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​ = 60 kNP2​ = 35 kNABRA​ = ?RB​1 m2 m7 m

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

L = 10 mP1 = 60 kN at 1 mP2 = 35 kN at 3 m
RA = kN
2.Beam support reactionsHard
w = 6 kN/mP = 40 kNABRA​ = ?RB​2.5 m3.5 m

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

L = 6 mP = 40 kN at 2.5 mw = 6 kN/m from 0 to 6 m
RA = kN
3.Truss: method of jointsMedium
ABBCACACB30 kN5 m4 m2 m

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

span = 5 mheight = 2 mB is 4 m from Avertical load = 30 kN
FAB = kN
4.Truss: method of jointsHard
ABBCACACB40 kN20 kN4 m3 m4 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 = 4 mB is 3 m from Avertical load = 40 kNhorizontal load = 20 kN →
FAB = kN
5.Shear force & bending momentMedium
w = 8 kN/mP = 30 kNABsection0.5 m0.5 m3 m

The cantilever is fixed at A. It carries a uniformly distributed load w over its whole length and a point load P at 1 m from A. Find the bending moment Mx at the section x = 0.5 m from the fixed support A. Use sagging moments positive and upward shear on the left face positive.

L = 4 mP = 30 kN at 1 mw = 8 kN/m from 0 to 4 mx = 0.5 m
Mx = kN·m
6.Shear force & bending momentHard
w = 12 kN/mAB2 m6 m2 m

The simply supported beam carries a uniformly distributed load over part of its span. Find the maximum bending moment Mmax in the beam.

L = 10 mw = 12 kN/m from 2 to 8 m
Mmax = kN·m
7.Beam deflectionMedium
w = 12 kN/mδL = 2.5 m

A cantilever carries a uniformly distributed load w over its whole length. Find the deflection δ at the free end.

w = 12 kN/mL = 2.5 mE = 11 GPa (timber)I = 160 × 10⁶ mm⁴
δ = mm
8.Beam deflectionHard
w = 8 kN/mP = 4 kNδL = 4 m

A simply supported beam carries a uniformly distributed load w and a point load P at midspan. Using superposition, find the midspan deflection δmax.

P = 4 kNw = 8 kN/mL = 4 mE = 11 GPa (timber)I = 84 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 6 md = 50 mmcross-section

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

L = 6 mE = 70 GPa (aluminium)d = 50 mm
Pcr = kN
10.Column bucklingHard
PL = 1 md = 25 mmcross-section

A column of length L made of steel is pinned at both ends. Find its slenderness and the critical buckling stress σcr from Euler’s formula.

L = 1 mE = 200 GPa (steel)d = 25 mm
σcr = MPa
11.Centroid & second moment of areaMedium
260160t = 18ȳ = ?dimensions in mm

A channel section lies with its open side up: a base plate 260 mm wide with two upright legs, 160 mm high overall. Base and legs are all 18 mm thick. Find the height ȳ of the centroid above the bottom edge.

b = 260 mmh = 160 mmt = 18 mm
ȳ = mm
12.Centroid & second moment of areaHard
200 mm300 mm210 mm30 × 40xIx​ = ?

A 200 mm × 300 mm plate has a rectangular cut-out 30 mm wide and 40 mm high, centred on the vertical centre line with its centre 210 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 200 mmh = 300 mmcut-out: 30 × 40 mmhole centre: y = 210 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
sandγd​ = 15.5 kN/m³γsat​ = 20 kN/m³8 mwater tableXz = 6 m

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

z = 6 mzw = 4 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 20 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 15 kN/m³γsat​ = 19 kN/m³6 mclayγsat​ = 17.5 kN/m³7 mwater tableXz = 9.5 m

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

z = 9.5 mzw = 4 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 19 kN/m³clay: γsat = 17.5 kN/m³
σ = kPa
15.Consolidation settlementMedium
Δσ = 120 kPasandclayCc​ = 0.5, Cr​ = 0.03e0​ = 0.9σ′0​ = 110 kPaσ′p​ = 170 kPa3.5 mwater table

A 3.5 m thick overconsolidated clay layer has Cc = 0.5, Cr = 0.03 and e₀ = 0.9. At its mid-depth the effective vertical stress is 110 kPa and the preconsolidation pressure is 170 kPa. A new building adds 120 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 3.5 mCc = 0.5Cr = 0.03e0 = 0.9σ′0 = 110 kPaσ′p = 170 kPaΔσ = 120 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 8.5 mcv​ = 0.5 m²/year8.5 mimpervious rockwater table

A clay layer 8.5 m thick has a coefficient of consolidation cv = 0.5 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 80% average consolidation the time factor is Tv = 0.567. How many years t does the layer take to reach 80% consolidation?

H = 8.5 mcv = 0.5 m²/yearU = 80%Tv = 0.567single drainage
t = years
17.Hydrostatic forceMedium
gated = 1 mH = 1 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of water, with its top edge 1 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 1 mH = 1 mb = 1.5 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 1 mH = 1 m

A vertical rectangular gate 1 m wide sits in the wall of a tank of seawater, with its top edge 1 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 1 mH = 1 mb = 1 mρ = 1025 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
V = 2.9 m/sD = 200 mmL = 1000 mf = 0.015

Water (ρ = 1000 kg/m³) flows at 2.9 m/s through a horizontal pipe, 1000 m long, with an inside diameter of 200 mm. Use the Darcy friction factor f = 0.015 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 2.9 m/sL = 1000 mD = 200 mmf = 0.015ρ = 1000 kg/m³
Δp = kPa
20.Pipe friction & head lossHard
K = 10Δz = 30 mL = 200 m, D = 200 mm, f = 0.022× bend (K = 0.3)

Two open reservoirs are joined by a pipe 200 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.02. The water surface of the upper reservoir is 30 m above that of the lower one. The minor losses are a square-edged entrance (K = 0.5), 2 bends (K = 0.3 each), a valve (K = 10) 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 = 30 mL = 200 mD = 200 mmf = 0.02Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 10Kexit = 1.0
Q = L/s
21.Open-channel flow (Manning)Medium
b = 3 my = 1.4 m2 : 1n = 0.015, S = 0.001

A trapezoidal brickwork channel has a bottom width of 3 m and side slopes of 2:1 (horizontal:vertical). Water flows uniformly 1.4 m deep. Manning n = 0.015 and the bed slope is S = 0.001. Find the flow rate Q in m³/s.

b = 3 my = 1.4 mz = 2n = 0.015S = 0.001
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 2.5 my = 2.2 mn = 0.03, Q = 3.5 m³/s

A rectangular grass-lined earth channel 2.5 m wide must carry 3.5 m³/s in uniform flow at a depth of 2.2 m. Manning n = 0.03. Find the required bed slope S (in m/m).

Q = 3.5 m³/sb = 2.5 my = 2.2 mn = 0.03
S = m/m
23.Pumps & pump powerMedium
PQ = 150 L/sH = 14 m

A pump with an efficiency of 78% delivers 150 L/s of water (ρ = 1000 kg/m³) against a head of 14 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 150 L/sH = 14 mη = 78%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 100 L/sΔz = 7 mL = 100 m, D = 250 mm, f = 0.018, 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 7 m higher. The pipe is 100 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.018; 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 = 7 mL = 100 mD = 250 mmf = 0.018ΣK = 8
H = m
25.Time value of moneyMedium
periods0123411 + EAR = ?16% / 4

A credit card charges a nominal interest rate of 16% per year, compounded quarterly. Find the effective annual rate EAR in percent.

r = 16%m = 4
EAR = %
26.Time value of moneyHard
months0123…324€200€200€200FV = ?

You save €200 at the end of every month for 27 years. The account pays 4.8% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €2004.8% / 12N = 324
FV = €
27.NPV & IRRMedium
years01234−45 00013 00013 00010 00020 000

An investment of €45 000 gives these cash flows at the end of years 1 to 4: €13 000, €13 000, €10 000, €20 000. The cost of capital is 7.000000000000001%. Find the net present value NPV.

r = 7.000000000000001%CF0 = −45 000CF1 = 13 000CF2 = 13 000CF3 = 10 000CF4 = 20 000
NPV = €
28.NPV & IRRHard
years012−25 00012 50015 500

A project costs €25 000 and returns €12 500, €15 500 at the end of years 1 to 2. Find its internal rate of return IRR in percent.

CF0 = −25 000CF1 = 12 500CF2 = 15 500
IRR = %
29.Normal distributionMedium
26.341.3P = ?

The delivery times are normally distributed with mean 32 min and standard deviation 6 min. What fraction lies between 26.3 and 41.3 min? Give P as a decimal.

μ = 32σ = 6x1 = 26.3x2 = 41.3
P =
30.Normal distributionHard
35455565758595pointstop 85%

The exam scores are normally distributed with mean 65 points and standard deviation 10 points. Drag the cut-off so the shaded top 85% is to the right of it. Find the cut-off x.

μ = 65 pointsσ = 10 points85%
x = points

3Solutions

1.Beam support reactions

Answer: RA = 78.5 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​ = 60 kNP2​ = 35 kNABRA​RB​1 m2 m7 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 = 60·1 + 35·3
RB = 165/10 = 16.5 kN
ΣFy = 0: RA = 95 − 16.5 = 78.5 kN

Answer

RA = 78.5 kN
2.Beam support reactions

Answer: RA = 41.33 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 = 6 kN/mP = 40 kNABRA​RB​2.5 m3.5 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 = 6·6 = 36 kN, acting at x̄ = 3 m
ΣMA = 0: RB·6 = 40·2.5 + 6·6·3
RB = 208/6 = 34.67 kN
ΣFy = 0: RA = 76 − 34.67 = 41.33 kN

Answer

RA = 41.33 kN
3.Truss: method of joints

Answer: FAB = −13.42 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·5 = 30·4 → Cy = 24 kN
ΣFy = 0: Ay = 30 − 24 = 6 kN

Joint A

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

sin α = 2/4.472 = 0.4472
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −6/0.4472 = −13.42 kN

Answer

FAB = −13.42 kN (compression)
4.Truss: method of joints

Answer: FAB = 12.5 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.

ABBCACACB40 kN20 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·4 = 40·3 + 20·4 → Cy = 50 kN
ΣFy = 0: Ay = 40 − 50 = −10 kN
ΣFx = 0: Ax = −20 kN

Joint A

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

sin α = 4/5 = 0.8
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −−10/0.8 = 12.5 kN

Answer

FAB = 12.5 kN (tension)
5.Shear force & bending moment

Answer: Mx = −64 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.

Keep the free-end part

P: −30·0.5 = −15 kN·m
w: −8·3.5²/2 = −49 kN·m
Mx = −15 − 49 = −64 kN·m

Answer

Mx = −64 kN·m

Negative means hogging: tension on the top face.

6.Shear force & bending moment

Answer: Mmax = 126 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. Maximum moment: since dM/dx = V, the bending moment has its peak where the shear force passes through zero, either at a point load or inside a distributed load.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 12·6 = 72 kN, acting at x̄ = 5 m
ΣMA = 0: RB·10 = 12·6·5
RB = 360/10 = 36 kN
ΣFy = 0: RA = 72 − 36 = 36 kN

Zero shear

The shear force starts at RA, stays constant over any unloaded part and falls with slope w inside the load.

RA − w·(x0 − 2) = 0
x0 = 2 + 36/12 = 5 m

Maximum moment

Mmax = RA·x0 − w·(x0 − 2)²/2 = 36·5 − 12·3²/2 = 126 kN·m

Answer

Mmax = 126 kN·m
7.Beam deflection

Answer: δ = 33.29 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.

w = 12 N/mm, L = 2500 mm
EI = 1.76 × 10¹² N·mm²

Deflection

δ = wL⁴/(8EI) = 12·2500⁴/(8·1.76 × 10¹²) = 33.29 mm

Answer

δ = 33.29 mm
8.Beam deflection

Answer: δmax = 34.63 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 = 4000 N, w = 8 N/mm, L = 4000 mm, EI = 9.24 × 10¹¹ N·mm²

Each load on its own

δP = PL³/(48EI) = 4000·4000³/(48·9.24 × 10¹¹) = 5.772 mm
δw = 5wL⁴/(384EI) = 5·8·4000⁴/(384·9.24 × 10¹¹) = 28.86 mm

Add them

δmax = 5.772 + 28.86 = 34.63 mm

Answer

δmax = 34.63 mm
9.Column buckling

Answer: Pcr = 12.02 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·50⁴/64 = 306796 mm⁴

Effective length

KL = 0.7·6000 = 4200 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·306796/4200² = 12016 N = 12.02 kN

Answer

Pcr = 12.02 kN
10.Column buckling

Answer: σcr = 77.11 MPa

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·25⁴/64 = 19175 mm⁴

Radius of gyration and slenderness

A = 490.9 mm²
r = √(I/A) = √(19175/490.9) = 6.25 mm
KL = 1·1000 = 1000 mm
KL/r = 1000/6.25 = 160

Critical stress

σcr = π²E/(KL/r)² = π²·200000/160² = 77.11 MPa

Answer

σcr = 77.11 MPa
11.Centroid & second moment of area

Answer: ȳ = 50.76 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 = 260·18 = 4680 mm², y1 = 9 mm
two legs: A2 = 2·18·142 = 5112 mm², y2 = 18 + 142/2 = 89 mm

Centroid

ȳ = (4680·9 + 5112·89)/9792 = 50.76 mm

Answer

ȳ = 50.76 mm
12.Centroid & second moment of area

Answer: Ix = 445.4 × 10⁶ mm⁴

Sections with holes: treat a hole as a negative area. The centroid is ȳ = (A₁y₁ − A₂y₂)/(A₁ − A₂), with A₁, y₁ for the full plate and A₂, y₂ for the hole. For the second moment of area about the centroidal axis, use the parallel-axis theorem for each part and subtract the hole: I = (Ic1 + A₁d₁²) − (Ic2 + A₂d₂²), where d is the distance from each part's own centroid to the axis through ȳ. A rectangle has Ic = bh³/12 and a circle Ic = πd⁴/64.

Centroid

ȳ = (60000·150 − 1200·210)/(60000 − 1200) = 148.8 mm

Full plate about ȳ

200·300³/12 + 60000·1.224² = 450.1 × 10⁶ mm⁴

Hole about ȳ

30·40³/12 + 1200·61.22² = 4.658 × 10⁶ mm⁴

Subtract

Ix = 445.4 × 10⁶ mm⁴

Answer

Ix = 445.4 × 10⁶ mm⁴
13.Effective stress in soil

Answer: σ′ = 82.38 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·zw + γsat·(z − zw) = 15.5·4 + 20·2 = 102 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·2 = 19.62 kPa

Effective stress

σ′ = σ − u = 102 − 19.62 = 82.38 kPa

Answer

σ′ = 82.38 kPa
14.Effective stress in soil

Answer: σ = 159.3 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·4 + γsat,sand·2 + γsat,clay·3.5
σ = 15·4 + 19·2 + 17.5·3.5 = 159.3 kPa

Answer

σ = 159.3 kPa
15.Consolidation settlement

Answer: S = 131.4 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 = 110 + 120 = 230 kPa > 170 kPa

Settlement

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

S = 0.03·3.5/(1 + 0.9)·log₁₀(170/110) + 0.5·3.5/(1 + 0.9)·log₁₀(230/170)
S = 10.45 + 120.9 = 131.4 mm

Answer

S = 131.4 mm
16.Consolidation settlement

Answer: t = 81.93 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 = 8.5 m

Time

t = Tv·Hdr²/cv = 0.567·8.5²/0.5 = 81.93 years

Answer

t = 81.93 years
17.Hydrostatic force

Answer: F = 22.07 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 + 1/2 = 1.5 m
A = H·b = 1·1.5 = 1.5 m²
gated = 1 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·1.5·1.5 = 22.07 kN

Answer

F = 22.07 kN
18.Hydrostatic force

Answer: F = 15.08 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 + 1/2 = 1.5 m
A = H·b = 1·1 = 1 m²
gated = 1 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 1025·9.81·1.5·1 = 15.08 kN

Answer

F = 15.08 kN
19.Pipe friction & head loss

Answer: Δp = 315.4 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) = 0.015·(1000/0.2)·2.9²/(2·9.81) = 32.15 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 = 1000·9.81·32.15 = 315375 Pa = 315.4 kPa

Answer

Δp = 315.4 kPa
20.Pipe friction & head loss

Answer: Q = 134.5 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 = 0.02·200/0.2 = 20
ΣK = 0.5 + 2·0.3 + 10 + 1.0 = 12.1

Energy equation

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

30 = (20 + 12.1)·V²/(2·9.81)
V = √(2·9.81·30/32.1) = 4.282 m/s

Flow rate

Q = V·π·D²/4 = 4.282·0.03142 = 0.1345 m³/s = 134.5 L/s

Answer

Q = 134.5 L/s
21.Open-channel flow (Manning)

Answer: Q = 15.68 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 + 2·1.4)·1.4 = 8.12 m²
P = b + 2y·√(1 + z²) = 3 + 2·1.4·√(1 + 2²) = 9.261 m
R = A/P = 0.8768 m

Velocity

V = (1/0.015)·0.87682/3·0.0011/2 = 1.931 m/s

Flow rate

Q = A·V = 8.12·1.931 = 15.68 m³/s

Answer

Q = 15.68 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.0004931 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 = 2.5·2.2 = 5.5 m²
P = b + 2y = 2.5 + 2·2.2 = 6.9 m
R = A/P = 0.7971 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.03·3.5/(5.5·0.8597) = 0.02221
S = 0.02221² = 0.0004931

Answer

S = 0.0004931

That is a fall of 0.4931 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 26.41 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 = 1000·9.81·0.15·14 = 20.6 kW

Shaft power

Pshaft = Ph/η = 20.6/0.78 = 26.41 kW

Answer

Pshaft = 26.41 kW
24.Pumps & pump power

Answer: H = 10.22 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) = (7.2 + 8)·0.2115 = 3.215 m

Pump head

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

H = Δz + hL = 7 + 3.215 = 10.22 m

Answer

H = 10.22 m
25.Time value of money

Answer: EAR = 16.99 %

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 per period

r/m = 0.16/4 = 0.04

Compound over one year

EAR = (1 + 0.04)4 − 1 = 1.17 − 1 = 16.99%

Answer

EAR = 16.99%

The EAR is always above the nominal rate when interest compounds more than once a year.

26.Time value of money

Answer: FV = 132261 €

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 rate and number of deposits

i = 0.048/12 = 0.004
N = 12·27 = 324

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 200·(3.645 − 1)/0.004 = €132 260.67

Answer

FV = €132 260.67

You paid in €64 800 yourself; the rest is interest.

27.NPV & IRR

Answer: NPV = 1925 €

Net present value: discount every cash flow back to today with the required rate of return r, then add them up: NPV = Σ CFₜ/(1 + r)ᵗ. A project with NPV > 0 earns more than r and adds value. The internal rate of return (IRR) is the rate at which NPV = 0.

Present value of each cash flow

CF0 = −45 000
CF1/(1 + 0.07)1 = 13 000/1.07 = 12 149.53
CF2/(1 + 0.07)2 = 13 000/1.145 = 11 354.70
CF3/(1 + 0.07)3 = 10 000/1.225 = 8 162.98
CF4/(1 + 0.07)4 = 20 000/1.311 = 15 257.90

Add them up

NPV = €1 925.12

Answer

NPV = €1 925.12

NPV is positive, so the project earns more than the required return.

28.NPV & IRR

Answer: IRR = 7.614 %

Net present value: discount every cash flow back to today with the required rate of return r, then add them up: NPV = Σ CFₜ/(1 + r)ᵗ. A project with NPV > 0 earns more than r and adds value. The internal rate of return (IRR) is the rate at which NPV = 0.

Bracket the IRR

NPV falls as the rate rises, so the IRR lies between a rate with positive NPV and one with negative NPV.

NPV(5%) = 963.72
NPV(10%) = −826.45

Narrow down

Linear interpolation gives a first estimate; repeating it (or a calculator's IRR function) gives the exact rate.

IRR ≈ 5 + 5·963.72/(963.72 − (−826.45)) = 7.692%
exact: NPV(7.614%) = 0 → IRR = 7.614%

Answer

IRR = 7.614%
29.Normal distribution

Answer: P = 0.7684

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 = (26.3 − 32)/6 = −0.95
z₂ = (41.3 − 32)/6 = 1.55

Area between

P = Φ(1.55) − Φ(−0.95) = 0.9394 − 0.1711 = 0.7684

Answer

P = 0.7684
30.Normal distribution

Answer: x = 54.6 points

From an area back to z: Φ(z) is the area to the left of z. For a left-tail area A, find z with Φ(z) = A in the table. A right-tail area A means Φ(z) = 1 − A. A central area A between −z and z leaves (1 − A)/2 in each tail, so Φ(z) = (1 + A)/2. For a value x, use x = μ + zσ.

Area to the left

Φ(z) = 0.15

z from the table

z ≈ −1.04

Back to the original units

x = 65 − 1.04·10 = 54.6 points

Answer

x = 54.6 points

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