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FE Environmental formula sheet

136 key equations from 15 study topics, each with what it is for and where to look it up: the FE Reference Handbook 10.6 section, or the code or textbook when the handbook does not print it. No signup. These are the equations from the free chapters of our FE Environmental study handbook; the full handbook covers every topic at this depth, with worked examples and the traps that cost points.

136

Equations

15

Study topics

15

Concepts

Mathematics
5% of the exam

Analytic geometry and trigonometry, algebraic equations and roots, differential and integral calculus, differential equations, and numerical methods including error propagation.

Calculus and Differential Equations

Derivatives as rates and integrals as accumulated mass, maxima and minima, the fundamental theorem, and first- and second-order linear ODEs for decay, reactor, and mixing models.

Definition of the derivative
dydx=lim⁡Δx→0f(x+Δx)−f(x)Δx\dfrac{dy}{dx} = \lim_{\Delta x \to 0}\dfrac{f(x + \Delta x) - f(x)}{\Delta x}
Instantaneous rate of change / slope of y=f(x)y = f(x). In process terms, a flux or reaction rate.
Chain and product rules
ddxf(u)=f′(u)dudx,ddx(uv)=udvdx+vdudx\dfrac{d}{dx}f(u) = f'(u)\dfrac{du}{dx}, \qquad \dfrac{d}{dx}(uv) = u\dfrac{dv}{dx} + v\dfrac{du}{dx}
Differentiation of composites and products; the chain rule drives every e−kte^{-kt} derivative.
Max/min/inflection test
f′(x∗)=0;f′′<0⇒max⁡,    f′′>0⇒min⁡,    f′′=0 (sign change)⇒inflectionf'(x^\ast) = 0; \quad f''<0 \Rightarrow \max,\;\; f''>0 \Rightarrow \min,\;\; f''=0\text{ (sign change)} \Rightarrow \text{inflection}
First derivative locates stationary points; second derivative classifies them.
Fundamental theorem of calculus
∫abf(x) dx=F(b)−F(a),ddx∫axf(t) dt=f(x)\int_a^b f(x)\,dx = F(b) - F(a), \qquad \dfrac{d}{dx}\int_a^x f(t)\,dt = f(x)
Integration and differentiation are inverse operations; FF is any antiderivative of ff.
Accumulated mass (loading)
M=∫0TQ(t) C(t) dtM = \int_0^T Q(t)\,C(t)\,dt
Total mass discharged over time. QQ = flow, CC = concentration; mind unit conversion to kg or lb.
First-order decay
dCdt=−kC  ⇒  C(t)=C0e−kt\dfrac{dC}{dt} = -kC \;\Rightarrow\; C(t) = C_0 e^{-kt}
Decay/BOD/disinfection model. kk = rate constant (time−1^{-1}); time constant τ=1/k\tau = 1/k.
Half-life
t1/2=ln⁡2kt_{1/2} = \dfrac{\ln 2}{k}
Time for a first-order quantity to halve; independent of C0C_0.
CSTR transient (first-order nonhomogeneous)
C(t)=Cin(1−e−t/τ)+C0 e−t/τ,τ=VQC(t) = C_{in}\big(1 - e^{-t/\tau}\big) + C_0\,e^{-t/\tau}, \qquad \tau = \dfrac{V}{Q}
Step response of a completely mixed tank; approaches CinC_{in} as t→∞t \to \infty. τ\tau = hydraulic residence time.
Second-order characteristic equation
y′′+ay′+by=0  ⇒  r2+ar+b=0y'' + ay' + by = 0 \;\Rightarrow\; r^2 + ar + b = 0
Roots rr set the modes of the response; sign of a2−4ba^2 - 4b gives over/critical/underdamped.
Underdamped solution
y=eαx(C1cos⁡βx+C2sin⁡βx),α=−a2y = e^{\alpha x}\big(C_1\cos\beta x + C_2\sin\beta x\big), \quad \alpha = -\tfrac{a}{2}
Complex-root case (a2<4ba^2 < 4b): decaying oscillation, with β=124b−a2\beta = \tfrac{1}{2}\sqrt{4b - a^2}.

Where it lives: NCEES FE Reference Handbook — Mathematics (Differential and Integral Calculus, Differential Equations) · Metcalf & Eddy, Wastewater Engineering: Treatment and Resource Recovery · Davis & Cornwell, Introduction to Environmental Engineering

Read the Mathematics chapter

Probability and Statistics
4% of the exam

Measures of central tendency and dispersion, probability distributions, confidence intervals for a single mean, regression and curve fitting, and hypothesis testing.

Hypothesis Testing

Frame null and alternative hypotheses, run one- and two-tailed z and t tests, control Type I and II error, and decide with critical values and p-values.

z test statistic (σ known)
Z0=Xˉ−μ0σ/nZ_0=\dfrac{\bar{X}-\mu_0}{\sigma/\sqrt{n}}
Standardized distance of the sample mean from μ0\mu_0 when the population σ\sigma is known.
t test statistic (σ unknown)
t0=Xˉ−μ0s/nt_0=\dfrac{\bar{X}-\mu_0}{s/\sqrt{n}}
Same form using the sample ss; compare to tα, n−1t_{\alpha,\,n-1} or tα/2, n−1t_{\alpha/2,\,n-1}.
Two-tailed rejection (z)
reject H0 if ∣Z0∣>zα/2\text{reject } H_0 \text{ if } |Z_0|>z_{\alpha/2}
H1:μ≠μ0H_1:\mu\neq\mu_0. At α=0.05\alpha=0.05, zα/2=1.960z_{\alpha/2}=1.960.
One-tailed rejection (z)
Z0>zα  or  Z0<−zαZ_0>z_{\alpha}\ \ \text{or}\ \ Z_0<-z_{\alpha}
Upper- or lower-tail H1H_1. At α=0.05\alpha=0.05, zα=1.645z_{\alpha}=1.645.
Type I and Type II error
α=P(reject H0∣H0 true),β=P(accept H0∣H0 false)\alpha=P(\text{reject }H_0\mid H_0\ \text{true}), \quad \beta=P(\text{accept }H_0\mid H_0\ \text{false})
α\alpha = false alarm (significance level); β\beta = missed detection.
Power of the test
power=1−β\text{power}=1-\beta
Probability of correctly rejecting a false H0H_0; rises with nn and effect size.
P-value decision rule
reject H0  ⟺  p≤α\text{reject } H_0 \iff p\le\alpha
pp = probability of a statistic at least as extreme as observed, given H0H_0. Double the one-tail area for two-tailed tests.
Pooled variance (two means)
sp2=(n1−1)s12+(n2−1)s22n1+n2−2s_p^2=\dfrac{(n_1-1)s_1^2+(n_2-1)s_2^2}{n_1+n_2-2}
Combined variance estimate for comparing two means with equal variances; df =n1+n2−2=n_1+n_2-2.

Where it lives: NCEES FE Reference Handbook — Engineering Probability and Statistics · Montgomery & Runger, Applied Statistics and Probability for Engineers · Davis & Cornwell, Introduction to Environmental Engineering

Read the Probability and Statistics chapter

Ethics and Professional Practice
5% of the exam

Codes of ethics, public health, safety, and welfare, professional liability and licensure, compliance with environmental statutes (CWA, CAA, RCRA, CERCLA, SDWA, NEPA, OSHA), and the engineer's role in sustainability.

Codes of Ethics and Public Welfare

How the NCEES Model Rules put public health, safety, and welfare above client loyalty, demand competence, forbid conflicts of interest, and frame ethical dilemmas.

Hierarchy of obligation
Public H, S & W≻Employer / Client≻Other Licensees≻Self\text{Public H, S \& W} \succ \text{Employer / Client} \succ \text{Other Licensees} \succ \text{Self}
Lexical priority of the three Model Rules tiers. When duties conflict, the higher tier controls; the public's health, safety, and welfare is paramount.
Paramount-duty trigger
judgment overruled  ∧  public endangered  ⇒  notify employer/client + proper authority\text{judgment overruled} \;\wedge\; \text{public endangered} \;\Rightarrow\; \text{notify employer/client + proper authority}
Action rule from Section 240.15(A)(3): if your professional judgment is overruled in a way that endangers the public, you must notify your employer or client and an appropriate authority.
Responsible-charge / sealing rule
may seal  ⟺  (prepared by you ∨ under your responsible charge)  ∧  within competence\text{may seal} \iff (\text{prepared by you } \vee \text{ under your responsible charge}) \;\wedge\; \text{within competence}
You may sign and seal a document only if it was prepared by you or under your responsible charge and lies within your area of competence. Plan-stamping fails this test.
Conflict-of-interest test
appears to influence judgment  ⇒  disclose in writing to all parties\text{appears to influence judgment} \;\Rightarrow\; \text{disclose in writing to all parties}
The appearance standard: any interest that could influence or appear to influence professional judgment must be disclosed; gifts/gratuities from connected parties are prohibited outright.
Acceptable carcinogenic risk band
10−6≤Risk≤10−410^{-6} \le \text{Risk} \le 10^{-4}
EPA range of acceptable added individual lifetime cancer risk; the quantitative anchor for a risk-vs-benefit ethical tradeoff. Risk is dimensionless (probability).
Added cancer risk
Risk=CDI×CSF\text{Risk} = CDI \times CSF
Carcinogenic risk = chronic daily intake CDICDI (mg/(kg·day)) times cancer slope factor CSFCSF ((mg/(kg·day))−1^{-1}); Safety chapter tool used to argue 'how safe is safe enough.'
Noncarcinogen hazard index
HI=CDInoncarcRfDHI = \dfrac{CDI_{\text{noncarc}}}{RfD}
Hazard index = chronic daily intake divided by the reference dose RfDRfD (mg/(kg·day)); HI≤1HI \le 1 is considered acceptable. Both terms share units, so HIHI is dimensionless.

Where it lives: NCEES FE Reference Handbook — Ethics and Professional Practice (Model Rules Section 240.15) · NCEES FE Reference Handbook — Safety: Risk Assessment / Toxicology · NCEES Model Rules and Model Law (Rules of Professional Conduct)

Read the Ethics and Professional Practice chapter

Engineering Economics
5% of the exam

Time value of money and equivalence, cost types and breakdowns, benefit-cost, break-even, and life-cycle analyses, and project selection with depreciation and unequal lives.

Time Value of Money and Life-Cycle Cost

The interest-factor family (P/F, F/P, P/A, A/P, A/F, F/A), gradients, nominal vs effective rates, and putting capital and annual O&M on one basis for life-cycle cost.

Single-payment compound amount (F/P)
F=P (1+i)nF = P\,(1+i)^{n}
Grows a present lump sum PP to its future value FF after nn periods at periodic rate ii. Factor symbol (F/P,i%,n)(F/P,i\%,n).
Single-payment present worth (P/F)
P=F (1+i)−nP = F\,(1+i)^{-n}
Discounts a future amount FF back to the present. Reciprocal of (F/P)(F/P); the building block of all present-worth analysis.
Uniform-series present worth (P/A)
P=A (1+i)n−1i (1+i)nP = A\,\dfrac{(1+i)^{n}-1}{i\,(1+i)^{n}}
Present value of an end-of-period annuity AA for nn periods. Used to capitalize annual O&M or benefits.
Capital recovery (A/P)
A=P i (1+i)n(1+i)n−1A = P\,\dfrac{i\,(1+i)^{n}}{(1+i)^{n}-1}
Spreads a present cost PP into nn equal payments AA; this annualizes capital cost. Reciprocal of (P/A)(P/A).
Sinking fund (A/F)
A=F i(1+i)n−1A = F\,\dfrac{i}{(1+i)^{n}-1}
Equal deposits AA that accumulate to a future amount FF (e.g., a replacement reserve). Note (A/P)=(A/F)+i(A/P)=(A/F)+i.
Uniform-series compound amount (F/A)
F=A (1+i)n−1iF = A\,\dfrac{(1+i)^{n}-1}{i}
Future value of an annuity AA after nn periods. Reciprocal of (A/F)(A/F).
Gradient present worth (P/G)
P=G[(1+i)n−1i2(1+i)n−ni (1+i)n]P = G\left[\dfrac{(1+i)^{n}-1}{i^{2}(1+i)^{n}} - \dfrac{n}{i\,(1+i)^{n}}\right]
Present worth of an arithmetic gradient 0,G,2G,…,(n−1)G0,G,2G,\dots,(n-1)G. GG = constant yearly increase.
Gradient to uniform series (A/G)
A=G[1i−n(1+i)n−1]A = G\left[\dfrac{1}{i} - \dfrac{n}{(1+i)^{n}-1}\right]
Equivalent flat annuity of an arithmetic gradient. Add to a base A1A_1 to levelize a rising cost.
Effective annual interest rate
ie=(1+rm)m−1i_e = \left(1 + \dfrac{r}{m}\right)^{m} - 1
Converts nominal annual rate rr with mm compoundings/yr to the effective annual rate iei_e. m→∞m\to\infty gives ie=er−1i_e=e^{r}-1.
Equivalent uniform annual cost (EUAC)
EUAC=P (A/P,i,n)+AO&M−S (A/F,i,n)\text{EUAC} = P\,(A/P,i,n) + A_{\text{O\&M}} - S\,(A/F,i,n)
Levelized annual life-cycle cost: capital recovery plus annual O&M less salvage credit. SS = salvage at year nn.
Capitalized cost (perpetual)
P=AiP = \dfrac{A}{i}
Present worth of a uniform cost continuing forever (n→∞n\to\infty); used for permanent works and replacement-in-perpetuity comparisons.

Where it lives: NCEES FE Reference Handbook — Engineering Economics · Newnan, Lavelle & Eschenbach, Engineering Economic Analysis · Davis & Cornwell, Introduction to Environmental Engineering

Read the Engineering Economics chapter

Fundamental Principles
7% of the exam

Population projections and water, wastewater, and solid-waste demand calculations, ideal reactor models (CSTR, batch, plug flow), and materials science including properties and corrosion.

Ideal Reactors: Batch, CSTR, and Plug Flow

The three ideal reactors, the general mass balance, hydraulic residence time, and why a PFR always beats a CSTR for first-order conversion.

General mass balance (constant V)
VdCdt=Q C0−Q C+rAVV\dfrac{dC}{dt} = Q\,C_0 - Q\,C + r_A V
Accumulation = in − out + generation. rA<0r_A<0 for a consumed reactant; set the left side to zero for steady state.
Batch reactor, first order
CA=CA0 e−ktC_A = C_{A0}\,e^{-kt}
No flow; concentration decays with reaction time tt. kk in time−1\text{time}^{-1}.
CSTR design equation
V=Q (C0−C)−rAV = \dfrac{Q\,(C_0 - C)}{-r_A}
−rA-r_A evaluated at EXIT (tank) conditions. VV = volume, QQ = volumetric flow.
CSTR, first order
CC0=11+kτ\dfrac{C}{C_0} = \dfrac{1}{1 + k\tau}
Fraction remaining for a single completely-mixed tank; τ=V/Q\tau=V/Q.
PFR design integral
τ=−∫C0CdC−rA\tau = -\int_{C_0}^{C}\dfrac{dC}{-r_A}
Each slice acts as a batch element; reduces to e−kτe^{-k\tau} for first order.
PFR, first order
CC0=e−kτ\dfrac{C}{C_0} = e^{-k\tau}
Fraction remaining for plug flow; identical to a batch reactor with t=τt=\tau.
Hydraulic residence time
τ=VQ\tau = \dfrac{V}{Q}
Mean detention time (space-time). Reciprocal is space-velocity SV=1/τSV=1/\tau.
Zero-order conversion
C=C0−kτ(CSTR or PFR)C = C_0 - k\tau \quad (\text{CSTR or PFR})
For a zero-order reaction the rate is constant, so CSTR and PFR give the SAME effluent; kk in mass/(vol·time).
Damköhler number
Da=kτDa = k\tau
Dimensionless ratio of reaction rate to throughput; governs conversion in both continuous reactors.

Where it lives: NCEES FE Reference Handbook — Chemical Engineering (Reactor Design; Flow Reactors, Steady State) · NCEES FE Reference Handbook — Environmental Engineering (hydraulic residence time) · Metcalf & Eddy, Wastewater Engineering: Treatment and Resource Recovery · Davis & Cornwell, Introduction to Environmental Engineering

Read the Fundamental Principles chapter

Environmental Chemistry
7% of the exam

Stoichiometry and chemical equilibrium, acid-base and oxidation-reduction reactions, pC-pH diagrams, reaction kinetics, organic chemistry, and multimedia partitioning by Henry's law and the octanol-water coefficient.

Chemical Equilibrium, Acids–Bases, and pH

Balance reactions and find limiting reactants, then use the equilibrium constant, Kw, and pKa to predict pH, buffering, and as-CaCO3 equivalents.

Moles from mass
n=mMn = \dfrac{m}{M}
nn = moles, mm = mass (g), MM = molar mass (g/mol). The starting point of every stoichiometry problem.
Equilibrium constant
Keq=[C]c[D]d[A]a[B]bK_{eq} = \dfrac{[C]^{c}[D]^{d}}{[A]^{a}[B]^{b}}
Ratio of product to reactant activities for aA+bB⇌cC+dDaA+bB\rightleftharpoons cC+dD; pure solids/liquids count as 1. Dimensionless in concentration form here.
Ion product of water
Kw=[H+][OH−]=1.0×10−14K_w = [\text{H}^+][\text{OH}^-] = 1.0\times10^{-14}
At 25∘C25^\circ\text{C}. Fixes [OH−][\text{OH}^-] once [H+][\text{H}^+] is known (mol/L).
pH and pOH
pH=−log⁡10[H+],pH+pOH=14\text{pH} = -\log_{10}[\text{H}^+], \quad \text{pH}+\text{pOH}=14
[H+][\text{H}^+] in mol/L. Acids: pH < 7; bases: pH > 7 at 25∘C25^\circ\text{C}.
Acid dissociation constant
Ka=[H+][A−][HA],pKa=−log⁡10KaK_a = \dfrac{[\text{H}^+][\text{A}^-]}{[\text{HA}]}, \quad \text{p}K_a = -\log_{10}K_a
Strength of a weak acid HA. Larger KaK_a (smaller pKa\text{p}K_a) = stronger acid.
Weak-acid pH approximation
[H+]≈Ka Ca[\text{H}^+] \approx \sqrt{K_a\,C_a}
CaC_a = analytical acid concentration (mol/L). Valid when dissociation is < ~5% of CaC_a.
Henderson–Hasselbalch
pH=pKa+log⁡10 ⁣[A−][HA]\text{pH} = \text{p}K_a + \log_{10}\!\dfrac{[\text{A}^-]}{[\text{HA}]}
Buffer pH from the conjugate base-to-acid ratio. pH=pKa\text{pH}=\text{p}K_a when the two are equal.
Solubility product
Ksp=[A+]m[B−]nK_{sp} = [\text{A}^{+}]^{m}[\text{B}^{-}]^{n}
For AmBn(s)⇌mA++nB−\text{A}_m\text{B}_n(s)\rightleftharpoons m\text{A}^{+}+n\text{B}^{-}. Precipitation occurs when the ion product exceeds KspK_{sp}.
Equivalent weight and normality
EW=MWz,N=M zEW = \dfrac{\mathrm{MW}}{z}, \qquad N = M\,z
MW\mathrm{MW} = molar mass (g/mol); MM = molarity (mol/L); zz = charge or protons exchanged per mole. Equivalent weight (g/eq) is the basis for the as-CaCO3 system; normality N=M×zN = M\times z.
Conversion to as-CaCO3
Cas CaCO3=Cspecies×50EWspeciesC_{\text{as CaCO}_3} = C_{species}\times\dfrac{50}{EW_{species}}
EW(CaCO3)=50EW(\text{CaCO}_3)=50 g/eq. Use to add hardness/alkalinity ions on a common basis (mg/L as CaCO3).
Alkalinity (carbonate system)
Alk=[HCO3−]+2[CO32−]+[OH−]−[H+]\text{Alk} = [\text{HCO}_3^-] + 2[\text{CO}_3^{2-}] + [\text{OH}^-] - [\text{H}^+]
Acid-neutralizing capacity in eq/L; multiply by 50,00050{,}000 to express as mg/L as CaCO3.

Where it lives: NCEES FE Reference Handbook — Chemistry and Biology · NCEES FE Reference Handbook — Environmental Engineering (equivalent-weight / common radicals table) · Davis & Cornwell, Introduction to Environmental Engineering · Sawyer, McCarty & Parkin, Chemistry for Environmental Engineering and Science · Snoeyink & Jenkins, Water Chemistry

Read the Environmental Chemistry chapter

Health Hazards and Risk Assessment
4% of the exam

Dose-response toxicity for carcinogens and noncarcinogens, exposure routes and pathways and chronic daily intake, and occupational health including PPE and noise exposure.

Dose–Response Toxicity (Carcinogens and Noncarcinogens)

How a contaminant dose becomes a quantified health risk along two NCEES tracks: linear-no-threshold cancer risk (Risk = CDI×CSF) and the noncancer hazard quotient (HI = CDI/RfD).

Cancer risk (linear, no threshold)
Risk=CDI×CSF\text{Risk} = \text{CDI}\times\text{CSF}
Excess lifetime cancer probability (dimensionless). CDI = chronic daily intake in mg/(kg⋅day)\text{mg}/(\text{kg}\cdot\text{day}); CSF = cancer slope factor in [mg/(kg⋅day)]−1[\text{mg}/(\text{kg}\cdot\text{day})]^{-1}. Acceptable EPA range 10−610^{-6} to 10−410^{-4}.
Hazard quotient
HQ=CDIRfD\text{HQ} = \dfrac{\text{CDI}}{\text{RfD}}
Fraction of the safe dose received for one noncarcinogen and pathway (dimensionless). RfD = reference dose in mg/(kg⋅day)\text{mg}/(\text{kg}\cdot\text{day}).
Hazard index
HI=∑iCDIiRfDi\text{HI} = \sum_i \dfrac{\text{CDI}_i}{\text{RfD}_i}
Sum of hazard quotients over all noncarcinogens and routes. HI>1.0\text{HI}>1.0 indicates possible adverse effect.
Reference dose from NOAEL
RfD=NOAELUF\text{RfD} = \dfrac{\text{NOAEL}}{\text{UF}}
Chronic safe daily dose, mg/(kg⋅day)\text{mg}/(\text{kg}\cdot\text{day}). NOAEL = no-observed-adverse-effect level from the animal dose-response curve; UF = total uncertainty factor (often 1010–10,00010{,}000).
Safe human dose
SHD=RfD⋅W=NOAEL⋅WUF\text{SHD} = \text{RfD}\cdot W = \dfrac{\text{NOAEL}\cdot W}{\text{UF}}
Allowable daily intake in mg/day\text{mg}/\text{day} for a person of body weight WW (kg).
Median lethal dose / concentration
LD50, LC50\text{LD}_{50},\ \text{LC}_{50}
Dose (mg/kg\text{mg}/\text{kg}) or air concentration killing 50%50\% of test animals. Smaller value = more toxic. LD10/LC10\text{LD}_{10}/\text{LC}_{10} defined at 10%10\%.
Hazard index pass/fail
HI≤1.0 ⇒ acceptable,HI>1.0 ⇒ possible adverse effect\text{HI} \le 1.0 \ \Rightarrow\ \text{acceptable}, \qquad \text{HI} > 1.0 \ \Rightarrow\ \text{possible adverse effect}
EPA decision rule for noncarcinogenic risk characterization.
Acceptable carcinogenic risk band
10−6≤Risk≤10−410^{-6} \le \text{Risk} \le 10^{-4}
EPA range for incremental lifetime cancer risk used in site cleanup decisions.

Where it lives: NCEES FE Reference Handbook — Safety (Risk Assessment/Toxicology) · EPA, Risk Assessment Guidance for Superfund, Vol. I (Human Health Evaluation Manual, Part A) · Davis & Cornwell, Introduction to Environmental Engineering

Read the Health Hazards and Risk Assessment chapter

Fluid Mechanics and Hydraulics
12% of the exam

Fluid statics, closed-conduit flow (Darcy-Weisbach, Hazen-Williams, Moody), open-channel flow (Manning), pumps and blowers, flow measurement with weirs and orifices, and the Bernoulli and continuity equations.

Continuity, Bernoulli, and the Energy Equation

Conservation of mass and energy along a streamline, the head form with pump, turbine, and friction terms, EGL/HGL, and the impulse-momentum principle.

Continuity (volumetric)
Q=A1v1=A2v2Q = A_1 v_1 = A_2 v_2
Incompressible steady flow; QQ in m3^3/s, AA in m2^2, vv in m/s. Velocity rises where area shrinks.
Continuity (mass)
m˙=ρAv=constant\dot m = \rho A v = \text{constant}
General steady form; use when density changes (gas/air streams), m˙\dot m in kg/s.
Energy equation (head form)
p1γ+v122g+z1+hp=p2γ+v222g+z2+ht+hf\frac{p_1}{\gamma} + \frac{v_1^2}{2g} + z_1 + h_p = \frac{p_2}{\gamma} + \frac{v_2^2}{2g} + z_2 + h_t + h_f
Each term a length; hph_p pump head added, hth_t turbine head removed, hfh_f friction + minor losses.
Bernoulli equation
pγ+v22g+z=constant\frac{p}{\gamma} + \frac{v^2}{2g} + z = \text{constant}
Frictionless, no machine, along a streamline. Use for nozzles, venturis, tank efflux.
Velocity head
hv=v22gh_v = \frac{v^2}{2g}
Kinetic energy per unit weight; the vertical gap between EGL and HGL (m or ft).
Pressure-head / pressure relation
p1−p2=γ hf=ρg hfp_1 - p_2 = \gamma\,h_f = \rho g\,h_f
Pressure drop in a horizontal constant-area pipe equals the friction head times specific weight.
Pump head and fluid power
W˙fluid=γQhp,W˙brake=γQhpη\dot W_{\text{fluid}} = \gamma Q h_p, \qquad \dot W_{\text{brake}} = \frac{\gamma Q h_p}{\eta}
Fluid (hydraulic) power vs. shaft/brake power; η\eta is pump efficiency (0-1).
Impulse-momentum
ΣF=ρQ (vout−vin)\Sigma F = \rho Q\,(v_{\text{out}} - v_{\text{in}})
Per direction; gives force on bends, nozzles, plates. Include pApA pressure forces on bends.
Force of a jet on a fixed plate
F=ρQvF = \rho Q v
Normal flat plate stops the jet (vout=0v_{\text{out}}=0 in flow direction); FF in N.

Where it lives: NCEES FE Reference Handbook — Fluid Mechanics · NCEES FE Reference Handbook — Civil Engineering · Munson, Young & Okiishi, Fundamentals of Fluid Mechanics

Read the Fluid Mechanics and Hydraulics chapter

Thermodynamics
3% of the exam

First and second laws, energy, heat, and work, efficiencies and coefficient of performance, conduction, convection, and radiation heat transfer, and the behavior of ideal gases.

Thermodynamic Laws, Efficiency, and COP

The first and second laws, the Carnot absolute-temperature ceiling, refrigeration and heat-pump COP, and the one-way direction of entropy.

First law for a cycle
QH=W+QLQ_H = W + Q_L
Over one complete cycle internal energy returns to its start; heat in equals net work plus heat rejected. Energies in consistent units (J, kJ, or W for rates).
Sensible-heat rate (first law, flowing stream)
Q˙=m˙ cp ΔT\dot{Q} = \dot{m}\,c_p\,\Delta T
m˙\dot{m} = mass flow (kg/s), cpc_p = specific heat (J/kg·K), ΔT=Tout−Tin\Delta T = T_{out}-T_{in} (K or °C, same magnitude). Gives rate in W.
Thermal efficiency
η=WQH=1−QLQH\eta = \frac{W}{Q_H} = 1 - \frac{Q_L}{Q_H}
Fraction of input heat converted to net work. Denominator is the heat supplied QHQ_H, never WW.
Carnot (maximum) efficiency
ηCarnot=1−TLTH\eta_{Carnot} = 1 - \frac{T_L}{T_H}
Upper bound for any engine between reservoirs at absolute temperatures THT_H and TLT_L (K or °R). No real engine can exceed it.
Second-law (exergetic) efficiency
ηII=ηactualηCarnot\eta_{II} = \frac{\eta_{actual}}{\eta_{Carnot}}
How close a real device comes to the reversible ideal; dimensionless, always < 1 for real machines.
Refrigeration COP
COPref=QLW\mathrm{COP}_{ref} = \frac{Q_L}{W}
Useful cooling (heat removed from cold space QLQ_L) per unit work input. For refrigerators and air conditioners.
Heat-pump COP
COPHP=QHW=COPref+1\mathrm{COP}_{HP} = \frac{Q_H}{W} = \mathrm{COP}_{ref} + 1
Useful heating (heat delivered to warm space QHQ_H) per unit work input.
Carnot COP ceilings
COPHP,max⁡=THTH−TL,COPref,max⁡=TLTH−TL\mathrm{COP}_{HP,\max} = \frac{T_H}{T_H-T_L}, \quad \mathrm{COP}_{ref,\max} = \frac{T_L}{T_H-T_L}
Maximum COP from a reversed-Carnot cycle; absolute temperatures only.
Increase-of-entropy principle
ΔStotal=ΔSsys+ΔSsurr≥0\Delta S_{total} = \Delta S_{sys} + \Delta S_{surr} \ge 0
Total entropy never decreases; equality only for a reversible process. Fixes the hot-to-cold direction of spontaneous heat flow.
Reservoir entropy change
ΔSres=QTres\Delta S_{res} = \frac{Q}{T_{res}}
Entropy change of a thermal reservoir exchanging heat QQ at constant absolute temperature TresT_{res} (J/K).

Where it lives: NCEES FE Reference Handbook — Thermodynamics · Moran, Shapiro, Boettner & Bailey, Fundamentals of Engineering Thermodynamics · Davis & Cornwell, Introduction to Environmental Engineering

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Surface Water Resources and Hydrology
9% of the exam

Runoff and the rational method, time of concentration and IDF curves, detention and retention storage sizing, channel and reservoir routing, water-quality modeling (Streeter-Phelps, eutrophication), and the water budget.

The Streeter–Phelps Dissolved-Oxygen Sag

Model the dissolved-oxygen sag below a BOD outfall: deoxygenation vs reaeration, the deficit equation, the critical point, temperature correction, and nutrient limitation.

BOD exertion (first-order)
BODt=Lo(1−e−kt)\text{BOD}_t = L_o\left(1 - e^{-k t}\right)
Oxygen demand exerted by time tt (days); LoL_o = ultimate BOD (mg/L), kk = base-ee decay constant (d−1^{-1}). A base-10 KK relates as k=2.303 Kk = 2.303\,K.
Mixed (initial) ultimate BOD
La=QrLr+QwLwQr+QwL_a = \dfrac{Q_r L_r + Q_w L_w}{Q_r + Q_w}
Flow-weighted ultimate BOD entering the reach; QQ = flow, LL = ultimate BOD, subscripts rr = river, ww = waste.
Initial DO deficit
Da=DOsat−Qr DOr+Qw DOwQr+QwD_a = \text{DO}_{sat} - \dfrac{Q_r\,\text{DO}_r + Q_w\,\text{DO}_w}{Q_r + Q_w}
Saturation DO minus the flow-weighted mixed DO (mg/L) at the outfall; the deficit the reach starts with.
Streeter–Phelps deficit
D=kdLakr−kd(e−kdt−e−krt)+Da e−krtD = \dfrac{k_d L_a}{k_r - k_d}\left(e^{-k_d t} - e^{-k_r t}\right) + D_a\,e^{-k_r t}
DO deficit (mg/L) at travel time tt (days). kdk_d = deoxygenation, krk_r = reaeration (both base-ee, d−1^{-1}). Then DO=DOsat−D\text{DO} = \text{DO}_{sat} - D.
Critical time
tc=1kr−kdln⁡ ⁣[krkd(1−Da (kr−kd)kd La)]t_c = \dfrac{1}{k_r - k_d}\ln\!\left[\dfrac{k_r}{k_d}\left(1 - \dfrac{D_a\,(k_r - k_d)}{k_d\,L_a}\right)\right]
Travel time (days) to the minimum DO, where dD/dt=0dD/dt = 0. Requires kr≠kdk_r \ne k_d.
Critical deficit
Dc=kdkr La e−kdtcD_c = \dfrac{k_d}{k_r}\,L_a\,e^{-k_d t_c}
Maximum DO deficit (mg/L), at tct_c. Minimum dissolved oxygen is DOmin=DOsat−Dc\text{DO}_{min} = \text{DO}_{sat} - D_c.
Temperature correction
kT=k20 θ T−20k_T = k_{20}\,\theta^{\,T-20}
Rate constant at stream temperature TT (∘^\circC). θkd=1.135\theta_{k_d} = 1.135 (4–20°C) or 1.0561.056 (21–30°C); θkr=1.024\theta_{k_r} = 1.024.
Mass loading
M (lb/day)=C (mg/L)×Q (MGD)×8.34M\,(\text{lb/day}) = C\,(\text{mg/L}) \times Q\,(\text{MGD}) \times 8.34
Converts a concentration and flow to a daily mass load; the 8.348.34 factor carries units lb·L/(mg·MG). Used to set BOD load limits.

Where it lives: NCEES FE Reference Handbook — Environmental Engineering: Stream Modeling (Streeter–Phelps) · NCEES FE Reference Handbook — Environmental Engineering: Kinetic Temperature Corrections · Davis & Cornwell, Introduction to Environmental Engineering · Clean Water Act (CWA)

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Groundwater, Soils, and Sediments
8% of the exam

Aquifer properties and hydrogeology, Darcy's law and seepage velocity, well drawdown (Theis, Jacob, Thiem, Dupuit), and soil, sediment, and groundwater remediation.

Darcy’s Law and Seepage Velocity

Darcy’s law, hydraulic conductivity, transmissivity and storativity, and the crucial gap between the Darcy flux and the seepage velocity a contaminant actually travels at.

Darcy’s law (discharge)
Q=−KA dhdxQ = -KA\,\dfrac{dh}{dx}
QQ = volumetric discharge (m³/s, ft³/s); KK = hydraulic conductivity (m/s, ft/s); AA = total cross-sectional area; dh/dxdh/dx = hydraulic gradient. Minus sign: flow goes down-gradient.
Specific discharge (Darcy flux)
q=QA=−K dhdx=K iq = \dfrac{Q}{A} = -K\,\dfrac{dh}{dx} = K\,i
Discharge per unit total area; units of velocity but NOT a particle speed. Use for flux/mass-loading. i=−dh/dxi = -dh/dx is the gradient (dimensionless).
Seepage (pore) velocity
v=qne=K inev = \dfrac{q}{n_e} = \dfrac{K\,i}{n_e}
Actual average water velocity through the interconnected pores; nen_e = effective porosity. This is the velocity for travel-time and plume problems.
Hydraulic gradient
i=−dhdx=h1−h2Li = -\dfrac{dh}{dx} = \dfrac{h_1 - h_2}{L}
Head drop per unit distance along the flow path, dimensionless. Use consistent length units for head and distance.
Transmissivity
T=K bT = K\,b
Conductivity times saturated thickness bb; units L2/TL^2/T (m²/d, ft²/s). Aquifer-scale measure of water-transmitting capacity.
Aquifer discharge through a width
Q=T i w=K b i wQ = T\,i\,w = K\,b\,i\,w
Discharge through a vertical strip of aquifer of width ww and thickness bb; folds thickness into TT.
Storativity (storage coefficient)
S=Ss b(confined),S≈Sy(unconfined)S = S_s\,b \quad (\text{confined}), \qquad S \approx S_y \quad (\text{unconfined})
Volume released per unit area per unit head drop, dimensionless. Confined S∼10−5–10−3S \sim 10^{-5}\text{–}10^{-3}; unconfined S≈Sy∼0.05–0.30S \approx S_y \sim 0.05\text{–}0.30.
Travel time
t=Lv=L neK it = \dfrac{L}{v} = \dfrac{L\,n_e}{K\,i}
Time for water (or a non-sorbing tracer) to travel distance LL at the seepage velocity. Uses nen_e, not qq.

Where it lives: NCEES FE Reference Handbook — Civil Engineering: Darcy's Law, Transmissivity, Storativity · Fetter, Applied Hydrogeology · Davis & Cornwell, Introduction to Environmental Engineering

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Water and Wastewater
12% of the exam

Water and wastewater characteristics, mass balance and removal-efficiency loading rates, physical, chemical, and biological treatment processes, sludge treatment and handling, and water conservation and reuse.

Activated Sludge: F/M, SRT, and Clarifiers

The workhorse of biological wastewater treatment, sized by F/M and solids retention time, balanced across the aeration basin and coupled secondary clarifier.

Food-to-microorganism ratio
F/M=Q0 S0V XA\text{F/M} = \dfrac{Q_0\,S_0}{V\,X_A}
Applied BOD load per unit biomass per day (kg BOD/(kg MLSS·d)). Q0Q_0=influent flow, S0S_0=influent BOD, VV=basin volume, XAX_A=MLSS. Conventional 0.2–0.4.
Solids retention time (SRT)
θc=V XAQwXw+QeXe\theta_c = \dfrac{V\,X_A}{Q_w X_w + Q_e X_e}
Mean cell residence time / sludge age (d). Basin solids inventory divided by solids leaving in waste + effluent.
Hydraulic retention time
θ=VQ\theta = \dfrac{V}{Q}
Liquid residence time in the basin (h). Typically 4–8 h for conventional activated sludge; distinct from SRT.
Biomass concentration (kinetics)
XA=θc Y (S0−Se)θ (1+kd θc)X_A = \dfrac{\theta_c\,Y\,(S_0 - S_e)}{\theta\,(1 + k_d\,\theta_c)}
Design MLSS from kinetics. YY=yield (kg VSS/kg BOD), kdk_d=decay rate (d⁻¹), SeS_e=effluent BOD.
Clarifier solids mass balance
(Q0+QR) XA=QeXe+QRXr+QwXw(Q_0 + Q_R)\,X_A = Q_e X_e + Q_R X_r + Q_w X_w
Steady-state solids around the secondary clarifier. XrX_r=RAS (underflow) solids, XwX_w=waste solids, XeX_e=effluent SS.
Recycle ratio
R=QRQ0=XAXr−XAR = \dfrac{Q_R}{Q_0} = \dfrac{X_A}{X_r - X_A}
Return-sludge ratio to hold target MLSS (right form neglects effluent/waste solids). Typically 0.25–1.0.
Sludge volume index
SVI=V30 (mL/L)×1000XMLSS (mg/L)\text{SVI} = \dfrac{V_{30}\,(\text{mL/L})\times 1000}{X_{\text{MLSS}}\,(\text{mg/L})}
Volume (mL) of 1 g settled solids after 30 min. <100 good settling, >150 bulking. Underflow Xr ≈ 10⁶/SVI.
Solids loading rate
SLR=(Q0+QR) XAA\text{SLR} = \dfrac{(Q_0 + Q_R)\,X_A}{A}
Thickening criterion for the secondary clarifier (kg/(m²·d) or lb/(ft²·d)); often controls over overflow rate.
Volumetric organic loading
Lv=Q0 S0VL_v = \dfrac{Q_0\,S_0}{V}
BOD load per basin volume (kg BOD/(m³·d)). Conventional ~0.3–0.6.

Where it lives: NCEES FE Reference Handbook — Environmental Engineering · Metcalf & Eddy, Wastewater Engineering: Treatment and Resource Recovery · Davis & Cornwell, Introduction to Environmental Engineering

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Air Quality and Control
8% of the exam

Ambient and indoor air quality, mass and energy balances, emission factors and rates, atmospheric dispersion and stability classes, and gas and particulate control technologies.

The Gaussian Plume and Atmospheric Stability

Predict downwind ground-level concentrations from an elevated source using the Gaussian dispersion model, Pasquill stability classes, effective stack height, and the lapse rate.

Gaussian plume (general)
C=Q2πuσyσzexp⁡ ⁣(−y22σy2) ⁣[exp⁡ ⁣(−(z−H)22σz2)+exp⁡ ⁣(−(z+H)22σz2)]C = \dfrac{Q}{2\pi u \sigma_y \sigma_z}\exp\!\left(-\dfrac{y^2}{2\sigma_y^2}\right)\!\left[\exp\!\left(-\dfrac{(z-H)^2}{2\sigma_z^2}\right)+\exp\!\left(-\dfrac{(z+H)^2}{2\sigma_z^2}\right)\right]
Concentration CC (μg/m3\mu\text{g/m}^3) at (x,y,z)(x,y,z) from a continuous elevated point source. QQ in μg/s\mu\text{g/s}, uu in m/s, σy,σz\sigma_y,\sigma_z in m, HH effective stack height in m.
Ground-level, centerline concentration
C(x,0,0)=Qπuσyσzexp⁡ ⁣(−H22σz2)C(x,0,0) = \dfrac{Q}{\pi u \sigma_y \sigma_z}\exp\!\left(-\dfrac{H^2}{2\sigma_z^2}\right)
Set z=0z=0 (ground reflection doubles the term) and y=0y=0 (on centerline). The everyday working form for worst-case ground exposure.
Effective stack height
H=h+ΔhH = h + \Delta h
hh = physical stack height (m), Δh\Delta h = plume rise (m) from buoyancy and exit momentum. Always use HH, not hh, in the dispersion equation.
Maximum ground-level concentration
Cmax⁡=Qπe u σyσz,at σz=H2C_{\max} = \dfrac{Q}{\pi e\, u\, \sigma_y \sigma_z}, \qquad \text{at } \sigma_z = \dfrac{H}{\sqrt{2}}
Peak ground concentration downwind for neutral atmospheric conditions (the handbook's stated case); the exponential becomes e−1e^{-1} when σz=H/2\sigma_z=H/\sqrt2. Other stability classes: the handbook's (Cu/Q)max⁡(Cu/Q)_{\max} chart. Evaluate σy\sigma_y at that same xx.
Lapse rate
Γ=−ΔTΔz,ΓAD=0.98 ∘C/100 m\Gamma = -\dfrac{\Delta T}{\Delta z}, \qquad \Gamma_{AD} = 0.98\,^\circ\text{C}/100\,\text{m}
Environmental lapse rate Γ\Gamma versus dry adiabatic ΓAD\Gamma_{AD}. ΔT\Delta T = temperature change, Δz\Delta z = elevation change.
Stability criterion
Γ>ΓAD ⇒ unstable;Γ=ΓAD ⇒ neutral;Γ<ΓAD ⇒ stable\Gamma > \Gamma_{AD}\ \Rightarrow\ \text{unstable}; \quad \Gamma = \Gamma_{AD}\ \Rightarrow\ \text{neutral}; \quad \Gamma < \Gamma_{AD}\ \Rightarrow\ \text{stable}
Inversion (Γ<0\Gamma<0) is the strongly stable limit that caps mixing and traps the plume.
ppb / concentration conversion
ppb=(μg/m3) RTP MW\text{ppb} = \dfrac{(\mu\text{g/m}^3)\,RT}{P\,\text{MW}}
Convert mass concentration to volume mixing ratio. R=0.0821 L⋅atm/(mol⋅K)R=0.0821\,\text{L·atm/(mol·K)}, TT in K, PP in atm, MW in g/mol.

Where it lives: NCEES FE Reference Handbook — Environmental Engineering · Turner, Workbook of Atmospheric Dispersion Estimates · Davis & Cornwell, Introduction to Environmental Engineering

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Solid and Hazardous Waste
7% of the exam

Solid waste management, collection, and disposal, landfill leachate and gas, mass and energy balances, hazardous waste compatibility, site characterization, and waste treatment and disposal.

Landfills: Airspace, Leachate, and Gas

Size landfill airspace from compacted density and compaction ratio, estimate leachate by water balance, predict landfill gas from anaerobic stoichiometry, and value MSW as fuel.

Airspace from compacted density
V=MρcV = \dfrac{M}{\rho_c}
Volume of airspace a waste mass MM consumes; ρc\rho_c = in-place compacted density (≈1,000\approx 1{,}000–1,400 lb/yd31{,}400\,\text{lb/yd}^3). Use compacted, never loose, density.
Compaction ratio
CR=VlooseVcompacted=ρcρlooseCR = \dfrac{V_{loose}}{V_{compacted}} = \dfrac{\rho_c}{\rho_{loose}}
How many loose volumes collapse into one compacted volume; about 44–88 from curbside-loose to in-place landfill density. Dimensionless.
Volume reduction
VR=Vi−VfVi×100%VR = \dfrac{V_i - V_f}{V_i}\times 100\%
Percent volume saved by compaction or baling; ViV_i initial (loose), VfV_f final (compacted). Related to CRCR by VR=1−1/CRVR = 1 - 1/CR.
Overburden specific weight
SWp=SWi+pa+b pSW_p = SW_i + \dfrac{p}{a + b\,p}
In-place specific weight (lb/yd3\text{lb/yd}^3) at overburden pressure pp (lb/in2\text{lb/in}^2); SWiSW_i initial compacted (≈1,000\approx 1{,}000), a,ba,b empirical constants.
Site life
L=VairspaceV˙waste+V˙coverL = \dfrac{V_{airspace}}{\dot V_{waste} + \dot V_{cover}}
Years of capacity = permitted airspace divided by annual airspace consumed by compacted waste plus cover soil.
Cover water balance (percolation)
PERsw=P−R−ET−ΔSLCPER_{sw} = P - R - ET - \Delta S_{LC}
Leachate percolation (in.) = precipitation −- runoff −- evapotranspiration −- change in cover-soil storage. At field capacity ΔSLC→0\Delta S_{LC}\to 0.
Clay-liner breakthrough time
t=d2 ηK (d+h)t = \dfrac{d^{2}\,\eta}{K\,(d + h)}
Years for leachate to penetrate a clay liner; dd thickness (ft), η\eta porosity, KK hydraulic conductivity (ft/yr), hh leachate head (ft).
Anaerobic stabilization (Buswell)
m=4a+b−2c−3d8,s=4a−b+2c+3d8m = \dfrac{4a + b - 2c - 3d}{8}, \quad s = \dfrac{4a - b + 2c + 3d}{8}
Methane (mm) and carbon-dioxide (ss) moles from complete stabilization of CaHbOcNd\mathrm{C_aH_bO_cN_d}. Ammonia coefficient =d= d; water r=(4a−b−2c+3d)/4r = (4a - b - 2c + 3d)/4.
First-order gas generation
QCH4=k L0 M e−k tQ_{CH_4} = k\,L_0\,M\,e^{-k\,t}
Methane rate from a waste mass MM; L0L_0 = methane potential (m3/Mg\text{m}^3/\text{Mg}), kk = decay constant (yr−1\text{yr}^{-1}), tt = age. Basis of EPA LandGEM.
Gas flux through cover (Fick)
NA=D ηgas4/3 CA,fill−CA,atmLN_A = D\,\eta_{gas}^{4/3}\,\dfrac{C_{A,fill} - C_{A,atm}}{L}
Diffusive (outward) flux of gas AA through cover of depth LL; DD diffusion coefficient, ηgas\eta_{gas} gas-filled porosity (the ηgas4/3\eta_{gas}^{4/3} factor is the porosity (tortuosity) correction that converts the free-gas diffusion coefficient DD into the effective diffusivity D ηgas4/3D\,\eta_{gas}^{4/3}). Writing the driving force as Cfill−CatmC_{fill}-C_{atm} makes outward flux positive.
Modified Dulong heating value
HHV=145 C+610(H−O8)+40 S+10 NHHV = 145\,C + 610\left(H - \tfrac{O}{8}\right) + 40\,S + 10\,N
Higher heating value (Btu/lb) from ultimate-analysis mass percents C,H,O,S,NC,H,O,S,N. The O/8O/8 term removes hydrogen already bound as water.

Where it lives: NCEES FE Reference Handbook — Environmental Engineering · NCEES FE Reference Handbook — Chemistry and Biology · Tchobanoglous, Theisen & Vigil, Integrated Solid Waste Management · U.S. EPA LandGEM, Landfill Gas Emissions Model

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Energy and Environment
4% of the exam

Conventional and alternative energy source concepts and the environmental impacts of energy production, including greenhouse gas emissions, carbon footprint, and thermal and water demands.

Greenhouse Gases and Carbon Footprint

Normalize greenhouse gases to CO2-equivalent via global warming potential, account for emissions with emission factors and life-cycle energy, and quantify the thermal/water burden of power production.

Carbon-dioxide equivalent
CO2e=∑imi GWPi\text{CO}_2e = \sum_i m_i\,GWP_i
Common-scale total of a gas mixture; mim_i = mass of gas ii (any consistent unit), GWPiGWP_i = its global warming potential (dimensionless, 100-yr: CO2 1\text{CO}_2\,1, CH4 28\text{CH}_4\,28, N2O 265\text{N}_2\text{O}\,265).
Carbon footprint by emission factor
ECO2e=∑jAj EFjE_{\text{CO}_2e} = \sum_j A_j\,EF_j
Total emissions from activities; AjA_j = activity (kWh, L, km), EFjEF_j = emission factor (mass CO2e\text{CO}_2e per unit activity).
Carbon-to-CO2 mass ratio
mCO2=4412 mC=3.67 mCm_{\text{CO}_2} = \frac{44}{12}\,m_{\text{C}} = 3.67\,m_{\text{C}}
Every fuel carbon atom becomes one CO2\text{CO}_2; molar masses 4444 and 12 g/mol12\ \text{g/mol}. For methane, mCO2=2.75 mCH4m_{\text{CO}_2}=2.75\,m_{\text{CH}_4} (44/1644/16).
Methane combustion
CH4+2 O2→CO2+2 H2O\text{CH}_4 + 2\,\text{O}_2 \to \text{CO}_2 + 2\,\text{H}_2\text{O}
Stoichiometric complete combustion (FE Handbook, Thermodynamics — Combustion Processes); basis for the natural-gas carbon factor.
Heat-engine (thermal) efficiency
η=WQH=QH−QLQH\eta = \frac{W}{Q_H} = \frac{Q_H - Q_L}{Q_H}
Fraction of fuel heat QHQ_H converted to work/electricity WW; QLQ_L = rejected heat. Handbook, Thermodynamics — Basic Cycles.
Carnot efficiency limit
ηc=1−TLTH\eta_c = 1 - \frac{T_L}{T_H}
Upper bound on any heat engine between absolute temperatures THT_H and TLT_L (K or R). Real plants reach a fraction of this.
Rejected (waste) heat
Qrej=P(1η−1)Q_{rej} = P\left(\frac{1}{\eta}-1\right)
Low-grade heat dumped per unit electrical output PP; fuel input is QH=P/ηQ_H = P/\eta.
Cooling-water energy balance
Qrej=m˙ cp ΔT=ρ Q cp ΔTQ_{rej} = \dot{m}\,c_p\,\Delta T = \rho\,Q\,c_p\,\Delta T
Temperature rise ΔT\Delta T of cooling flow; water ρ=1000 kg/m3\rho=1000\ \text{kg/m}^3, cp=4186 J/kg⋅Kc_p=4186\ \text{J/kg}\cdot\text{K}, QQ = volumetric flow (m3/s\text{m}^3/\text{s}).
Heat rate
HR=3413η [BtukWh]HR = \frac{3413}{\eta}\ \left[\frac{\text{Btu}}{\text{kWh}}\right]
Fuel heat per kWh delivered; inverse measure of efficiency (1 kWh=3413 Btu1\ \text{kWh}=3413\ \text{Btu}, per the handbook energy-unit table). Lower heat rate = higher efficiency.
Life-cycle carbon intensity
CI=ECO2e, lifelifetime energy generatedCI = \frac{E_{\text{CO}_2e,\,\text{life}}}{\text{lifetime energy generated}}
Cradle-to-grave CO2e\text{CO}_2e per kWh (g CO2e/kWh\text{g CO}_2e/\text{kWh}); the metric for comparing sources fairly, capturing embodied as well as operational emissions.

Where it lives: NCEES FE Reference Handbook — Environmental Engineering · NCEES FE Reference Handbook — Thermodynamics: Combustion Processes, Basic Cycles (Carnot) · IPCC Fifth Assessment Report (AR5), Working Group I · US EPA, Emission Factors for Greenhouse Gas Inventories

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Many equations follow the FE Reference Handbook 10.6 as NCEES prints it; the rest come from the code, design standard or textbook named in their “Where it lives” line or note. The on-screen reference NCEES supplies on exam day is the copy that counts, so check the edition for your sitting. Independent study resource; not affiliated with, endorsed by, or sponsored by NCEES.