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PE Mechanical: HVAC and Refrigeration formula sheet

135 key equations from 14 study topics, each with what it is for and where to look it up: the PE Mechanical Reference Handbook 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 PE Mechanical: HVAC and Refrigeration study handbook; the full handbook covers every topic at this depth, with worked examples and the traps that cost points.

135

Equations

14

Study topics

14

Concepts

Psychrometrics & Air Processes
14% of the exam

Moist-air properties, the psychrometric chart, and sensible, latent, mixing, humidification, and dehumidification processes at sea level and altitude.

Moist-Air Properties and the Psychrometric Chart

The six interlocking properties of moist air — dry-bulb, wet-bulb, dew point, humidity ratio, enthalpy, specific volume — and how to fix a state and read processes on the chart.

Humidity ratio from partial pressures
W=0.62198 pwp−pwW = 0.62198\,\dfrac{p_w}{p - p_w}
WW in lbw/lbda\text{lb}_w/\text{lb}_{da}; pwp_w = vapor partial pressure, pp = total pressure (psia). 7000 gr=1 lbw7000\,\text{gr}=1\,\text{lb}_w.
Saturation humidity ratio
Ws=0.62198 pwsp−pwsW_s = 0.62198\,\dfrac{p_{ws}}{p - p_{ws}}
Maximum WW at temperature tt; pwsp_{ws} = saturation pressure of water at tt (psia).
Relative humidity
ϕ=pwpws(t)\phi = \dfrac{p_w}{p_{ws}(t)}
Ratio of actual to saturated vapor partial pressure at the same dry-bulb tt and pp.
Dew point condition
pws(td)=pwp_{ws}(t_d) = p_w
tdt_d = temperature where saturation pressure equals the actual vapor pressure; set by WW alone.
Humidity ratio from wet-bulb
W=(1093−0.556 t∗) Ws∗−0.240 (t−t∗)1093+0.444 t−t∗W = \dfrac{(1093 - 0.556\,t^{*})\,W_s^{*} - 0.240\,(t - t^{*})}{1093 + 0.444\,t - t^{*}}
tt = dry-bulb, t∗t^{*} = wet-bulb (°F), Ws∗W_s^{*} = saturation humidity at t∗t^{*}. ASHRAE USCS correlation (not in the NCEES handbook, which gives WW only from partial pressures).
Moist-air specific enthalpy
h=0.240 t+W(1061+0.444 t)h = 0.240\,t + W(1061 + 0.444\,t)
Btu/lbda\text{Btu/lb}_{da}; tt in °F. First term dry-air sensible, parenthesis vapor latent + sensible.
Moist-air specific volume
v=0.370 (t+459.67)(1+1.6078 W)pv = \dfrac{0.370\,(t + 459.67)(1 + 1.6078\,W)}{p}
ft3/lbda\text{ft}^3/\text{lb}_{da}; tt in °F, pp in psia. Per pound of DRY air, not mixture.
Degree of saturation
μ=WWs(t,p)\mu = \dfrac{W}{W_s(t,p)}
Dimensionless; close to but not equal to relative humidity ϕ\phi.

Where it lives: NCEES PE Mechanical Reference Handbook — §7 Psychrometrics · NCEES PE Mechanical Reference Handbook — §7.4 Thermodynamic Properties of Moist Air · ASHRAE Handbook—Fundamentals, Chapter 1, Psychrometrics

Read the Psychrometrics & Air Processes chapter

Heating & Cooling Loads
10% of the exam

Envelope conduction, solar and internal gains, infiltration and ventilation loads, supply-air flow from room sensible heat, and reheat.

Envelope Conduction Loads: U-Factor, R-Value and CLTD

Build the overall U-factor from series and parallel thermal resistances, then drive heating loads with UAΔT and cooling loads with the CLTD method.

Layer resistance (conduction)
R=LkR = \dfrac{L}{k}
Unit thermal resistance of a solid layer; LL = thickness (ft or in), kk = conductivity (Btu·in/(h·ft²·°F) or Btu/(h·ft·°F)). Units of RR are h·ft²·°F/Btu.
Series resistance and U
Rtotal=Ro+∑jLjkj+Ri,U=1RtotalR_{\text{total}} = R_o + \textstyle\sum_j \dfrac{L_j}{k_j} + R_i, \quad U = \dfrac{1}{R_{\text{total}}}
Add layer and film resistances in series; UU is the reciprocal. Ri≈0.68R_i \approx 0.68 (still indoor air), Ro≈0.17R_o \approx 0.17 winter / 0.250.25 summer.
Parallel-path (area-weighted) U
Uavg=∑ifi UiU_{\text{avg}} = \textstyle\sum_i f_i\,U_i
For framing and other parallel paths; fif_i = area fraction, UiU_i = transmittance of path ii. Weight U-values, never R-values.
Steady-state heating conduction
qheat=UA (ti−to)q_{\text{heat}} = U A\,(t_i - t_o)
Design heating load through a surface, Btu/h. No solar or internal credit; AA in ft², ΔT\Delta T in °F.
Heat gain through interior partitions
q=UA (tb−ti)q = U A\,(t_b - t_i)
Gain from an adjacent unconditioned space at temperature tbt_b to the conditioned space at tit_i (handbook §9.1.9).
CLTD cooling load (opaque)
qcool=UA (CLTD)corrq_{\text{cool}} = U A\,(\text{CLTD})_{\text{corr}}
Cooling load through a sunlit wall or roof, Btu/h. CLTD (°F) embeds sol-air temperature and mass time lag.
CLTD temperature correction
(CLTD)corr=CLTDtable+(78−ti)+(to,mean−85)(\text{CLTD})_{\text{corr}} = \text{CLTD}_{\text{table}} + (78 - t_i) + (t_{o,\text{mean}} - 85)
Adjusts a table value (78 °F indoor, 85 °F mean outdoor basis) to actual design temperatures; to,mean=to,design−12(daily range)t_{o,\text{mean}} = t_{o,\text{design}} - \tfrac12(\text{daily range}).

Where it lives: NCEES PE Mechanical Reference Handbook — §9 Heating, Ventilation, and Air Conditioning (§9.1.9 interior surfaces, §9.1.11 thermal resistance, §9.1.13 fenestration U-factors) · ASHRAE Handbook—Fundamentals, Ch. 18 (Nonresidential Cooling and Heating Load Calculations) and Ch. 26 (Material Properties) · ASHRAE Standard 90.1 — Energy Standard for Buildings

Read the Heating & Cooling Loads chapter

Air Distribution & Ductwork
6% of the exam

Duct sizing and friction, equal-friction and static-regain methods, fan total/static pressure, terminal devices, diffusers, and VAV airflow.

Duct Sizing: Friction, Velocity Pressure, Equal-Friction and Static Regain

How the friction chart, velocity pressure (V/4005)², equivalent diameter, and the equal-friction and static-regain methods turn an airflow schedule into a sized, balanced duct system.

Continuity (duct velocity)
V=QAV = \dfrac{Q}{A}
VV in fpm, QQ in cfm, AA in ft2\text{ft}^2. The first line of nearly every duct calculation.
Velocity pressure (general)
pv=ρ(V1097)2p_v = \rho\left(\dfrac{V}{1097}\right)^2
pvp_v in in. wg, VV in fpm, ρ\rho in lbm/ft3\text{lbm/ft}^3. Use this form whenever air is non-standard (altitude, hot air).
Velocity pressure (standard air)
pv=(V4005)2p_v = \left(\dfrac{V}{4005}\right)^2
Valid only at ρ=0.075 lbm/ft3\rho = 0.075\ \text{lbm/ft}^3; 4005=1097/0.0754005 = 1097/\sqrt{0.075}.
Total pressure
pt=ps+pvp_t = p_s + p_v
Total = static + velocity, all in in. wg. Fans and Bernoulli work in total pressure; friction consumes it.
Darcy friction loss
Δpf=f 12LDh pv\Delta p_f = f\,\dfrac{12L}{D_h}\,p_v
Δpf\Delta p_f in in. wg; LL in ft, DhD_h in in., ff from Colebrook at ε=0.0003 ft\varepsilon=0.0003\ \text{ft}. The friction chart evaluates this for you.
Hydraulic diameter
Dh=4APD_h = \dfrac{4A}{P}
For non-circular duct; AA = area, PP = wetted perimeter (consistent units). Used inside the Darcy relation.
Circular equivalent diameter
De=1.30 (ab)0.625(a+b)0.25D_e = 1.30\,\dfrac{(ab)^{0.625}}{(a+b)^{0.25}}
Round diameter (in.) giving equal airflow, friction, and length to a rectangle of sides a,ba,b (in.). Equal friction, NOT equal area.
Equal-friction principle
ΔpfL=constant for every section\dfrac{\Delta p_f}{L} = \text{constant for every section}
Hold one friction rate (e.g. 0.10 in. wg/100 ft0.10\ \text{in. wg}/100\ \text{ft}); read each section's size from the chart at its airflow.
Static-regain recovery
Δps,regain=R (pv,1−pv,2)\Delta p_{s,\text{regain}} = R\,(p_{v,1} - p_{v,2})
Static recovered as air slows; recovery factor R≈0.5R\approx 0.5–0.750.75. Set equal to downstream friction to keep static constant.
Local loss coefficient
C=ΔptpvC = \dfrac{\Delta p_t}{p_v}
Dimensionless ratio of a fitting's total-pressure loss to the reference velocity pressure; ties duct loss to fittings (see the fittings concept).

Where it lives: NCEES PE Mechanical Reference Handbook — §9.3.6 Duct Design · ASHRAE Handbook—Fundamentals, Ch. 21 Duct Design · ASHRAE Standard 90.1 — Energy Standard

Read the Air Distribution & Ductwork chapter

Ventilation & Indoor Air Quality
5% of the exam

Outdoor-air requirements, dilution and contaminant balances, filtration efficiency (MERV), mixing, exhaust, and pressurization.

Outdoor-Air Rates, Dilution and the Ventilation-Rate Procedure

How ASHRAE 62.1 sizes minimum outdoor air from people-plus-area components, why a single critical zone sets system intake, and the efficiency math behind it.

Breathing-zone outdoor airflow
Vbz=Rp Pz+Ra AzV_{bz} = R_p\,P_z + R_a\,A_z
Minimum outdoor air for the occupied zone. RpR_p = per-person rate (cfm/person), PzP_z = people, RaR_a = per-area rate (cfm/ft2^2), AzA_z = floor area (ft2^2).
Zone outdoor airflow
Voz=VbzEzV_{oz} = \dfrac{V_{bz}}{E_z}
Supply outdoor air after correcting for distribution. EzE_z = zone air-distribution effectiveness (1.0 cooling ceiling supply, 0.8 warm ceiling supply 15 °F or more above space with a ceiling return, 1.2 displacement).
Uncorrected outdoor-air intake
Vou=D∑RpPz+∑RaAzV_{ou} = D\sum R_p P_z + \sum R_a A_z
Sum of zone requirements with occupant diversity DD applied to the people term only. D=D = peak system population / sum of zone populations.
Outdoor-air fraction (system)
Xs=VouVpsX_s = \dfrac{V_{ou}}{V_{ps}}
Average uncorrected outdoor fraction of the system primary airflow VpsV_{ps} (cfm).
Outdoor-air fraction (critical zone)
Zp=VozVpzZ_p = \dfrac{V_{oz}}{V_{pz}}
Outdoor fraction required in a zone's primary supply VpzV_{pz}. The largest ZpZ_p flags the critical zone.
Zone ventilation efficiency
Evz=1+Xs−ZpE_{vz} = 1 + X_s - Z_p
Appendix-A single-zone estimate. <1<1 when the zone needs a richer outdoor mix than the system average.
System ventilation efficiency
Ev=min⁡(Evz)E_v = \min\left(E_{vz}\right)
Smallest zone efficiency governs; dimensionless, typically 0.6–1.0.
Corrected outdoor-air intake
Vot=VouEvV_{ot} = \dfrac{V_{ou}}{E_v}
Actual outdoor air the AHU must draw so the critical zone is satisfied (cfm).
Single-zone intake
Vot=Voz=RpPz+RaAzEzV_{ot} = V_{oz} = \dfrac{R_p P_z + R_a A_z}{E_z}
Collapsed procedure when one zone is served by one unit (100% outdoor or single-zone recirculating).

Where it lives: NCEES PE Mechanical Reference Handbook — §9 Heating, Ventilation, and Air Conditioning (§9.1.2 Human Oxygen Consumption) · ANSI/ASHRAE Standard 62.1 — Ventilation for Acceptable Indoor Air Quality · ASHRAE Handbook — Fundamentals

Read the Ventilation & Indoor Air Quality chapter

Hydronic, Steam & Piping Systems
7% of the exam

Pipe head loss and pump head, hydronic coil capacity, glycol corrections, steam and condensate sizing, and expansion-tank sizing.

Pipe Head Loss, Pump Head and the 500 Water Coefficient

How to size a hydronic loop end to end: friction and fitting head loss, total pump head from the critical circuit, and the q = 500·GPM·ΔT heat-transport rule.

Reynolds number
Re=ρvDμ=vDνRe = \dfrac{\rho v D}{\mu} = \dfrac{v D}{\nu}
Flow regime for pipe flow (handbook §3.4.1): laminar Re<2,000Re<2{,}000, critical/unstable zone 2,0002{,}000–4,0004{,}000, transition zone 4,0004{,}000–12,00012{,}000, fully turbulent Re>12,000Re>12{,}000. DD in ft, vv in fps, ν\nu kinematic viscosity in ft²/s.
Water velocity shortcut
v=0.4085 Qd2v = \dfrac{0.4085\,Q}{d^{2}}
vv in fps from QQ in gpm and inside diameter dd in inches; keep mains at 4–8 fps to limit noise and erosion.
Darcy–Weisbach head loss
hf=f LD v22gh_f = f\,\dfrac{L}{D}\,\dfrac{v^{2}}{2g}
Universal friction loss (ft) for any fluid; ff from Moody/Colebrook, or 64/Re64/Re if laminar. Use whenever the fluid is not standard water.
Laminar friction factor
f=64Ref = \dfrac{64}{Re}
Exact for Re<2000Re < 2000; independent of roughness.
Swamee–Jain (turbulent f)
f=0.25[log⁡10 ⁣(ε/D3.7+5.74Re0.9)]2f = \dfrac{0.25}{\left[\log_{10}\!\left(\dfrac{\varepsilon/D}{3.7}+\dfrac{5.74}{Re^{0.9}}\right)\right]^{2}}
Explicit fit to the Colebrook equation; ε\varepsilon is absolute roughness (≈0.00015\approx 0.00015 ft for commercial steel).
Hazen–Williams (water)
hf=0.2083(100C)1.852Q1.852d4.8655h_f = 0.2083\left(\dfrac{100}{C}\right)^{1.852}\dfrac{Q^{1.852}}{d^{4.8655}}
Head loss in ft per 100 ft; QQ gpm, dd inches. C≈C\approx 150 plastic, 130 copper/cast iron, 120 new welded steel, ~100 old steel (handbook §3.4.2.3). Water only.
Minor (fitting) loss
hm=K v22gh_m = K\,\dfrac{v^{2}}{2g}
KK is the geometry-dependent loss coefficient (handbook §3.4.2.4, Minor Losses in Pipe Fittings, Contractions, and Expansions); sum the KK's along the critical circuit and apply at local velocity.
Equivalent length
Leq=K DfL_{eq} = K\,\dfrac{D}{f}
Straight-pipe length giving the same loss as a fitting; alternative to the KK method — do not use both on one fitting.
Total pump head
Hpump=hf+∑hm+∑hequipH_{pump} = h_{f}+ \sum h_{m} + \sum h_{equip}
Closed loop: no static lift, only friction + fittings + equipment drop along the worst (critical) path.
Water horsepower
whp=Q h3960=Q ΔP1714\text{whp} = \dfrac{Q\,h}{3960} = \dfrac{Q\,\Delta P}{1714}
QQ gpm, hh ft, ΔP\Delta P psi; constants bake in water density (handbook §3.7.5).
Brake horsepower
BHP=Q h (SG)3960 ηp\text{BHP} = \dfrac{Q\,h\,(SG)}{3960\,\eta_p}
Divide hydraulic power by pump efficiency; multiply by specific gravity for non-water fluids. Sizes the motor.
Sensible water heat transport (500 rule)
q=500 Q ΔTq = 500\,Q\,\Delta T
qq Btu/h, QQ gpm, ΔT\Delta T °F. 500=8.33 lb/gal×60 min/h×1.0 Btu/lb⋅°F500 = 8.33\,\text{lb/gal}\times 60\,\text{min/h}\times 1.0\,\text{Btu/lb·°F}; valid for water only.

Where it lives: NCEES PE Mechanical Reference Handbook — §3 Hydraulics, Fluids, and Pipe Flow (§3.4 Fluid Flow, §3.7 Fluid Flow Machinery — §3.7.5 Pump Power Equation) · ASHRAE Handbook—Fundamentals, Pipe Sizing (Ch. 22) · ASHRAE Handbook—HVAC Systems and Equipment, Hydronic Heating and Cooling (Ch. 13)

Read the Hydronic, Steam & Piping Systems chapter

HVAC Controls & Instrumentation
5% of the exam

Valve and damper authority and Cv, sensors and actuators, economizer and reset strategies, and PID feedback response.

Control-Valve Sizing: Cv, Authority and Characteristic

Size a modulating valve from its flow coefficient, protect controllability with valve authority, and match an equal-percentage trim to a nonlinear coil for linear control.

Flow coefficient (general fluid)
Cv=QSgΔPC_v = Q\sqrt{\dfrac{S_g}{\Delta P}}
QQ in gpm, ΔP\Delta P across the valve in psi, SgS_g = specific gravity (1.0 for water). Defines the valve size.
Flow from Cv
Q=CvΔPSgQ = C_v\sqrt{\dfrac{\Delta P}{S_g}}
Square-root law: flow through a fixed opening scales with ΔP\sqrt{\Delta P}. Use to back-check actual drop at a chosen CvC_v.
Cv for water
Cv=QΔPC_v = \dfrac{Q}{\sqrt{\Delta P}}
Sg=1S_g = 1 simplification. CvC_v equals the gpm of 60∘F60^\circ\text{F} water at 1 psi1\,\text{psi} drop.
Equal-percentage characteristic
qqmax⁡=R (x−1)\dfrac{q}{q_{\max}} = R^{\,(x-1)}
xx = fractional stroke (0–1), RR = rangeability (max/min controllable flow). Flow rises by a constant percentage per equal stroke step.
Rangeability
R=qmax⁡qmin⁡R = \dfrac{q_{\max}}{q_{\min}}
Ratio of maximum to minimum controllable flow at a stated characteristic; larger is better for turndown.
Valve authority
β=ΔPvalve, openΔPbranch, open\beta = \dfrac{\Delta P_{\text{valve, open}}}{\Delta P_{\text{branch, open}}}
Open-valve drop divided by total variable branch drop (valve + coil + balancing + fittings) at full flow. Target β≥0.5\beta \ge 0.5.
Installed characteristic
φ=fβ+(1−β) f2\varphi = \dfrac{f}{\sqrt{\beta + (1-\beta)\,f^{2}}}
Maps inherent flow fraction ff to installed flow fraction φ\varphi given authority β\beta. Lower β\beta distorts toward quick-opening.
Valve gain
gain=ΔqΔx\text{gain} = \dfrac{\Delta q}{\Delta x}
Slope of the installed flow-vs-stroke curve. Good control wants this roughly constant across the operating range.

Where it lives: NCEES PE Mechanical Reference Handbook — §11 Temperature Controls (§11.3 Control Valves) · ASHRAE Handbook — Fundamentals, Ch. 7 Fundamentals of Control · ASHRAE Handbook — HVAC Systems and Equipment, Valve characteristics and selection

Read the HVAC Controls & Instrumentation chapter

Refrigeration Cycles & Systems
8% of the exam

Vapor-compression cycles on the p-h diagram, COP and capacity, refrigerant properties and selection, subcooling, superheat, and food/process refrigeration loads.

The Vapor-Compression Cycle: COP, Capacity and the p-h Diagram

The four-process vapor-compression cycle on the pressure-enthalpy diagram, refrigeration effect and compressor work, and how COP, tons, and kW/ton fall out of enthalpy differences.

Refrigeration effect
qL=h1−h4=h1−h3q_L = h_1 - h_4 = h_1 - h_3
Useful cooling per unit mass (Btu/lb). h4=h3h_4 = h_3 because expansion is isenthalpic.
Compressor work
wc=h2−h1w_c = h_2 - h_1
Ideal (isentropic) work per unit mass (Btu/lb); h2h_2 at condenser pressure on the s=s1s = s_1 line.
Heat rejected
qH=h2−h3=qL+wcq_H = h_2 - h_3 = q_L + w_c
Condenser duty per unit mass; energy balance closes the loop.
Capacity from mass flow
Q˙L=m˙ (h1−h4)\dot Q_L = \dot m\,(h_1 - h_4)
Evaporator duty (Btu/h) with m˙\dot m in lb/h; divide by 12,000 for tons.
Ton of refrigeration
1 ton=12,000 Btuh=200 Btumin=3.517 kW1\ \text{ton} = 12{,}000\ \tfrac{\text{Btu}}{\text{h}} = 200\ \tfrac{\text{Btu}}{\text{min}} = 3.517\ \text{kW}
Standard refrigeration capacity unit; use to convert between tons and Btu/h or kW.
Coefficient of performance (refrigerator)
COPR=qLwc=h1−h4h2−h1\mathrm{COP}_R = \dfrac{q_L}{w_c} = \dfrac{h_1 - h_4}{h_2 - h_1}
Cooling delivered per unit compressor work (dimensionless).
COP heat pump
COPHP=qHwc=COPR+1\mathrm{COP}_{HP} = \dfrac{q_H}{w_c} = \mathrm{COP}_R + 1
Same hardware billed for heat rejected; always one greater than the cooling COP.
EER and kW/ton
EER=3.412 COP,kW/ton=3.517COP=12EER\mathrm{EER} = 3.412\,\mathrm{COP}, \qquad \mathrm{kW/ton} = \dfrac{3.517}{\mathrm{COP}} = \dfrac{12}{\mathrm{EER}}
Mixed-unit restatements of COP. High EER and LOW kW/ton both mean efficient.
Carnot (reversed) COP
COPC=TLTH−TL\mathrm{COP}_{C} = \dfrac{T_L}{T_H - T_L}
Thermodynamic ceiling; TLT_L, THT_H ABSOLUTE (∘R^\circ\text{R} or K). Real plant 45–60 % of this.
Compressor isentropic efficiency
ηs=h2s−h1h2a−h1\eta_s = \dfrac{h_{2s} - h_1}{h_{2a} - h_1}
Ratio of ideal to actual work; solve for actual exit enthalpy h2ah_{2a} to size real power.
Compressor power
W˙c=m˙ (h2−h1)\dot W_c = \dot m\,(h_2 - h_1)
Btu/h; divide by 2,544 for hp or by 3,412 for kW.
Volumetric flow / displacement
V˙1=m˙ v1\dot V_1 = \dot m\,v_1
Suction volume flow (ft³/min); v1v_1 = specific volume of suction vapor. Sets compressor displacement.

Where it lives: NCEES PE Mechanical Reference Handbook — §8 Refrigeration · NCEES PE Mechanical Reference Handbook — §4.5 Thermodynamic Cycles and Compressors · ASHRAE Handbook—Fundamentals, Ch. 2 Thermodynamics and Refrigeration Cycles

Read the Refrigeration Cycles & Systems chapter

Cooling Towers & Heat Rejection
5% of the exam

Tower range, approach, and effectiveness, evaporation and makeup water, cycles of concentration, and condenser-water heat balance.

Cooling-Tower Range, Approach, Effectiveness and Water Balance

Range, approach, and effectiveness define what a cooling tower delivers; the wet-bulb sets the thermodynamic floor and the 500-coefficient ties heat rejection to water flow.

Range
R=Thw−TcwR = T_{hw} - T_{cw}
Tower range (°F): entering hot minus leaving cold water. Equals the condenser-water rise across the chiller in a closed loop; set by load and flow.
Approach
A=Tcw−TwbA = T_{cw} - T_{wb}
Approach (°F): leaving cold water minus entering-air WET-BULB. Fixed by tower size and design wet-bulb; never zero.
Cold-water temperature
Tcw=Twb+AT_{cw} = T_{wb} + A
Leaving water at a given approach tracks the wet-bulb one-for-one; the quick way to re-estimate at a new design wet-bulb.
Tower effectiveness
ε=RR+A=Thw−TcwThw−Twb\varepsilon = \dfrac{R}{R+A} = \dfrac{T_{hw}-T_{cw}}{T_{hw}-T_{wb}}
Dimensionless thermal effectiveness; cold-side limit is the wet-bulb. Real towers ≈ 0.5–0.8.
Water-side heat rejection
q˙o=500 (gpm) R\dot q_o = 500\,(\text{gpm})\,R
Sensible heat carried by the circulating water (Btu/hr). The 500 = 8.34 lb/gal × 60 min/hr × 1 Btu/lb·°F assumes STANDARD water.
Required water flow
gpm=q˙o500 R\text{gpm} = \dfrac{\dot q_o}{500\,R}
Inverts the rejection equation; with a 10°F range and 15,000 Btu/hr per cooling-tower ton this gives the 3 gpm/ton rule.
Cooling-tower ton
1 CT ton=15,000 Btuhr1\ \text{CT ton} = 15{,}000\ \tfrac{\text{Btu}}{\text{hr}}
Industry rating adding compressor heat to the 12,000 Btu/hr refrigeration ton at ≈0.88 kW/ton. Do not confuse with the evaporator ton.
Heat-rejection from refrigeration tons
q˙o=q˙evap(1+3412 (kW/ton)12,000)\dot q_o = \dot q_{evap}\left(1 + \dfrac{3412\,(\text{kW/ton})}{12{,}000}\right)
Adds heat of compression to the chiller load; gives Btu/hr to reject for an electric chiller (3412 Btu/hr per kW).

Where it lives: NCEES PE Mechanical Reference Handbook — §9.3.9 Cooling Towers and Fluid Coolers · NCEES PE Mechanical Reference Handbook — §8.3 Condensers · ASHRAE Handbook — HVAC Systems and Equipment, Cooling Towers · Cooling Technology Institute (CTI) — Cooling Tower Performance terminology

Read the Cooling Towers & Heat Rejection chapter

Boilers, Furnaces & Combustion
6% of the exam

Fuel heating values, air-fuel ratio and excess air, combustion and thermal efficiency, boiler/furnace fuel rate, and flue-gas losses.

Heating Values, Combustion Efficiency and Fuel Rate

Higher vs lower heating value, combustion vs thermal efficiency, and how to back the fuel-input rate (and boiler horsepower) out of a required output.

Higher vs lower heating value
HHV=LHV+mw hfgHHV = LHV + m_{w}\,h_{fg}
mwm_w = mass of water formed per unit fuel (lb water / lb fuel), hfg≈1,060 Btu/lbh_{fg}\approx 1{,}060\,\text{Btu/lb} at the heating-value reference temperature (~60 °F, where the product water is condensed to liquid). HHV counts the latent heat of the product water; LHV does not.
Fuel-to-load (overall) efficiency
ηf-l=Q˙outHHV⋅m˙f\eta_{f\text{-}l} = \dfrac{\dot{Q}_{out}}{HHV\cdot \dot{m}_{f}}
Useful delivered heat divided by fuel energy input; debits stack, radiation, and blowdown losses. Q˙out\dot{Q}_{out} in Btu/h, m˙f\dot m_f in lb/h (or use HHVvolHHV_{vol} with volumetric flow). Use HHV with HHV-basis fuel data. This is the handbook's first §10.3 "thermal efficiency" form (useful heat / heating value of fuel); its alternative (Qh−Qfl)/Qh(Q_h-Q_{fl})/Q_h form, below, is stack-only.
Combustion efficiency (= handbook §10.3 stack-loss form)
ηc=100%−Lstack=Qh−QflQh×100%\eta_{c} = 100\% - L_{stack} = \dfrac{Q_h - Q_{fl}}{Q_h}\times 100\%
What a flue-gas analyzer reports; equals 100% minus the dry-gas and moisture stack losses. The NCEES handbook §10.3 prints this stack-loss form as its alternative ("or") definition of "thermal efficiency," after useful heat / heating value of fuel. Always higher than the fuel-to-load efficiency, which also subtracts radiation and blowdown.
Fuel-input rate from output
Q˙in=Q˙outη\dot{Q}_{in} = \dfrac{\dot{Q}_{out}}{\eta}
Required fuel energy input (Btu/h). Use the efficiency on the same heating-value basis as the fuel data.
Fuel quantity (mass or volume)
m˙f=Q˙inHHVV˙f=Q˙inHHVvol\dot{m}_{f} = \dfrac{\dot{Q}_{in}}{HHV}\qquad \dot{V}_{f} = \dfrac{\dot{Q}_{in}}{HHV_{vol}}
Mass rate (lb/h) for oil/coal using mass HHV (Btu/lb); volumetric rate (ft³/h or gal/h) for gas/oil using volumetric HHV (Btu/ft³ or Btu/gal).
Gas input rate with meter correction
Q˙=HHV⋅VFR⋅Ts PT Ps\dot{Q} = HHV\cdot VFR\cdot \dfrac{T_s\,P}{T\,P_s}
Handbook §10.6. Ts=520 ∘RT_s=520\,^\circ\text{R}, Ps=14.735 psiaP_s=14.735\,\text{psia}; TT,PP are absolute meter conditions; VFRVFR is metered volumetric flow (ft³/h).
Efficiency basis conversion
ηHHV=ηLHV LHVHHV\eta_{HHV} = \eta_{LHV}\,\dfrac{LHV}{HHV}
Convert a lower-heating-value efficiency to the higher-heating-value basis (and inverse). For methane LHV/HHV=0.900LHV/HHV = 0.900.
Boiler horsepower
BHP=Q˙out33,470=m˙s34.5\text{BHP} = \dfrac{\dot{Q}_{out}}{33{,}470} = \dfrac{\dot{m}_{s}}{34.5}
Output rating. Q˙out\dot Q_{out} in Btu/h; m˙s\dot m_s in lb/h of steam from and at 212 ∘F212\,^\circ\text{F}. 1 BHP also ≈9.81 kW\approx 9.81\,\text{kW}.
Boiler steam output (real feedwater)
Q˙out=m˙s (hs−hfw)\dot{Q}_{out} = \dot{m}_{s}\,(h_{s} - h_{fw})
hsh_s = enthalpy of generated steam, hfwh_{fw} = feedwater enthalpy (Btu/lb). Reduces to the latent heat only when feedwater is saturated liquid at 212 °F.
Hot-water output (standard coefficient)
Q˙=500⋅gpm⋅ΔT\dot{Q} = 500\cdot \text{gpm}\cdot \Delta T
Sensible heat of water; 500=8.33 lbgal×60 minh×1 Btulb ∘F500 = 8.33\,\tfrac{\text{lb}}{\text{gal}}\times 60\,\tfrac{\text{min}}{\text{h}}\times 1\,\tfrac{\text{Btu}}{\text{lb}\,^\circ\text{F}}. ΔT\Delta T in °F; valid for water near room temperature.

Where it lives: NCEES PE Mechanical Reference Handbook — §10 Combustion and Fuels · NCEES PE Mechanical Reference Handbook — §6 Steam (boiler plant basics) · ASHRAE Handbook—Fundamentals, Ch. 28 Combustion and Fuels · ASHRAE Handbook—HVAC Systems and Equipment, Boilers chapter

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Heat Exchangers & Coils
7% of the exam

LMTD and effectiveness-NTU methods, shell-and-tube and plate-and-frame exchangers, correction factors, and cooling/heating coil duty.

The LMTD Method and the F Correction Factor

Counterflow vs parallel flow, the log-mean temperature difference, and the F factor that lets Q = U·A·LMTD·F size shell-and-tube and cross-flow exchangers.

Heat-exchanger rate equation
Q=UA ΔTlm FQ = U A\,\Delta T_{lm}\,F
Duty QQ (Btu/h); UU overall coefficient (Btu/h·ft²·°F) on area AA (ft²); ΔTlm\Delta T_{lm} counterflow LMTD; FF correction factor (=1=1 for pure counter/parallel flow and for phase-change streams).
Log-mean temperature difference
ΔTlm=ΔT1−ΔT2ln⁡ ⁣(ΔT1/ΔT2)\Delta T_{lm} = \dfrac{\Delta T_1 - \Delta T_2}{\ln\!\left(\Delta T_1/\Delta T_2\right)}
ΔT1,ΔT2\Delta T_1,\Delta T_2 are the terminal temperature differences (°F or °R — same value). Reduces to ΔT1\Delta T_1 when the two ends are equal.
Counterflow terminal differences
ΔT1=THi−TCo,ΔT2=THo−TCi\Delta T_1 = T_{Hi}-T_{Co}, \quad \Delta T_2 = T_{Ho}-T_{Ci}
Hot inlet pairs with cold outlet, hot outlet with cold inlet. Use for the LMTD baseline even on multipass units.
Parallel-flow terminal differences
ΔT1=THi−TCi,ΔT2=THo−TCo\Delta T_1 = T_{Hi}-T_{Ci}, \quad \Delta T_2 = T_{Ho}-T_{Co}
Both streams enter the same end. Gives a smaller LMTD than counterflow for identical temperatures (equal only when one stream is isothermal).
First-law duty
Q=m˙ cp (Tin−Tout)Q = \dot{m}\,c_p\,(T_{in}-T_{out})
Energy balance on one stream; for water m˙cp≈500 (gpm)\dot m c_p \approx 500\,(\text{gpm}) Btu/h·°F. Both streams carry the same QQ (adiabatic shell).
F-factor parameter P (effectiveness)
P=to−tiTi−tiP = \dfrac{t_o - t_i}{T_i - t_i}
Tube-side temperature rise over the maximum available difference; tt = tube (usually cold) stream, TT = shell stream. 0≤P≤10\le P\le 1.
F-factor parameter R (capacity ratio)
R=Ti−Toto−tiR = \dfrac{T_i - T_o}{t_o - t_i}
Ratio of the two stream temperature changes; equals m˙cp\dot m c_p of tube side over that of shell side. RR may be above or below 1.
F factor, 1 shell pass / 2+ tube passes
F=R2+1 ln⁡ ⁣1−P1−PR(R−1) ln⁡ ⁣2−P(R+1−R2+1)2−P(R+1+R2+1)F = \dfrac{\sqrt{R^2+1}\,\ln\!\dfrac{1-P}{1-PR}}{(R-1)\,\ln\!\dfrac{2-P\left(R+1-\sqrt{R^2+1}\right)}{2-P\left(R+1+\sqrt{R^2+1}\right)}}
Closed form for the most common shell-and-tube geometry (valid R≠1R\ne1). The exam usually supplies FF from a chart; know how PP and RR feed it.
Equal-end LMTD limit
ΔTlm=ΔT1=ΔT2(when ΔT1=ΔT2)\Delta T_{lm} = \Delta T_1 = \Delta T_2 \quad(\text{when }\Delta T_1=\Delta T_2)
Avoids the 0/0 logarithm; occurs in balanced counterflow (CH=CCC_H = C_C), where ΔT\Delta T is constant along the length — not in a condenser, whose ends differ by the other stream's temperature change.
Required area
A=QU ΔTlm FA = \dfrac{Q}{U\,\Delta T_{lm}\,F}
Sizing form. AA is on the same reference surface as UU (inside or outside).

Where it lives: NCEES PE Mechanical Reference Handbook — §5.5 Heat Exchangers · ASHRAE Handbook—Fundamentals, Heat Transfer chapter · Incropera & DeWitt, Fundamentals of Heat and Mass Transfer

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Chillers, Heat Pumps & Thermal Storage
6% of the exam

Chiller kW/ton and IPLV, heat-pump heating COP and balance point, condenser/evaporator duty, and chilled-water and ice thermal storage.

Chiller Performance: kW/ton, COP, EER and IPLV

Translate freely among kW/ton, COP and EER, weight the four part-load points into IPLV, and connect water- vs air-cooled chillers to the condenser and evaporator approach.

Cooling COP
COP=Q˙LW˙\text{COP} = \dfrac{\dot Q_L}{\dot W}
Dimensionless; cooling effect Q˙L\dot Q_L over compressor input W˙\dot W, both in the same units. Convert Btu/h to W with 3.412 Btu/h=1 W3.412\ \text{Btu/h}=1\ \text{W}.
Ton of refrigeration
1 ton=12,000 Btu/h=3.516 kW1\ \text{ton} = 12{,}000\ \text{Btu/h} = 3.516\ \text{kW}
The conversion that links every chiller rating; from §4 Thermodynamics (3,516 W3{,}516\ \text{W} per ton).
kW/ton to COP
kW/ton=3.516COP\text{kW/ton} = \dfrac{3.516}{\text{COP}}
Inverse efficiency — lower is better. 3.5163.516 is kW of heat per ton. Typical water-cooled 0.5–0.60.5\text{–}0.6, air-cooled 1.0–1.21.0\text{–}1.2.
EER definition
EER=Q˙L [Btu/h]W˙ [W]\text{EER} = \dfrac{\dot Q_L\,[\text{Btu/h}]}{\dot W\,[\text{W}]}
Cooling in Btu/h per watt of input; quoted as a bare number but carries units Btu/(W⋅h)\text{Btu/(W}\cdot\text{h)}.
EER from kW/ton and COP
EER=12kW/ton=3.412 COP\text{EER} = \dfrac{12}{\text{kW/ton}} = 3.412\,\text{COP}
The 12 is 12,000 Btu/h12{,}000\ \text{Btu/h} per ton divided by 1000 W; the 3.4123.412 is Btu/h per watt.
IPLV, AHRI 550/590 (COP or EER)
IPLV=0.01 A+0.42 B+0.45 C+0.12 D\text{IPLV} = 0.01\,A + 0.42\,B + 0.45\,C + 0.12\,D
Weighted sum of COP or EER (higher is better) at 100/75/50/25% load; this is the AHRI 550/590 definition for efficiencies. Weights are operating-hour fractions. Not printed in the PE Mechanical Reference Handbook.
IPLV, AHRI 550/590 (kW/ton)
IPLV=10.01A+0.42B+0.45C+0.12D\text{IPLV} = \dfrac{1}{\dfrac{0.01}{A}+\dfrac{0.42}{B}+\dfrac{0.45}{C}+\dfrac{0.12}{D}}
Use when AA–DD are kW/ton (lower is better). It equals 3.5163.516 divided by the COP-form IPLV. Not printed in the PE Mechanical Reference Handbook.
Condenser approach
Approachcond=Tcond,sat−Tcw,leaving\text{Approach}_{\text{cond}} = T_{\text{cond,sat}} - T_{\text{cw,leaving}}
Saturated condensing temperature minus leaving condenser-water temperature (°F). Widens with fouling.
Evaporator approach
Approachevap=Tchw,leaving−Tevap,sat\text{Approach}_{\text{evap}} = T_{\text{chw,leaving}} - T_{\text{evap,sat}}
Leaving chilled-water temperature minus saturated suction temperature (°F).
Condenser heat rejection
Q˙rej=Q˙L+W˙\dot Q_{\text{rej}} = \dot Q_L + \dot W
First-law balance: heat the condenser must reject equals evaporator cooling plus compressor work (Btu/h).
Condenser water flow
gpm=Q˙rej500 ΔT\text{gpm} = \dfrac{\dot Q_{\text{rej}}}{500\,\Delta T}
Q˙rej\dot Q_{\text{rej}} in Btu/h, ΔT\Delta T = condenser-water range (°F). The 500 bakes in water density and cpc_p (8.34×608.34\times60).

Where it lives: NCEES PE Mechanical Reference Handbook — §8 Refrigeration · NCEES PE Mechanical Reference Handbook — §4 Thermodynamics (COP, ton definition) · AHRI Standard 550/590 — Performance Rating of Water-Chilling Packages · ASHRAE Handbook — HVAC Systems and Equipment, Liquid-Chilling Systems

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Pumps, Compressors & Fans
7% of the exam

Affinity laws, pump and fan power and efficiency, NPSH and cavitation, operating point, parallel/series operation, and compressor work.

Pump and Fan Affinity Laws and the Operating Point

The affinity laws (flow ∝ N, head ∝ N², power ∝ N³), riding the pump/fan curve, and why a VFD beats a throttling valve on energy.

Affinity laws — speed change
Q2Q1=N2N1,h2h1=(N2N1)2,bhp2bhp1=(N2N1)3\frac{Q_2}{Q_1}=\frac{N_2}{N_1},\quad \frac{h_2}{h_1}=\left(\frac{N_2}{N_1}\right)^{2},\quad \frac{bhp_2}{bhp_1}=\left(\frac{N_2}{N_1}\right)^{3}
Fixed impeller, variable speed NN (rpm). Flow linear, head/pressure square, power cube. Valid at constant efficiency.
Affinity laws — impeller diameter
Q2Q1=D2D1,h2h1=(D2D1)2,bhp2bhp1=(D2D1)3\frac{Q_2}{Q_1}=\frac{D_2}{D_1},\quad \frac{h_2}{h_1}=\left(\frac{D_2}{D_1}\right)^{2},\quad \frac{bhp_2}{bhp_1}=\left(\frac{D_2}{D_1}\right)^{3}
Fixed speed, trimmed impeller diameter DD. Same 1-2-3 exponents as speed change.
Specific-gravity scaling
bhp2bhp1=SG2SG1(at fixed Q,h)\frac{bhp_2}{bhp_1}=\frac{SG_2}{SG_1}\quad(\text{at fixed }Q,h)
Head in feet of fluid is density-independent; pressure (psi) and brake horsepower scale linearly with SGSG.
Fan law form (pressure)
P2P1=(N2N1)2(ρ2ρ1)\frac{P_2}{P_1}=\left(\frac{N_2}{N_1}\right)^{2}\left(\frac{\rho_2}{\rho_1}\right)
PP = fan total, static, or velocity pressure (in. wg). Fan pressure also scales with air density ρ\rho — important at altitude or elevated temperature.
Fan law form (power)
W˙2W˙1=(N2N1)3(ρ2ρ1)\frac{\dot{W}_2}{\dot{W}_1}=\left(\frac{N_2}{N_1}\right)^{3}\left(\frac{\rho_2}{\rho_1}\right)
Fan shaft power scales with speed cubed and linearly with air density. Per NCEES §9.3.8.3 (dry standard air, 14.696 psia, 70°F unless stated).
Friction-system power reduction
P2P1≈(Q2Q1)3\frac{P_2}{P_1}\approx\left(\frac{Q_2}{Q_1}\right)^{3}
VFD savings estimate on a friction-dominated system (h∝Q2h\propto Q^2 through the origin). Overstates savings if static head is present.
Head as a parabola through the origin
h2=h1(Q2Q1)2h_2 = h_1\left(\frac{Q_2}{Q_1}\right)^{2}
Combines the flow and head laws; eliminating NN shows affinity-scaled points lie on a parabola h∝Q2h\propto Q^2 through the origin.
Operating point definition
hpump(Q)=hsystem(Q)h_{pump}(Q)=h_{system}(Q)
Steady-state flow is the intersection of pump/fan curve and system curve. Affinity scaling moves the machine curve; the system curve is unchanged.

Where it lives: NCEES PE Mechanical Reference Handbook — §3.7.6 Pump Affinity Laws · NCEES PE Mechanical Reference Handbook — §9.3.8.3 Fan Affinity Laws · ASHRAE Handbook—HVAC Systems and Equipment, Ch. 44 (Centrifugal Pumps) and Ch. 21 (Fans) · ASHRAE 90.1 — Energy Standard (variable-speed drive provisions)

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Energy Recovery
4% of the exam

Sensible and total (enthalpy) recovery effectiveness, enthalpy wheels, heat pipes, and run-around loops, with recovered-energy and economizer savings.

Sensible and Total Energy-Recovery Effectiveness

How sensible, latent, and total effectiveness define an HRV/ERV, how to find leaving conditions and recovered energy, and how the supply/exhaust airflow ratio and frost control bound it.

Sensible effectiveness
εs=m˙scps(t2−t1)Cmin(t3−t1)=m˙ecpe(t3−t4)Cmin(t3−t1)\varepsilon_s = \frac{\dot m_s c_{ps}(t_2 - t_1)}{C_{min}(t_3 - t_1)} = \frac{\dot m_e c_{pe}(t_3 - t_4)}{C_{min}(t_3 - t_1)}
Ratio of actual to maximum sensible recovery. t1t_1 outdoor in, t2t_2 supply out, t3t_3 exhaust in, t4t_4 exhaust out (°F); Cmin=min⁡(m˙scps,m˙ecpe)C_{min}=\min(\dot m_s c_{ps},\dot m_e c_{pe}) is the smaller air-capacity rate. Because numerator and denominator share the same m˙\dot m basis, the ratio is dimensionless regardless of whether m˙\dot m is taken in lb/min or lb/h.
Latent (moisture) effectiveness
εL=m˙s(w2−w1)m˙min(w3−w1)\varepsilon_L = \frac{\dot m_s(w_2 - w_1)}{\dot m_{min}(w_3 - w_1)}
Built on humidity ratio ww (lbw/lbda\text{lb}_w/\text{lb}_{da}). m˙min\dot m_{min} = smaller dry-air mass flow (lb/min). Zero for an HRV; nonzero only for vapor-permeable ERV media.
Total (enthalpy) effectiveness
εt=m˙s(h2−h1)m˙min(h3−h1)\varepsilon_t = \frac{\dot m_s(h_2 - h_1)}{\dot m_{min}(h_3 - h_1)}
Built on moist-air enthalpy hh (Btu/lbda\text{Btu/lb}_{da}). Total recovery equals the sum of sensible and latent recovery.
Supply leaving temperature
t2=t1+εs Cminm˙scps (t3−t1)t_2 = t_1 + \varepsilon_s\,\frac{C_{min}}{\dot m_s c_{ps}}\,(t_3 - t_1)
Conditioned outdoor air handed to the downstream coil. Reduces to t2=t1+εs(t3−t1)t_2 = t_1 + \varepsilon_s(t_3-t_1) when the supply is the smaller (or balanced) stream.
Exhaust leaving temperature
t4=t3−εs Cminm˙ecpe (t3−t1)t_4 = t_3 - \varepsilon_s\,\frac{C_{min}}{\dot m_e c_{pe}}\,(t_3 - t_1)
Used for the frost check: t4t_4 below 32 °F at the exhaust dew point freezes condensate inside the device.
Recovered sensible heat
q˙s=1.10 Qs (t2−t1)=60 m˙scps(t2−t1)\dot q_s = 1.10\,Q_s\,(t_2 - t_1) = 60\,\dot m_s c_{ps}(t_2 - t_1)
Btu/h. The 1.101.10 coefficient assumes sea-level standard air (ρ=0.075\rho=0.075 lb/ft³, cp=0.24+0.45w≈0.244c_p = 0.24 + 0.45w \approx 0.244; handbook §9.1.7). QsQ_s = supply cfm.
Recovered latent heat
q˙L=4,840 Qs (w2−w1)=0.691 Qs (gr2−gr1)\dot q_L = 4{,}840\,Q_s\,(w_2 - w_1) = 0.691\,Q_s\,(\text{gr}_2 - \text{gr}_1)
Btu/h. Use 4,840=60(0.075)(1,076)4{,}840 = 60(0.075)(1{,}076) with Δw\Delta w in lbw/lbda\text{lb}_w/\text{lb}_{da} (handbook §9.1.7), or 0.691=4,840/7,0000.691 = 4{,}840/7{,}000 with Δw\Delta w in grains per lbda\text{lb}_{da} — the two embed the same hfg≈1,076 Btu/lbh_{fg}\approx1{,}076\ \text{Btu/lb}. Standard air.
Recovered total heat
q˙t=4.5 Qs (h2−h1)=q˙s+q˙L\dot q_t = 4.5\,Q_s\,(h_2 - h_1) = \dot q_s + \dot q_L
Btu/h. The 4.54.5 coefficient (60×0.07560\times0.075) assumes standard air; total = sensible + latent.
Maximum sensible recovery
q˙s,max⁡=1.10 Qmin (t3−t1)\dot q_{s,\max} = 1.10\,Q_{min}\,(t_3 - t_1)
Denominator of εs\varepsilon_s. Built on the smaller airflow QminQ_{min} and the full inlet temperature difference.
Capacity rate
C=60 m˙cp=60 Q ρ cp,Cmin=min⁡(Cs,Ce)C = 60\,\dot m c_p = 60\,Q\,\rho\,c_p, \qquad C_{min} = \min(C_s, C_e)
Air-side heat capacity rate (Btu/h·°F) with m˙\dot m in lb/min and QQ in cfm; the 6060 converts min→\toh. The smaller stream caps recovery. In the dimensionless effectiveness ratios the 6060 cancels, so Cmin/(m˙scps)C_{min}/(\dot m_s c_{ps}) may be evaluated on either basis.
Effectiveness decomposition
εt (h3−h1)=εs cp(t3−t1)+εL hfg(w3−w1)\varepsilon_t\,(h_3 - h_1) = \varepsilon_s\,c_p(t_3 - t_1) + \varepsilon_L\,h_{fg}(w_3 - w_1)
Total recovery is sensible plus latent; with hfg≈1,076 Btu/lbh_{fg}\approx1{,}076\ \text{Btu/lb} (the value behind the handbook's 4,8404{,}840 latent coefficient) this ties εt\varepsilon_t back to εs\varepsilon_s and εL\varepsilon_L at balanced flow.

Where it lives: NCEES PE Mechanical Reference Handbook — §9.2.7 Heat-Recovery Ventilator and §9.2.8 Energy-Recovery Ventilator · ASHRAE Handbook—HVAC Systems and Equipment, Ch. 26 Air-to-Air Energy Recovery Equipment · AHRI Standard 1060 — Performance Rating of Air-to-Air Exchangers for Energy Recovery Ventilation · ASHRAE Handbook—Fundamentals, Ch. 1 Psychrometrics

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Codes, Acoustics, Economics & Electrical
10% of the exam

Codes and standards, sound and vibration control (NC, dBA, isolation), life-cycle and payback economics, and motor power, amperage, and heat output.

Life-Cycle Cost, Simple and Discounted Payback

Compare HVAC alternatives on a present-worth basis with the interest factors, and judge energy retrofits with simple and discounted payback.

Single-payment compound amount (F/P)
(F/P,i,n)=(1+i)n(F/P,i,n)=(1+i)^{n}
Moves a present sum PP forward nn periods to its future worth FF at periodic rate ii.
Single-payment present worth (P/F)
(P/F,i,n)=(1+i)−n(P/F,i,n)=(1+i)^{-n}
Discounts a single future sum FF (e.g., salvage, a future replacement) back to year 0.
Uniform-series present worth (P/A)
(P/A,i,n)=(1+i)n−1i (1+i)n(P/A,i,n)=\dfrac{(1+i)^{n}-1}{i\,(1+i)^{n}}
Collapses a level annual series AA (energy, O&M) over nn years into one present worth PP.
Capital recovery factor (A/P)
(A/P,i,n)=i (1+i)n(1+i)n−1(A/P,i,n)=\dfrac{i\,(1+i)^{n}}{(1+i)^{n}-1}
Spreads a present cost into nn equal annual payments; the reciprocal of (P/A)(P/A). Used for equivalent annual cost.
Uniform-series compound amount (F/A)
(F/A,i,n)=(1+i)n−1i(F/A,i,n)=\dfrac{(1+i)^{n}-1}{i}
Future worth of a level annual series; (A/F)=i/[(1+i)n−1](A/F)=i/[(1+i)^n-1] is its reciprocal (sinking fund).
Effective interest rate
ie=(1+rm)m−1i_e=\left(1+\dfrac{r}{m}\right)^{m}-1
rr = nominal annual rate, mm = compounding periods per year. Convert before using period factors.
Life-cycle cost
LCC=C0+AO&M (P/A,i,n)−Sn (P/F,i,n)LCC = C_0 + A_{\text{O\&M}}\,(P/A,i,n) - S_n\,(P/F,i,n)
Present-worth total of ownership: first cost C0C_0, annual costs, less salvage SnS_n. Lowest LCC wins.
Simple payback
nsimple=C0−SAsavingsn_{\text{simple}}=\dfrac{C_0-S}{A_{\text{savings}}}
Years for undiscounted annual savings to repay first cost; screening only — ignores ii and post-payback value.
Discounted payback
n=ln⁡[ CRF/(CRF−i) ]ln⁡(1+i),CRF=AsavingsC0n=\dfrac{\ln[\,CRF/(CRF-i)\,]}{\ln(1+i)},\quad CRF=\dfrac{A_{\text{savings}}}{C_0}
Handbook improved-payback period. Requires CRF>iCRF>i or the project never pays back.
Net present worth of a measure
NPW=Asavings (P/A,i,n)−ΔC0NPW = A_{\text{savings}}\,(P/A,i,n) - \Delta C_0
Decision metric for an efficiency upgrade; NPW>0NPW>0 accept. ΔC0\Delta C_0 = incremental first cost.
Uniform gradient present worth (P/G)
(P/G,i,n)=(1+i)n−in−1i2(1+i)n(P/G,i,n)=\dfrac{(1+i)^{n}-i n-1}{i^{2}(1+i)^{n}}
Present worth of a cost that increases by a constant amount GG each year (e.g., escalating maintenance).

Where it lives: NCEES PE Mechanical Reference Handbook — §1.6 Economic Analysis (factor formulas and factor tables) · ASHRAE Handbook—HVAC Applications, Owning and Operating Costs (life-cycle cost method) · NIST Handbook 135 — Life-Cycle Costing Manual for the Federal Energy Management Program

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