GATE GUIDE

GATE CE Fluid Mechanics and Hydrology Formula Sheet 2027

By MD ANISH AHAMADUpdated 4 Oct 202610 min read
GATE CE Fluid Mechanics and Hydrology Formula Sheet 2027

This GATE CE fluid mechanics and hydrology formula sheet collects the Water Resources Engineering formulas you need for the 2027 paper, grouped by topic. Each table gives the formula, when it applies and the trap that costs marks. Short worked examples with made-up numbers show every formula in use.

In this guide
  1. Key takeaways
  2. How to read this sheet: notation and units
  3. Fluid properties, hydrostatics and the flow equations
  4. Pipe flow, drag and model similitude
  5. Open-channel flow: energy, the jump and uniform flow
  6. Hydrology and groundwater
  7. Irrigation: duty, delta and the exit gradient
  8. Quick revision

Key takeaways

How to read this sheet: notation and units

A few symbols recur throughout. Density ρ\rho is mass per volume; for water take 10001000 kg/m³. Unit weight γw=ρg\gamma_w = \rho g is weight per volume, 9.819.81 kN/m³ for water. Dynamic viscosity μ\mu links shear stress to the velocity gradient. Kinematic viscosity ν=μ/ρ\nu = \mu/\rho is the same property divided by density.

Head means energy per unit weight, measured in metres of the flowing fluid. Hydraulic radius R=A/PR = A/P is flow area over wetted perimeter. It is not the geometric radius and not the depth. In the sheet, log⁡\log means base 10 and ln⁡\ln means natural, exactly as in the book. Take g=9.81g = 9.81 m/s² unless a question says otherwise.

Fluid properties, hydrostatics and the flow equations

Properties and statics

Formula Symbols / when it applies Watch out for
τ=μ dudy\displaystyle \tau = \mu\,\dfrac{du}{dy} Newton's law of viscosity μ\mu has dimensions ML−1T−1ML^{-1}T^{-1}; ν\nu has L2T−1L^2T^{-1}
p=ρghp = \rho g h Pressure at depth hh in a still liquid Gauge pressure; add atmospheric only if asked for absolute
FB=γwVF_B = \gamma_w V Archimedes: weight of fluid displaced The body's own density does not enter
GM=IV−BG\displaystyle GM = \dfrac{I}{V} - BG Floating stability; II of the waterplane area Stable only if the metacentre lies above GG

For example, at 55 m depth, p=1000×9.81×5=49.05p = 1000 \times 9.81 \times 5 = 49.05 kPa. A block of 0.50.5 m³ held fully under water feels FB=9.81×0.5=4.905F_B = 9.81 \times 0.5 = 4.905 kN, whatever it is made of.

Continuity, Bernoulli and momentum

Continuity says the same discharge passes every section of a pipe. Bernoulli says total head stays constant along a streamline when losses are negligible:

A1V1=A2V2,p1ρg+V122g+z1=p2ρg+V222g+z2A_1 V_1 = A_2 V_2, \qquad \frac{p_1}{\rho g} + \frac{V_1^2}{2g} + z_1 = \frac{p_2}{\rho g} + \frac{V_2^2}{2g} + z_2

Halve a pipe from 300300 mm to 150150 mm at V1=1.5V_1 = 1.5 m/s, and V2=1.5×4=6V_2 = 1.5 \times 4 = 6 m/s. On a horizontal pipe the pressure drop is ρ(V22−V12)/2=1000×33.75/2=16.875\rho(V_2^2 - V_1^2)/2 = 1000 \times 33.75/2 = 16.875 kPa.

Trap: Velocity scales with area, so it goes as the diameter squared. Scaling with diameter alone, or dropping the half in the kinetic term, are the two classic wrong answers.

For a pipe bend, the momentum equation gives the force in each direction as pA+ρQVpA + \rho Q V. Add the two perpendicular components as vectors, never arithmetically. The venturimeter combines continuity and Bernoulli:

Q=Cd A1A2A12−A22 2ghQ = C_d \, \frac{A_1 A_2}{\sqrt{A_1^2 - A_2^2}} \, \sqrt{2gh}

Here hh is head of the flowing fluid. A mercury manometer under water reading xx gives h=12.6xh = 12.6x.

Pipe flow, drag and model similitude

Reynolds number and Darcy–Weisbach

Formula Symbols / when it applies Watch out for
Re=VDν=ρVDμ\displaystyle Re = \dfrac{VD}{\nu} = \dfrac{\rho V D}{\mu} Pipe flow; laminar below 20002000, turbulent above 40004000 Using μ\mu where ν\nu is given
hf=fLV22gD\displaystyle h_f = \dfrac{f L V^2}{2 g D} ff is the Darcy friction factor Fanning f′=f/4f' = f/4; a value near 0.0050.005 suggests Fanning
f=64Re\displaystyle f = \dfrac{64}{Re} Laminar flow only Never apply it to turbulent flow
hf∝1D5\displaystyle h_f \propto \dfrac{1}{D^5} Fixed discharge QQ Small diameter changes have large effects

Water at 1.51.5 m/s in a 5050 mm pipe with ν=10−6\nu = 10^{-6} m²/s has Re=75,000Re = 75{,}000, so it is turbulent. A 500500 m pipe of 300300 mm diameter, with f=0.025f = 0.025 and V=1.5V = 1.5 m/s, loses hf=28.125/5.886=4.78h_f = 28.125/5.886 = 4.78 m.

Drag on an immersed body

The drag force is FD=12CDρAV2\displaystyle F_D = \tfrac{1}{2} C_D \rho A V^2, where AA is the projected frontal area. A plate of 0.50.5 m² normal to water at 22 m/s, with CD=1.2C_D = 1.2, carries FD=0.5×1.2×1000×0.5×4=1200F_D = 0.5 \times 1.2 \times 1000 \times 0.5 \times 4 = 1200 N. For a sphere, use the area of a disc of the same diameter, not the surface area, which is four times larger.

Froude similitude for models

Free-surface flow is governed by gravity, so a spillway model must match the Froude number Fr=V/gLFr = V/\sqrt{gL}. Each quantity then scales as a power of the length ratio LrL_r:

Quantity Scale ratio Watch out for
Velocity, time Lr1/2L_r^{1/2} A model runs faster than the prototype
Discharge Lr5/2L_r^{5/2} Not Lr3L_r^3; discharge is not a volume
Force Lr3L_r^3 Pressure scales as LrL_r

At a scale of 1:36, a model discharge of 0.050.05 m³/s means 0.05×362.5=388.80.05 \times 36^{2.5} = 388.8 m³/s in the prototype. Reynolds similitude governs enclosed flows instead, and the two generally cannot be satisfied together.

This sheet is a selection. The book's last-minute sheet of formulae and code constants covers all eight technical sections, and every entry traces back to a fully worked solution. It is part of the GATE CE 2027 book.

Open-channel flow: energy, the jump and uniform flow

Specific energy and critical depth

Specific energy is the energy per unit weight measured from the channel bed. For a rectangular channel carrying qq per unit width:

E=y+q22gy2,yc=(q2g)1/3,Emin⁡=1.5 ycE = y + \frac{q^2}{2 g y^2}, \qquad y_c = \left(\frac{q^2}{g}\right)^{1/3}, \qquad E_{\min} = 1.5\,y_c

Critical depth ycy_c gives the minimum specific energy and Fr=V/gy=1Fr = V/\sqrt{gy} = 1. Below it the flow is supercritical; above it, subcritical. For q=3q = 3 m²/s, yc=(9/9.81)1/3=0.972y_c = (9/9.81)^{1/3} = 0.972 m and Emin⁡=1.458E_{\min} = 1.458 m.

Remember: Critical depth depends only on discharge per unit width. Neither Manning's nn nor the bed slope appears, so compute q=Q/bq = Q/b first.

The hydraulic jump

A hydraulic jump turns supercritical flow into subcritical flow. Check Fr1>1Fr_1 > 1 first, because no jump forms otherwise.

Formula Symbols / when it applies Watch out for
y2y1=12(1+8Fr12−1)\displaystyle \dfrac{y_2}{y_1} = \dfrac{1}{2}\left(\sqrt{1 + 8 Fr_1^2} - 1\right) Bélanger, from momentum; horizontal rectangular channel Dropping the half doubles the answer
ΔE=(y2−y1)34y1y2\displaystyle \Delta E = \dfrac{(y_2 - y_1)^3}{4 y_1 y_2} Energy loss once both depths are known The cube, not the square

With y1=0.4y_1 = 0.4 m and Fr1=4Fr_1 = 4, y2=0.2(129−1)=2.072y_2 = 0.2(\sqrt{129} - 1) = 2.072 m. The loss is ΔE=1.6723/(4×0.4×2.072)=1.409\Delta E = 1.672^3/(4 \times 0.4 \times 2.072) = 1.409 m.

Manning, efficient sections and profiles

Manning's equation gives the velocity of uniform flow, where bed slope, water-surface slope and energy slope are equal:

V=1nR2/3S1/2,R=APV = \frac{1}{n} R^{2/3} S^{1/2}, \qquad R = \frac{A}{P}

With n=0.02n = 0.02, R=0.8R = 0.8 m and S=0.0004S = 0.0004, V=50×0.862×0.02=0.862V = 50 \times 0.862 \times 0.02 = 0.862 m/s.

The most efficient rectangular section has b=2yb = 2y, so R=y/2R = y/2. A trapezoid is most efficient when its sloping side equals half the top width, again giving R=y/2R = y/2. An area of 1818 m² therefore needs y=3y = 3 m and b=6b = 6 m.

Water-surface profiles take a letter from the slope and a number from the zone. Mild means yn>ycy_n > y_c; steep means yn<ycy_n < y_c. Zone 1 lies above both depths, zone 2 between them, zone 3 below both.

Sharp-crested weirs

The discharge over a sharp-crested rectangular weir comes from integrating 2gh\sqrt{2gh} over the head:

Q=23 Cd L 2g H3/2Q = \frac{2}{3}\,C_d\,L\,\sqrt{2g}\,H^{3/2}

For L=2L = 2 m, H=0.4H = 0.4 m and Cd=0.6C_d = 0.6, Q=0.896Q = 0.896 m³/s. End contractions shorten the effective length to L−0.1nHL - 0.1nH. Flow past sharp-crested weirs had no question in any of the sixteen counted papers; the 2027 syllabus changes explain why it still deserves your time.

Trap: An orifice uses Q=CdA2gHQ = C_d A \sqrt{2gH} with a half power. A weir uses the three-halves power. Mixing them up is the standard error.

Hydrology and groundwater

Risk, rainfall and runoff

Formula Symbols / when it applies Watch out for
R=1−(1−1T)n\displaystyle R = 1 - \left(1 - \dfrac{1}{T}\right)^n Risk of at least one exceedance in nn years Reliability is 1−R1 - R
Pˉ=∑AiPi∑Ai\displaystyle \bar{P} = \dfrac{\sum A_i P_i}{\sum A_i} Thiessen mean rainfall Do not divide again if weights sum to 1
f=fc+(f0−fc) e−ktf = f_c + (f_0 - f_c)\,e^{-kt} Horton infiltration capacity fcf_c is the final constant rate
Peak flood =k×UH peak+base flow= k \times \text{UH peak} + \text{base flow} kk cm effective rain of the UH's duration Never scale the base flow
Q=∑aiViQ = \sum a_i V_i Area–velocity streamflow method Sum the products; do not average first
ΔS=(Iˉ−Oˉ) Δt\Delta S = (\bar{I} - \bar{O})\,\Delta t Storage equation behind all routing Convert hours to seconds

A structure designed for a 100100-year flood over a 2525-year life carries R=1−0.9925=0.222R = 1 - 0.99^{25} = 0.222, about 22 per cent. A 33-hour unit hydrograph peaking at 4040 m³/s, with 2.52.5 cm of effective rain in 33 hours and 1010 m³/s base flow, peaks at 2.5×40+10=1102.5 \times 40 + 10 = 110 m³/s.

The φ-index is the constant loss rate that makes rainfall above it equal the observed runoff volume. Subtract it before applying the unit hydrograph. Muskingum routing uses S=K[xI+(1−x)O]S = K[xI + (1 - x)O], and x=0x = 0 reduces it to a reservoir. Streamflow measurement is newly named, yet it was examined in 2023 Set 2, Q.63.

Darcy's law and well hydraulics

Formula Symbols / when it applies Watch out for
Q=kiAQ = k i A; vs=v/nv_s = v/n Darcy; seepage velocity with porosity nn Laminar flow only
Q=2πkb (h2−h1)ln⁡(r2/r1)\displaystyle Q = \dfrac{2\pi k b\,(h_2 - h_1)}{\ln(r_2/r_1)} Confined aquifer of thickness bb; T=kbT = kb Natural log, not base 10
Q=πk (h22−h12)ln⁡(r2/r1)\displaystyle Q = \dfrac{\pi k\,(h_2^2 - h_1^2)}{\ln(r_2/r_1)} Unconfined; heads from the impervious base Heads are squared

With k=20k = 20 m/day, b=15b = 15 m, a head difference of 1.51.5 m and radii of 55 and 5050 m, a confined well gives Q=2827/2.303=1228Q = 2827/2.303 = 1228 m³/day. An unconfined well with k=15k = 15 m/day, heads of 2020 and 1818 m and the same radius ratio gives 15551555 m³/day.

In one line: A given thickness means confined and a linear head term; saturated depths mean unconfined and squared heads.

Irrigation: duty, delta and the exit gradient

Delta is the total depth of water a crop needs over its base period. Duty is the area one cumec can irrigate. With base period BB in days and duty DD in hectares per cumec, Δ=8.64 B/D\Delta = 8.64\,B/D metres. For B=100B = 100 days and D=1200D = 1200 ha/cumec, Δ=0.72\Delta = 0.72 m, or 7272 cm.

To find what must be released at the canal head, divide the field requirement by the efficiency. Multiplying is the wrong direction.

For a weir on a permeable foundation, Khosla's exit gradient is:

GE=Hd⋅1πλ,λ=1+1+α22,α=bdG_E = \frac{H}{d}\cdot\frac{1}{\pi\sqrt{\lambda}}, \qquad \lambda = \frac{1 + \sqrt{1 + \alpha^2}}{2}, \qquad \alpha = \frac{b}{d}

With H=3H = 3 m, a 44 m downstream cut-off and a 2424 m floor, α=6\alpha = 6, λ=3.541\lambda = 3.541 and GE=0.127G_E = 0.127, about 1 in 7.9. As dd shrinks towards zero, GEG_E grows without limit, so the downstream cut-off is essential. Lacey's regime equations were examined in 2025 Set 1, Q.43, but they are not on this sheet.

To see how these topics weigh against the rest of the paper, read the GATE CE subject-wise weightage. Practise the arithmetic on the GATE virtual calculator, and fit the revision into the last two months strategy for GATE CE.

More formula sheets: all of GATE Civil · Environmental and Transportation · Geotechnical · Structural Engineering

Quick revision

  1. Continuity first, then Bernoulli; velocity scales with the diameter squared.
  2. Use the Darcy friction factor in hf=fLV2/(2gD)h_f = fLV^2/(2gD), and f=64/Ref = 64/Re only for laminar flow.
  3. Drag uses the projected frontal area, and Froude models scale discharge as Lr5/2L_r^{5/2}.
  4. Critical depth is (q2/g)1/3(q^2/g)^{1/3}, and Emin⁡=1.5 ycE_{\min} = 1.5\,y_c for a rectangular channel.
  5. Jump: check Fr1>1Fr_1 > 1, use Bélanger for y2y_2, then the cube formula for the loss.
  6. Manning uses R2/3S1/2R^{2/3}S^{1/2}; the efficient rectangle has b=2yb = 2y and R=y/2R = y/2.
  7. Weir discharge goes as H3/2H^{3/2}; risk is 1−(1−1/T)n1 - (1 - 1/T)^n; well equations use ln⁡\ln.
  8. Delta in metres is 8.64 B/D8.64\,B/D, and the exit gradient needs a downstream cut-off.

Frequently asked questions

Which logarithm do the well equations use?

The natural logarithm. Both the confined form Q=2πkb(h2−h1)/ln⁡(r2/r1)Q = 2\pi k b (h_2 - h_1)/\ln(r_2/r_1) and the unconfined form use ln⁡\ln. Taking base 10 instead makes the discharge too large by a factor of about 2.303. Only the ratio of the two radii enters, so observation wells at 5 m and 50 m give the same answer as wells at 10 m and 100 m.

Why is the momentum equation used across a hydraulic jump and not Bernoulli?

A jump dissipates a large and unknown amount of energy in turbulence, so energy is not conserved across it and Bernoulli cannot be applied. The hydrostatic forces on the two faces are known, so momentum can. That gives the sequent depth first. The energy loss then follows from ΔE=(y2−y1)3/(4y1y2)\Delta E = (y_2 - y_1)^3/(4 y_1 y_2).

What is the discharge scale ratio under Froude similitude?

Discharge scales as Lr5/2L_r^{5/2}. Velocity scales as Lr1/2L_r^{1/2} because the Froude number must match, and area scales as Lr2L_r^2, so their product gives the five-halves power. A common error is to scale discharge as Lr3L_r^3, as if it were a volume. Time also scales as Lr1/2L_r^{1/2}, so a model runs faster than the prototype.

What is the difference between Darcy velocity and seepage velocity?

Darcy velocity is discharge divided by the gross cross-sectional area, v=Q/A=kiv = Q/A = ki. Water moves only through the voids, so the actual particle speed, the seepage velocity, is v/nv/n with nn the porosity. Use the Darcy velocity for discharge and the seepage velocity for travel time, for example how long a contaminant takes to reach a well.

Can I take a formula sheet into the GATE CE exam hall?

No paper of your own is allowed in the exam hall, and a virtual calculator is provided on screen. The water resources formulas therefore have to be in memory. Writing the few you forget most on the rough sheet in the first minutes is a useful habit. Confirm the current rules at gate2027.iitm.ac.in, because exam-day rules can change from year to year.

Sources

Dates, fees and the syllabus are set by the GATE 2027 organising institute and can change. Always confirm at gate2027.iitm.ac.in.

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