Delta T_2)}
    ΔT1\Delta T_1 and ΔT2\Delta T_2 are the hot-to-cold temperature differences at the two ends of the exchanger.
  35. 35
    Heat exchanger design equation
    Q=UA ΔTlmQ = UA\,\Delta T_{\text{lm}}
    For multipass or crossflow exchangers, multiply ΔTlm\Delta T_{\text{lm}} by a correction factor F≤1F \le 1.
  36. 36
    Overall heat transfer coefficient for a thin flat wall
    1U=1hi+Δxkw+1ho\dfrac{1}{U} = \dfrac{1}{h_i} + \dfrac{\Delta x}{k_w} + \dfrac{1}{h_o}
    Resistances in series: inside film, wall (thickness Δx\Delta x, conductivity kwk_w) and outside film. For tubes, each term is scaled by its area.
  37. 37
    Fouling
    Deposits such as scale, corrosion products or biological growth on heat transfer surfaces, which add thermal resistance and lower U
    Designers add fouling resistances RfR_f to 1/U1/U, which makes the exchanger larger.
  38. 38
    Power-law rate law and reaction order
    −rA=k CAαCBβ-r_A = k\,C_A^{\alpha} C_B^{\beta}; the overall order is α+β\alpha + \beta
    Orders are found by experiment; for an elementary reaction they equal the stoichiometric coefficients.
  39. 39
    Arrhenius equation
    k=A e−Ea/RTk = A\,e^{-E_a/RT}
    AA is the pre-exponential factor and EaE_a the activation energy. A plot of ln⁡k\ln k against 1/T1/T has slope −Ea/R-E_a/R.
  40. 40
    Integrated first-order rate law at constant volume
    ln⁡CA0CA=kt\ln\dfrac{C_{A0}}{C_A} = kt
    The half-life, t1/2=ln⁡2kt_{1/2} = \dfrac{\ln 2}{k}, doesn’t depend on the starting concentration.
  41. 41
    Units of the rate constant for an nth-order reaction
    (concentration)1−n (time)−1(\text{concentration})^{1-n}\,(\text{time})^{-1}
    First order: s−1\mathrm{s^{-1}}. Second order: L mol−1 s−1\mathrm{L\,mol^{-1}\,s^{-1}}.
  42. 42
    Batch reactor design equation
    NA0 dXdt=−rAVN_{A0}\,\dfrac{dX}{dt} = -r_A V
    NA0N_{A0} is the initial moles of A and XX its conversion. Integrating gives the time to reach a given conversion.
  43. 43
    CSTR design equation
    V=FA0 X−rAV = \dfrac{F_{A0}\,X}{-r_A}
    The rate is evaluated at the exit conditions, since a perfectly mixed tank has the exit composition throughout.
  44. 44
    PFR design equation
    V=FA0∫0XdX−rAV = F_{A0}\displaystyle\int_0^X \dfrac{dX}{-r_A}
    From the differential form FA0 dXdV=−rAF_{A0}\,\dfrac{dX}{dV} = -r_A.
  45. 45
    Space time
    τ=Vv0\tau = \dfrac{V}{v_0}
    Reactor volume divided by the entering volumetric flow rate v0v_0. It equals the mean residence time when the volumetric flow is constant.
  46. 46
    CSTR vs PFR volume for a positive-order reaction
    A PFR needs less volume for the same conversion, because a CSTR runs entirely at the low exit concentration
    Several CSTRs in series approach the volume of a PFR.
  47. 47
    Feedback control
    Measure the controlled variable, compare it with the set point, and adjust a manipulated variable to reduce the error
    It can only correct a disturbance after it has affected the process.
  48. 48
    PID control law
    u(t)=uˉ+Kc[e(t)+1τI∫0te(t′) dt′+τD dedt]u(t) = \bar{u} + K_c\left[e(t) + \frac{1}{\tau_I}\int_0^t e(t')\,dt' + \tau_D\,\frac{de}{dt}\right]
    ee is the error (set point minus measurement), KcK_c the controller gain, τI\tau_I the integral (reset) time, τD\tau_D the derivative time and uˉ\bar{u} the bias.
  49. 49
    Offset in proportional-only control
    A steady-state error that remains after a set-point change or sustained disturbance; integral action removes it
    A higher proportional gain shrinks the offset but can make the loop oscillate.
  50. 50
    Controlled, manipulated and disturbance variables
    Controlled: what is held at a set point. Manipulated: what the controller adjusts. Disturbance: an input that is not adjusted but upsets the process
    Example: a tank’s temperature is controlled by adjusting steam flow, while the feed temperature is a disturbance.

Frequently asked questions

Which courses does this deck cover?

Material and energy balances, thermodynamics, separations, fluid mechanics, heat transfer, reaction engineering and an introduction to process control, as in a typical second- and third-year curriculum.

Does it use the Darcy or the Fanning friction factor?

The Darcy factor, which is four times the Fanning factor. The cards give both where it matters, so check which one your textbook and charts use.

Why are the reactor design equations written in terms of conversion?

The conversion of one reactant describes the progress of the reaction with a single variable, which makes it easy to compare reactor types and to chain reactors in series.

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