FE Civil exam practice: cram pack

Formula sheets, the key method steps for every topic and 30 practice problems, with full solutions at the back.

New problemsBack to the course

In the print window, choose “Save as PDF” to keep a copy on your device.

1Formulas and methods

Beam support reactions

Equilibrium
ΣFx = 0, ΣFy = 0, ΣM = 0
Uniform load
resultant w·L at the middle of the load
Moment
M = F·d

Method

  1. Draw a free-body diagram and replace each support by its reactions.
  2. Replace every distributed load by a single force at its centroid.
  3. Take moments about one support to find the reaction at the other.
  4. Use ΣFy = 0 to find the remaining reaction, and check with a second moment equation.

Truss: method of joints

Method of joints
ΣFx = 0, ΣFy = 0 at each joint
Method of sections
ΣM = 0 about a cut point
Member force
positive = tension, negative = compression

Method

  1. Find the support reactions for the whole truss.
  2. Method of joints: start at a joint with at most two unknown member forces and use ΣFx = 0 and ΣFy = 0.
  3. Method of sections: cut through the member you need and take moments about a point where the other unknown members meet.
  4. Assume tension; a negative answer means compression.

Shear force & bending moment

Shear and moment
V = ΣF on one side, M = ΣF·d on one side
Bending stress
σ = M·y/I
Rectangle
I = bh³/12
Section modulus
W = I/ymax
Simply supported, uniform load
Mmax = wL²/8

Method

  1. Find the support reactions from equilibrium of the whole beam.
  2. Cut the beam at the section you need and keep one side.
  3. Shear force: sum of the vertical forces on that side. Bending moment: sum of their moments about the cut.
  4. For the maximum moment, find where the shear force is zero.

Beam deflection

Point load at midspan
δ = PL³/(48EI)
Uniform load, simply supported
δ = 5wL⁴/(384EI)
Cantilever, end load
δ = PL³/(3EI)
Cantilever, uniform load
δ = wL⁴/(8EI)
Superposition
δ = δ1 + δ2

Column buckling

Euler load
Pcr = π²EI/(KL)²
Effective length factor
K = 1 pinned–pinned, 0.5 fixed–fixed, 0.7 fixed–pinned, 2 fixed–free
Critical stress
σcr = Pcr/A
Slenderness
λ = KL/r, r = √(I/A)

Centroid & second moment of area

Centroid
ȳ = ΣAiyi/ΣAi
Rectangle
I = bh³/12
Parallel-axis theorem
I = Ic + A·d²
Composite section
I = Σ(Ic,i + Aidi²)

Effective stress in soil

Total stress
σ = Σγi·hi
Pore water pressure
u = γw·(z − zw)
Effective stress
σ′ = σ − u
Water
γw = 9.81 kN/m³

Consolidation settlement

Normally consolidated
S = Cc·H/(1 + e0)·log₁₀(σ′f/σ′0)
Final stress
σ′f = σ′0 + Δσ (at mid-depth of the layer)
Overconsolidated, σ′f ≤ σ′p
S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0)
Overconsolidated, σ′f > σ′p
S = H/(1 + e0)·[Cr·log₁₀(σ′p/σ′0) + Cc·log₁₀(σ′f/σ′p)]
Overconsolidation ratio
OCR = σ′p/σ′0
Time for consolidation
t = Tv·Hdr²/cv
Drainage path
Hdr = H/2 (double drainage), H (single drainage)
Time factors
U 50% → 0.197, 60% → 0.287, 70% → 0.403, 80% → 0.567, 90% → 0.848

Hydrostatic force

Pressure at depth
p = ρgh
Force on a vertical wall
F = ρg·hc·A
Centre of pressure
yp = yc + Ic/(ycA)
Rectangle
Ic = bH³/12

Pipe friction & head loss

Reynolds number
Re = V·D/ν = ρ·V·D/μ
Flow regime
laminar below Re ≈ 2000, turbulent above Re ≈ 4000
Mean velocity
V = Q/A, A = π·D²/4
Darcy–Weisbach
hf = f·(L/D)·V²/(2g)
Minor losses
hm = ΣK·V²/(2g)
Typical K values
entrance 0.5, exit 1.0, 90° bend ≈ 0.3
Pressure drop
Δp = ρ·g·hf
Two open reservoirs
Δz = (f·L/D + ΣK)·V²/(2g)
Free outlet
H = (1 + f·L/D + ΣK)·V²/(2g)

Open-channel flow (Manning)

Manning equation
V = (1/n)·R2/3·S1/2
Flow rate
Q = A·V
Hydraulic radius
R = A/P (P = wetted perimeter, free surface excluded)
Rectangle
A = b·y, P = b + 2y
Trapezoid (side slope z:1)
A = (b + z·y)·y, P = b + 2y·√(1 + z²)
Circular pipe, full or half full
R = D/4
Required slope
S = (n·Q/(A·R2/3))²

Pumps & pump power

Hydraulic power
Ph = ρ·g·Q·H = Q·Δp
Shaft power
Pshaft = Ph/ηpump
Electrical power
Pel = Pshaft/ηmotor
Pump head
H = Δz + Δp/(ρ·g) + hL
System losses
hL = (f·L/D + ΣK)·V²/(2g)

Time value of money

Future value
FV = PV·(1 + i)n
Present value
PV = FV/(1 + i)n
Several periods per year
i = r/m, N = m·n
Annuity, present value
PV = PMT·[1 − (1 + i)−n]/i
Annuity, future value
FV = PMT·[(1 + i)n − 1]/i

Method

  1. Draw a timeline with every cash flow and its timing.
  2. Match the rate to the period: a monthly rate for monthly payments.
  3. Use FV = PV·(1 + i)ⁿ for single amounts and the annuity formulas for equal payments.
  4. Check the sign and the order of magnitude of the answer.

NPV & IRR

Net present value
NPV = −C0 + Σ CFt/(1 + r)t
Equal cash flows
NPV = −C0 + CF·[1 − (1 + r)−n]/r
Internal rate of return
the r at which NPV = 0
Decision
accept when NPV > 0 (or IRR > required return)

Method

  1. List all cash flows with their year; the investment at year 0 is negative.
  2. Discount each cash flow: CFt/(1 + r)t.
  3. Add them up to get the NPV. Positive means the project earns more than r.
  4. For the IRR, find the rate that makes NPV zero by trial or interpolation.

Normal distribution

z-score
z = (x − μ)/σ
Below x
P(X < x) = Φ(z)
Above x
P(X > x) = 1 − Φ(z)
Between
Φ(z2) − Φ(z1)
Percentile
x = μ + z·σ

Method

  1. Convert the value to a z-score: z = (x − μ)/σ.
  2. Look up Φ(z), the area to the left of z.
  3. For the area to the right use 1 − Φ(z); for an interval subtract the two left areas.
  4. For a percentile, work backwards: find z for the area, then x = μ + z·σ.

2Practice problems

1.Beam support reactionsMedium
P1​ = 40 kNP2​ = 40 kNABRA​ = ?RB​5 m1 m4 m

The simply supported beam has a pin at A and a roller at B. Find the vertical support reaction RA.

L = 10 mP1 = 40 kN at 5 mP2 = 40 kN at 6 m
RA = kN
2.Beam support reactionsHard
w = 3 kN/mP = 50 kNABRA​RB​ = ?3.5 m0.5 m2 m

The simply supported beam has a pin at A and a roller at B. Find the vertical support reaction RB.

L = 6 mP = 50 kN at 3.5 mw = 3 kN/m from 4 to 6 m
RB = kN
3.Truss: method of jointsMedium
ABBCACACB30 kN4 m1 m3 m

Use the method of joints to find the force FAB in member AB. Give tension as positive and compression as negative.

span = 4 mheight = 3 mB is 1 m from Avertical load = 30 kN
FAB = kN
4.Truss: method of jointsHard
ABBCACACB10 kN30 kN8 m2 m2 m

Use the method of joints to find the force FBC in member BC. Give tension as positive and compression as negative.

span = 8 mheight = 2 mB is 2 m from Avertical load = 10 kNhorizontal load = 30 kN ←
FBC = kN
5.Shear force & bending momentMedium
w = 3 kN/mABsection4.5 m1.5 m

Find the bending moment Mx at the section x = 4.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 6 mw = 3 kN/m from 0 to 6 mx = 4.5 m
Mx = kN·m
6.Shear force & bending momentHard
w = 5 kN/mP = 60 kNABsection7 m1 m

Find the bending moment Mx at the section x = 7 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 8 mP = 60 kN at 7 mw = 5 kN/m from 0 to 8 mx = 7 m
Mx = kN·m
7.Beam deflectionMedium
w = 12 kN/mP = 24 kNABδ4 m

A cantilever carries a uniformly distributed load w over its whole length and a point load P at its free end. Using superposition, find the deflection δ at the free end.

P = 24 kNw = 12 kN/mL = 4 mE = 200 GPa (steel)I = 57 × 10⁶ mm⁴
δ = mm
8.Beam deflectionHard
P = 25 kNAB2.5 m2.5 m

A propped cantilever is fixed at A and simply supported (propped) at B. It carries a point load P at midspan. EI is constant. Find the reaction RB at the prop.

L = 5 mP = 25 kN at 2.5 m
RB = kN
9.Column bucklingMedium
PL = 6 md = 80 mmcross-section

A column of length L made of steel is fixed at the base and pinned at the top. Using Euler’s formula, find its critical buckling load Pcr.

L = 6 mE = 200 GPa (steel)d = 80 mm
Pcr = kN
10.Column bucklingHard
P = 30 kNL = 6 md = ?cross-section

A solid round column of length L made of aluminium is fixed at the base and pinned at the top. It must carry 30 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.

P = 30 kNn = 3L = 6 mE = 70 GPa (aluminium)
d = mm
11.Centroid & second moment of areaMedium
12060t = 12ȳ = ?dimensions in mm

A channel section lies with its open side up: a base plate 120 mm wide with two upright legs, 60 mm high overall. Base and legs are all 12 mm thick. Find the height ȳ of the centroid above the bottom edge.

b = 120 mmh = 60 mmt = 12 mm
ȳ = mm
12.Centroid & second moment of areaHard
2403012020xM = 30 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 30 kN·m. Find the bending stress σbottom at the bottom edge.

bf = 240 mmtf = 30 mmtw = 20 mmhw = 120 mmM = 30 kN·m
σbottom = MPa
13.Effective stress in soilMedium
sandγd​ = 15 kN/m³γsat​ = 20.5 kN/m³11 mwater tableXz = 7 m

For the soil profile shown, find the pore water pressure u at point X.

z = 7 mzw = 2 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 20.5 kN/m³
u = kPa
14.Effective stress in soilHard
sandγd​ = 16.5 kN/m³γsat​ = 19.5 kN/m³3 mclayγsat​ = 17.5 kN/m³7 mwater tableXz = 6.5 m

For the soil profile shown, find the vertical effective stress σ′ at point X.

z = 6.5 mzw = 2 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 19.5 kN/m³clay: γsat = 17.5 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 40 kPasandclayCc​ = 0.35, Cr​ = 0.04e0​ = 1.2σ′0​ = 115 kPaσ′p​ = 145 kPa6.5 mwater table

A 6.5 m thick overconsolidated clay layer has Cc = 0.35, Cr = 0.04 and e₀ = 1.2. At its mid-depth the effective vertical stress is 115 kPa and the preconsolidation pressure is 145 kPa. A new building adds 40 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 6.5 mCc = 0.35Cr = 0.04e0 = 1.2σ′0 = 115 kPaσ′p = 145 kPaΔσ = 40 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 5 mcv​ = 1.5 m²/year5 mimpervious rockwater table

A clay layer 5 m thick has a coefficient of consolidation cv = 1.5 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 70% average consolidation the time factor is Tv = 0.403. How many years t does the layer take to reach 70% consolidation?

H = 5 mcv = 1.5 m²/yearU = 70%Tv = 0.403single drainage
t = years
17.Hydrostatic forceMedium
gated = 1.5 mH = 1.5 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of water, with its top edge 1.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 1.5 mH = 1.5 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 0.5 mH = 1.5 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of glycerin, with its top edge 0.5 m below the surface. Find the depth ycp of the centre of pressure below the surface.

d = 0.5 mH = 1.5 mb = 2 mρ = 1260 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
V = 2.9 m/sD = 150 mmL = 200 mf = 0.028

Water (ρ = 1000 kg/m³) flows at 2.9 m/s through a horizontal pipe, 200 m long, with an inside diameter of 150 mm. Use the Darcy friction factor f = 0.028 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 2.9 m/sL = 200 mD = 150 mmf = 0.028ρ = 1000 kg/m³
Δp = kPa
20.Pipe friction & head lossHard
K = 5Δz = 9 mL = 150 m, D = 250 mm, f = 0.0253× bend (K = 0.3)

Two open reservoirs are joined by a pipe 150 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.025. The water surface of the upper reservoir is 9 m above that of the lower one. The minor losses are a square-edged entrance (K = 0.5), 3 bends (K = 0.3 each), a valve (K = 5) and the exit into the lower reservoir (K = 1.0). Use g = 9.81 m/s². Find the flow rate Q in L/s.

Δz = 9 mL = 150 mD = 250 mmf = 0.025Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 5Kexit = 1.0
Q = L/s
21.Open-channel flow (Manning)Medium
b = 3.5 my = 1.6 m1 : 1n = 0.014, S = 0.0015

A trapezoidal unfinished concrete channel has a bottom width of 3.5 m and side slopes of 1:1 (horizontal:vertical). Water flows uniformly 1.6 m deep. Manning n = 0.014 and the bed slope is S = 0.0015. Find the flow rate Q in m³/s.

b = 3.5 my = 1.6 mz = 1n = 0.014S = 0.0015
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 3.5 my = 2.4 mn = 0.022, Q = 21 m³/s

A rectangular clean earth channel 3.5 m wide must carry 21 m³/s in uniform flow at a depth of 2.4 m. Manning n = 0.022. Find the required bed slope S (in m/m).

Q = 21 m³/sb = 3.5 my = 2.4 mn = 0.022
S = m/m
23.Pumps & pump powerMedium
PQ = 25 L/sH = 16 m

A pump delivers 25 L/s of water (ρ = 1000 kg/m³) against a head of 16 m. The pump efficiency is 85% and the electric motor driving it has an efficiency of 92%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 25 L/sH = 16 mηpump = 85%ηmotor = 92%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
PQ = 100 L/sΔz = 9 mL = 150 m, D = 250 mm, f = 0.022, ΣK = 8

A pump moves 100 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 9 m higher. The pipe is 150 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.022; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². Find the head H the pump must add.

Q = 100 L/sΔz = 9 mL = 150 mD = 250 mmf = 0.022ΣK = 8
H = m
25.Time value of moneyMedium
years012345PV = ?€5 000

You need €5 000 in 5 years. An account pays 3.6% per year, compounded quarterly. How much must you deposit today? Find the present value PV.

FV = €5 0003.6% / 4n = 5
PV = €
26.Time value of moneyHard
months01…96…300€300 000AB = ?A7.2% / 12

A mortgage of €300 000 is repaid with equal monthly payments over 25 years at 7.2% per year, compounded monthly. How much is still owed just after the payment at the end of year 8? Find the outstanding balance B.

P = €300 0007.2% / 12N = 300k = 96
B = €
27.NPV & IRRMedium
years0123456€60 000€1 500€1 500€1 500€1 500€1 500€1 500r = 6%, EAC = ?

A machine costs €60 000 today, lasts 6 years and costs €1 500 per year to run (paid at the end of each year). The cost of capital is 6%. Find its equivalent annual cost EAC.

C0 = €60 000M = €1 500n = 6r = 6%
EAC = €
28.NPV & IRRHard
years0123−25 00010 00010 50014 000

A project costs €25 000 and returns €10 000, €10 500, €14 000 at the end of years 1 to 3. Cash flows can be reinvested at the cost of capital of 12%. Find the modified internal rate of return MIRR in percent.

r = 12%CF0 = −25 000CF1 = 10 000CF2 = 10 500CF3 = 14 000
MIRR = %
29.Normal distributionMedium
2338.3P = ?

The delivery times are normally distributed with mean 32 min and standard deviation 6 min. What fraction lies between 23 and 38.3 min? Give P as a decimal.

μ = 32σ = 6x1 = 23x2 = 38.3
P =
30.Normal distributionHard
10 g0X − Y?

The mass X of a product from line 1 and Y from line 2 are independent and normal: X has mean 500 g and standard deviation 8 g, Y has mean 490 g and standard deviation 6 g. Find the probability P that X is greater than Y. Round z to two decimals.

μX = 500 g, σX = 8 gμY = 490 g, σY = 6 g
P =

3Solutions

1.Beam support reactions

Answer: RA = 36 kN

Static equilibrium: a body at rest has ΣFx = 0, ΣFy = 0 and ΣM = 0 about any point. Taking moments about one support removes that support’s reaction from the equation.

P1​ = 40 kNP2​ = 40 kNABRA​RB​5 m1 m4 m

Free-body diagram

Replace the supports with reaction forces. A roller gives one vertical reaction; with only vertical loads the pin gives one vertical reaction too.

Equilibrium

Moments about A, counter-clockwise positive. Then vertical force balance.

ΣMA = 0: RB·10 = 40·5 + 40·6
RB = 440/10 = 44 kN
ΣFy = 0: RA = 80 − 44 = 36 kN

Answer

RA = 36 kN
2.Beam support reactions

Answer: RB = 34.17 kN

Static equilibrium: a body at rest has ΣFx = 0, ΣFy = 0 and ΣM = 0 about any point. Taking moments about one support removes that support’s reaction from the equation.

w = 3 kN/mP = 50 kNABRA​RB​3.5 m0.5 m2 m

Free-body diagram

Replace the supports with reaction forces. A roller gives one vertical reaction; with only vertical loads the pin gives one vertical reaction too.

Equilibrium

Moments about A, counter-clockwise positive. Then vertical force balance.

UDL resultant: W = w·ℓ = 3·2 = 6 kN, acting at x̄ = 5 m
ΣMA = 0: RB·6 = 50·3.5 + 3·2·5
RB = 205/6 = 34.17 kN
ΣFy = 0: RA = 56 − 34.17 = 21.83 kN

Answer

RB = 34.17 kN
3.Truss: method of joints

Answer: FAB = −23.72 kN

Method of joints: every pin of a truss is in equilibrium, so ΣFx = 0 and ΣFy = 0 at each joint. Start at a joint with at most two unknown member forces. A negative result means the member is in compression.

ABBCACACB30 kNAy​Cy​

Support reactions

Equilibrium of the whole truss. Moments about A, counter-clockwise positive.

ΣMA = 0: Cy·4 = 30·1 → Cy = 7.5 kN
ΣFy = 0: Ay = 30 − 7.5 = 22.5 kN

Joint A

Assume every member is in tension (pulling away from the joint). Only AB has a vertical component at A.

sin α = 3/3.162 = 0.9487
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −22.5/0.9487 = −23.72 kN

Answer

FAB = −23.72 kN (compression)
4.Truss: method of joints

Answer: FBC = 15.81 kN

Method of joints: every pin of a truss is in equilibrium, so ΣFx = 0 and ΣFy = 0 at each joint. Start at a joint with at most two unknown member forces. A negative result means the member is in compression.

ABBCACACB10 kN30 kNAy​Cy​Ax​

Support reactions

Equilibrium of the whole truss. Moments about A, counter-clockwise positive.

ΣMA = 0: Cy·8 = 10·2 − 30·2 → Cy = −5 kN
ΣFy = 0: Ay = 10 − −5 = 15 kN
ΣFx = 0: Ax = 30 kN

Joint C

The roller gives only a vertical reaction, so joint C has just two unknown member forces. Assume both in tension.

sin γ = 2/6.325 = 0.3162, cos γ = 6/6.325 = 0.9487
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −−5/0.3162 = 15.81 kN

Answer

FBC = 15.81 kN (tension)
5.Shear force & bending moment

Answer: Mx = 10.13 kN·m

Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 3·6 = 18 kN, acting at x̄ = 3 m
ΣMA = 0: RB·6 = 3·6·3
RB = 54/6 = 9 kN
ΣFy = 0: RA = 18 − 9 = 9 kN
w = 3 kN/mABRA​ = 9RB​ = 9section4.5 m1.5 m

Cut at x = 4.5 m and keep the left part

Only forces left of the cut appear. A UDL portion acts as one force at the middle of that portion.

M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 9·4.5 − 3·4.5·2.25 = 10.13 kN·m

Answer

Mx = 10.13 kN·m
6.Shear force & bending moment

Answer: Mx = 70 kN·m

Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 5·8 = 40 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 60·7 + 5·8·4
RB = 580/8 = 72.5 kN
ΣFy = 0: RA = 100 − 72.5 = 27.5 kN
w = 5 kN/mP = 60 kNABRA​ = 27.5RB​ = 72.5section7 m1 m

Cut at x = 7 m and keep the left part

Only forces left of the cut appear. A UDL portion acts as one force at the middle of that portion.

M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 27.5·7 − 5·7·3.5 = 70 kN·m

Answer

Mx = 70 kN·m
7.Beam deflection

Answer: δ = 78.6 mm

Beam deflection: deflections come from integrating the curvature M/(EI) twice. Standard cases are tabulated, for example PL³/(3EI) for a cantilever with an end load and 5wL⁴/(384EI) for a simply supported beam under a full uniform load. Deflections from separate loads add (superposition).

Consistent units

Work in N and mm: P in N, w in N/mm (kN/m = N/mm), L in mm, E in N/mm² (GPa × 1000), I in mm⁴.

P = 24000 N, w = 12 N/mm, L = 4000 mm
EI = 1.14 × 10¹³ N·mm²

Each load on its own

δP = PL³/(3EI) = 24000·4000³/(3·1.14 × 10¹³) = 44.91 mm
δw = wL⁴/(8EI) = 12·4000⁴/(8·1.14 × 10¹³) = 33.68 mm

Add them

δ = 44.91 + 33.68 = 78.6 mm

Answer

δ = 78.6 mm
8.Beam deflection

Answer: RB = 7.813 kN

Beam deflection: deflections come from integrating the curvature M/(EI) twice. Standard cases are tabulated, for example PL³/(3EI) for a cantilever with an end load and 5wL⁴/(384EI) for a simply supported beam under a full uniform load. Deflections from separate loads add (superposition). For a statically indeterminate beam, remove a redundant support and require the deflection there to be zero (compatibility).

Remove the prop

Without the prop the beam is a cantilever. Its free end would deflect under the load.

δload = P(L/2)²(3L − L/2)/(6EI) = 5PL³/(48EI)

Compatibility at the prop

The prop force RB alone lifts the free end by RBL³/(3EI). The prop holds B at zero deflection, so the two must cancel. EI cancels out.

RB·L³/(3EI) = 5PL³/(48EI) → RB = 5P/16 = 5·25/16 = 7.813 kN

Answer

RB = 7.813 kN
9.Column buckling

Answer: Pcr = 225 kN

Euler buckling: a slender column becomes unstable at Pcr = π²EI/(KL)², where KL is the effective length: K = 1 for pinned–pinned, 2 for fixed–free, 0.7 for fixed–pinned and 0.5 for fixed–fixed. It buckles about the axis with the smallest I. The formula holds for slender columns, whose critical stress stays below the yield stress.

Smallest second moment of area

A round section has the same I about every axis.

I = πd⁴/64 = π·80⁴/64 = 2.011 × 10⁶ mm⁴

Effective length

KL = 0.7·6000 = 4200 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·2.011 × 10⁶/4200² = 224989 N = 225 kN

Answer

Pcr = 225 kN
10.Column buckling

Answer: d = 82.72 mm

Euler buckling: a slender column becomes unstable at Pcr = π²EI/(KL)², where KL is the effective length: K = 1 for pinned–pinned, 2 for fixed–free, 0.7 for fixed–pinned and 0.5 for fixed–fixed. It buckles about the axis with the smallest I. The formula holds for slender columns, whose critical stress stays below the yield stress.

Required critical load

Pcr = n·P = 3·30000 = 90000 N
KL = 0.7·6000 = 4200 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·90000·4200²/(π³·70000))^(1/4) = 82.72 mm

Answer

d = 82.72 mm

Check: the slenderness KL/r is 203.1, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: ȳ = 19.33 mm

Composite areas: split the section into rectangles. The centroid is the area-weighted average ȳ = ΣAᵢyᵢ/ΣAᵢ. The second moment of area about the centroidal axis adds each part’s own bh³/12 and its parallel-axis term A·d², where d is the distance from the part’s centroid to the overall centroid. Bending stress is σ = M·y/I.

Split into rectangles

Take the base at full width and the two legs above it (height h − t), so nothing is counted twice.

base: A1 = 120·12 = 1440 mm², y1 = 6 mm
two legs: A2 = 2·12·48 = 1152 mm², y2 = 12 + 48/2 = 36 mm

Centroid

ȳ = (1440·6 + 1152·36)/2592 = 19.33 mm

Answer

ȳ = 19.33 mm
12.Centroid & second moment of area

Answer: σbottom = 257.5 MPa

Composite areas: split the section into rectangles. The centroid is the area-weighted average ȳ = ΣAᵢyᵢ/ΣAᵢ. The second moment of area about the centroidal axis adds each part’s own bh³/12 and its parallel-axis term A·d², where d is the distance from the part’s centroid to the overall centroid. Bending stress is σ = M·y/I.

Split into two rectangles

Measure every y from the bottom edge.

flange: Af = 240·30 = 7200 mm², yf = 120 + 30/2 = 135 mm
web: Aw = 20·120 = 2400 mm², yw = 120/2 = 60 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (7200·135 + 2400·60)/9600 = 116.3 mm

Parallel-axis theorem

flange: 240·30³/12 + 7200·(135 − 116.3)² = 3.071 × 10⁶ mm⁴
web: 20·120³/12 + 2400·(60 − 116.3)² = 1.047 × 10⁷ mm⁴
Ix = 3.071 × 10⁶ + 1.047 × 10⁷ = 1.355 × 10⁷ mm⁴

Bending stress

The bottom edge is ȳ from the axis.

y = 116.3 mm
σ = M·y/I = 3 × 10⁷·116.3/1.355 × 10⁷ = 257.5 MPa

Answer

σbottom = 257.5 MPa
13.Effective stress in soil

Answer: u = 49.05 kPa

Effective stress (Terzaghi): the soil skeleton carries σ′ = σ − u. The total stress σ is the weight of everything above the point, Σγ·h, using the dry unit weight above the water table and the saturated unit weight below it. Below the water table the pore water pressure is hydrostatic: u = γw·(depth below the water table).

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·5 = 49.05 kPa

Answer

u = 49.05 kPa
14.Effective stress in soil

Answer: σ′ = 69.6 kPa

Effective stress (Terzaghi): the soil skeleton carries σ′ = σ − u. The total stress σ is the weight of everything above the point, Σγ·h, using the dry unit weight above the water table and the saturated unit weight below it. Below the water table the pore water pressure is hydrostatic: u = γw·(depth below the water table).

Total stress

Add the weight of each soil band above X. Above the water table use the dry unit weight, below it the saturated one.

σ = γd·2 + γsat,sand·1 + γsat,clay·3.5
σ = 16.5·2 + 19.5·1 + 17.5·3.5 = 113.8 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·4.5 = 44.15 kPa

Effective stress

σ′ = σ − u = 113.8 − 44.15 = 69.6 kPa

Answer

σ′ = 69.6 kPa
15.Consolidation settlement

Answer: S = 41.85 mm

Primary consolidation of a clay layer of thickness H, using the effective stress at the middle of the layer: σ′f = σ′0 + Δσ. Normally consolidated clay: S = Cc·H/(1 + e0)·log₁₀(σ′f/σ′0). Overconsolidated clay recompresses along Cr up to the preconsolidation pressure σ′p and follows Cc only beyond it. Time: t = Tv·Hdr²/cv, where the drainage path Hdr is H/2 when water can leave at the top and bottom, and H when only one side drains.

Compare with the preconsolidation pressure

σ′f = 115 + 40 = 155 kPa > 145 kPa

Settlement

Recompression up to σ′p, virgin compression beyond it.

S = 0.04·6.5/(1 + 1.2)·log₁₀(145/115) + 0.35·6.5/(1 + 1.2)·log₁₀(155/145)
S = 11.9 + 29.95 = 41.85 mm

Answer

S = 41.85 mm
16.Consolidation settlement

Answer: t = 6.717 years

Primary consolidation of a clay layer of thickness H, using the effective stress at the middle of the layer: σ′f = σ′0 + Δσ. Normally consolidated clay: S = Cc·H/(1 + e0)·log₁₀(σ′f/σ′0). Overconsolidated clay recompresses along Cr up to the preconsolidation pressure σ′p and follows Cc only beyond it. Time: t = Tv·Hdr²/cv, where the drainage path Hdr is H/2 when water can leave at the top and bottom, and H when only one side drains.

Drainage path

Hdr = H = 5 m

Time

t = Tv·Hdr²/cv = 0.403·5²/1.5 = 6.717 years

Answer

t = 6.717 years
17.Hydrostatic force

Answer: F = 99.33 kN

Hydrostatic force on a plane surface: F = ρ·g·yc·A. It acts at the centre of pressure, ycp = yc + Ic/(ycA), which always lies below the centroid.

Centroid depth and area

yc = d + H/2 = 1.5 + 1.5/2 = 2.25 m
A = H·b = 1.5·3 = 4.5 m²
gated = 1.5 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2.25·4.5 = 99.33 kN

Answer

F = 99.33 kN
18.Hydrostatic force

Answer: ycp = 1.4 m

Hydrostatic force on a plane surface: F = ρ·g·yc·A. It acts at the centre of pressure, ycp = yc + Ic/(ycA), which always lies below the centroid.

Centroid depth and area

yc = d + H/2 = 0.5 + 1.5/2 = 1.25 m
A = H·b = 1.5·2 = 3 m²
gated = 0.5 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·1.25·3 = 46.35 kN

Centre of pressure

Pressure grows with depth, so the resultant acts below the centroid.

Ic = b·H³/12 = 2·1.5³/12 = 0.5625 m⁴
ycp = yc + Ic/(yc·A) = 1.25 + 0.5625/(1.25·3) = 1.4 m

Answer

ycp = 1.4 m
19.Pipe friction & head loss

Answer: Δp = 157 kPa

Pipe flow: the Reynolds number Re = V·D/ν = ρ·V·D/μ tells laminar flow (Re below about 2000) from turbulent flow (above about 4000). Friction along a pipe costs the Darcy–Weisbach head loss hf = f·(L/D)·V²/(2g). Fittings, valves, the entrance and the exit add minor losses hm = ΣK·V²/(2g). Between two open reservoir surfaces the energy equation gives Δz = hf + hm, with the exit loss K = 1 included.

Head loss

hf = f·(L/D)·V²/(2g) = 0.028·(200/0.15)·2.9²/(2·9.81) = 16 m

Pressure drop

The pipe is horizontal and the velocity does not change, so the energy equation reduces to Δp = ρ·g·hf.

Δp = ρ·g·hf = 1000·9.81·16 = 156987 Pa = 157 kPa

Answer

Δp = 157 kPa
20.Pipe friction & head loss

Answer: Q = 137.8 L/s

Pipe flow: the Reynolds number Re = V·D/ν = ρ·V·D/μ tells laminar flow (Re below about 2000) from turbulent flow (above about 4000). Friction along a pipe costs the Darcy–Weisbach head loss hf = f·(L/D)·V²/(2g). Fittings, valves, the entrance and the exit add minor losses hm = ΣK·V²/(2g). Between two open reservoir surfaces the energy equation gives Δz = hf + hm, with the exit loss K = 1 included.

Loss coefficients

f·L/D = 0.025·150/0.25 = 15
ΣK = 0.5 + 3·0.3 + 5 + 1.0 = 7.4

Energy equation

Both surfaces are open to the air and practically at rest, so all of Δz is lost in the pipe.

9 = (15 + 7.4)·V²/(2·9.81)
V = √(2·9.81·9/22.4) = 2.808 m/s

Flow rate

Q = V·π·D²/4 = 2.808·0.04909 = 0.1378 m³/s = 137.8 L/s

Answer

Q = 137.8 L/s
21.Open-channel flow (Manning)

Answer: Q = 22.83 m³/s

Manning’s equation (SI): for uniform flow in an open channel V = (1/n)·R2/3·S1/2 and Q = A·V, with n the roughness coefficient, S the bed slope (m/m) and R = A/P the hydraulic radius: flow area divided by wetted perimeter. Only the boundary in contact with the water counts in P, not the free surface. Rectangle: A = b·y, P = b + 2y. Trapezoid with side slopes z:1 (horizontal:vertical): A = (b + z·y)·y, P = b + 2y·√(1 + z²). A circular pipe flowing full or half full has R = D/4.

Geometry

A = (b + z·y)·y = (3.5 + 1·1.6)·1.6 = 8.16 m²
P = b + 2y·√(1 + z²) = 3.5 + 2·1.6·√(1 + 1²) = 8.025 m
R = A/P = 1.017 m

Velocity

V = (1/0.014)·1.0172/3·0.00151/2 = 2.797 m/s

Flow rate

Q = A·V = 8.16·2.797 = 22.83 m³/s

Answer

Q = 22.83 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.002977 m/m

Manning’s equation (SI): for uniform flow in an open channel V = (1/n)·R2/3·S1/2 and Q = A·V, with n the roughness coefficient, S the bed slope (m/m) and R = A/P the hydraulic radius: flow area divided by wetted perimeter. Only the boundary in contact with the water counts in P, not the free surface. Rectangle: A = b·y, P = b + 2y. Trapezoid with side slopes z:1 (horizontal:vertical): A = (b + z·y)·y, P = b + 2y·√(1 + z²). A circular pipe flowing full or half full has R = D/4.

Geometry

A = b·y = 3.5·2.4 = 8.4 m²
P = b + 2y = 3.5 + 2·2.4 = 8.3 m
R = A/P = 1.012 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.022·21/(8.4·1.008) = 0.05456
S = 0.05456² = 0.002977

Answer

S = 0.002977

That is a fall of 2.977 m per kilometre.

23.Pumps & pump power

Answer: Pel = 5.018 kW

Pump power: the power given to the water is the hydraulic power Ph = ρ·g·Q·H = Q·Δp. The shaft must deliver more because the pump loses some: Pshaft = Ph/ηpump, and the motor draws Pel = Pshaft/ηmotor. The pump head H follows from the energy equation: static lift + pressure head + all friction and minor losses.

Hydraulic power

Ph = ρ·g·Q·H = 1000·9.81·0.025·16 = 3.924 kW

Shaft power

Pshaft = 3.924/0.85 = 4.616 kW

Electrical power

Pel = 4.616/0.92 = 5.018 kW

Answer

Pel = 5.018 kW
24.Pumps & pump power

Answer: H = 13.48 m

Pump power: the power given to the water is the hydraulic power Ph = ρ·g·Q·H = Q·Δp. The shaft must deliver more because the pump loses some: Pshaft = Ph/ηpump, and the motor draws Pel = Pshaft/ηmotor. The pump head H follows from the energy equation: static lift + pressure head + all friction and minor losses.

Velocity

V = Q/A = 0.1/0.04909 = 2.037 m/s
V²/(2g) = 0.2115 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (13.2 + 8)·0.2115 = 4.484 m

Pump head

Both surfaces are open and practically at rest, so pressure and velocity terms drop out.

H = Δz + hL = 9 + 4.484 = 13.48 m

Answer

H = 13.48 m
25.Time value of money

Answer: PV = 4180 €

Time value of money: money today is worth more than the same amount later, because it can earn interest. With interest rate i per period, an amount grows as FV = PV·(1 + i)n. A series of equal payments (an annuity) is valued by adding up each payment, which gives the annuity formulas.

Rate and number of periods

i = 0.036000000000000004/4 = 0.009
N = 4·5 = 20

Present value

PV = FV/(1 + i)N = 5 000/1.196 = €4 179.72

Answer

PV = €4 179.72
26.Time value of money

Answer: B = 253609 €

Time value of money: money today is worth more than the same amount later, because it can earn interest. With interest rate i per period, an amount grows as FV = PV·(1 + i)n. A series of equal payments (an annuity) is valued by adding up each payment, which gives the annuity formulas.

Monthly payment

i = 0.006, N = 300
A = 300 000·0.006/(1 − (1 + 0.006)−300) = €2 158.77

Present value of the remaining payments

Whatever is still owed must be exactly paid off by the remaining payments.

N − k = 300 − 96 = 204
B = 2159·(1 − (1 + 0.006)−204)/0.006 = €253 608.59

Answer

B = €253 608.59
27.NPV & IRR

Answer: EAC = 13702 €

Equivalent annual cost: spread the present value of all costs over the life as an equal yearly amount (an annuity): EAC = PV·r/(1 − (1 + r)⁻ⁿ). It lets you compare machines with different lives.

Annuity factor

(1 − 1.06−6)/0.06 = 4.917

Annualised purchase price

60 000/4.917 = 12 201.76

EAC

EAC = 12 201.76 + 1 500 = €13 701.76

Answer

EAC = €13 701.76
28.NPV & IRR

Answer: MIRR = 15.28 %

Modified IRR: compound every inflow forward to the end of the project at the reinvestment rate (usually the cost of capital) to get the terminal value TV. MIRR is the rate that turns the initial investment into TV: MIRR = (TV/C₀)^(1/n) − 1.

Terminal value of the inflows

10 000·1.122 = 12 544.00
10 500·1.121 = 11 760.00
14 000·1.120 = 14 000.00
TV = 38 304.00

MIRR

MIRR = (38 304.00/25 000)1/3 − 1 = 15.28%

Answer

MIRR = 15.28%
29.Normal distribution

Answer: P = 0.7863

Normal distribution: convert a value x to a z-score, z = (x − μ)/σ, which counts standard deviations from the mean. A z-table (or Φ(z)) gives the area to the left of z, which is P(X < x). The area to the right is 1 − Φ(z), and the area between two values is the difference of their two areas.

z-scores

z₁ = (23 − 32)/6 = −1.5
z₂ = (38.3 − 32)/6 = 1.05

Area between

P = Φ(1.05) − Φ(−1.5) = 0.8531 − 0.06681 = 0.7863

Answer

P = 0.7863
30.Normal distribution

Answer: P = 0.8413

Sums and differences of normal variables: if X and Y are independent and normal, X + Y and X − Y are normal too. Means add or subtract: E(X ± Y) = μX ± μY. Variances always add, also for a difference: Var(X ± Y) = σX² + σY², so σ = √(σX² + σY²). Standard deviations never add directly. The total of n independent items with the same distribution has mean n·μ and standard deviation σ·√n. Then standardise as usual: z = (x − mean)/σ and read Φ(z).

Distribution of the difference

μ = 500 − 490 = 10 g, σ = 10 g

Standardise

z = (0 − 10)/10 = −1

Probability

P = 1 − Φ(−1) = 0.8413

Answer

P = 0.8413

This is independent practice material. ExamProblems is not affiliated with or endorsed by the organisation that runs this exam, and the exam name is used only to describe the content. The FE exam is run by NCEES, which is not affiliated with ExamProblems and does not endorse it.

ExamProblems · examproblems.com/courses/fe-exam-civil