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
w = 5 kN/mP = 45 kNABMA​ = ?6 m

The cantilever beam is fixed to the wall at A. It carries a uniformly distributed load w along its whole length and a point load P at 6 m from the wall. Find the magnitude of the reaction moment MA at the wall.

L = 6 mP = 45 kN at 6 mw = 5 kN/m from 0 to 6 m
MA = kN·m
2.Beam support reactionsHard
w0​ = 4 kN/mP = 50 kNABMA​ = ?2.5 m1.5 m

The cantilever beam is fixed to the wall at A. It carries a linearly varying load that is zero at the wall and rises to 4 kN/m at the free end B, plus a point load P at 2.5 m from the wall. Find the magnitude of the reaction moment MA at the wall.

L = 4 mw0 = 4 kN/mP = 50 kN at 2.5 m
MA = kN·m
3.Truss: method of jointsMedium
ABCDEFGH10 kN4 × 4 m4 m

Exactly one member of this truss carries no force under these loads. Which is the zero-force member? Click it in the diagram.

G: 10 kN ↓
  1. 1member AB
  2. 2member BC
  3. 3member CD
  4. 4member DE
  5. 5member FG
  6. 6member GH
  7. 7member AF
  8. 8member HE
  9. 9member BF
  10. 10member CG
  11. 11member DH
  12. 12member BG
  13. 13member DG
4.Truss: method of jointsHard
ABCDEFGH15 kN15 kN40 kN30 kN35 kN4 × 3 m4 m

Exactly one member of this truss carries no force under these loads. Which is the zero-force member? Click it in the diagram.

D: 15 kN ↓F: 15 kN ↓F: 40 kN →G: 30 kN ↓H: 35 kN ↓
  1. 1member AB
  2. 2member BC
  3. 3member CD
  4. 4member DE
  5. 5member FG
  6. 6member GH
  7. 7member AF
  8. 8member HE
  9. 9member BF
  10. 10member CG
  11. 11member DH
  12. 12member FC
  13. 13member HC
5.Shear force & bending momentMedium
w = 10 kN/mABsection1.5 m2.5 m

Find the bending moment Mx at the section x = 1.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 4 mw = 10 kN/m from 0 to 4 mx = 1.5 m
Mx = kN·m
6.Shear force & bending momentHard
w = 8 kN/mP = 50 kNABsection3.5 m3.5 m3 m

Find the bending moment Mx at the section x = 3.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 10 mP = 50 kN at 7 mw = 8 kN/m from 0 to 10 mx = 3.5 m
Mx = kN·m
7.Beam deflectionMedium
w = 8 kN/mδL = 1.5 m

A simply supported beam carries a uniformly distributed load w over its whole span. Find the maximum deflection δmax, at midspan.

w = 8 kN/mL = 1.5 mE = 11 GPa (timber)I = 23 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 12 kN/mP = 21 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 = 21 kNw = 12 kN/mL = 4 mE = 200 GPa (steel)I = 57 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 4 md = 80 mmcross-section

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

L = 4 mE = 200 GPa (steel)d = 80 mm
Pcr = kN
10.Column bucklingHard
PL = 2.5 md = 40 mmcross-section

A column of length L made of steel is fixed at the base and free at the top. Find its slenderness and the critical buckling stress σcr from Euler’s formula.

L = 2.5 mE = 200 GPa (steel)d = 40 mm
σcr = MPa
11.Centroid & second moment of areaMedium
1403014012xdimensions in mm

Find the second moment of area Ix of the T-section about the horizontal axis x through its centroid.

bf = 140 mmtf = 30 mmtw = 12 mmhw = 140 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
2402016014xM = 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 size of the bending stress σtop at the top edge.

bf = 240 mmtf = 20 mmtw = 14 mmhw = 160 mmM = 30 kN·m
σtop = MPa
13.Effective stress in soilMedium
sandγd​ = 17 kN/m³γsat​ = 19 kN/m³12 mwater tableXz = 10 m

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

z = 10 mzw = 3 mγw = 9.81 kN/m³sand: γd = 17 kN/m³sand: γsat = 19 kN/m³
u = kPa
14.Effective stress in soilHard
sandγd​ = 15 kN/m³γsat​ = 19 kN/m³5 mclayγsat​ = 19 kN/m³5 mwater tableXz = 7.5 m

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

z = 7.5 mzw = 1 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 19 kN/m³clay: γsat = 19 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 200 kPasandclayCc​ = 0.25, Cr​ = 0.04e0​ = 0.95σ′0​ = 75 kPaOCR = 1.54 mwater table

A 4 m thick overconsolidated clay layer has Cc = 0.25, Cr = 0.04 and e₀ = 0.95. At its mid-depth the effective vertical stress is 75 kPa and the overconsolidation ratio is OCR = 1.5. A new building adds 200 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 4 mCc = 0.25Cr = 0.04e0 = 0.95σ′0 = 75 kPaOCR = 1.5Δσ = 200 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 8 m8 msandwater table

In a laboratory oedometer test, a clay specimen 19 mm thick, drained at the top and bottom, reaches 50% consolidation in 12 min. In the field the same clay forms a layer 8 m thick. It lies between two sand layers, so water drains out at the top and the bottom. How many days t does the field layer take to reach 50% consolidation?

hlab = 19 mmtlab = 12 minH = 8 mfield: double drainage
t = days
17.Hydrostatic forceMedium
gated = 1.5 mH = 1 m

A vertical rectangular gate 1 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 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 4 mH = 1.5 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of oil, with its top edge 4 m below the surface. Find the depth ycp of the centre of pressure below the surface.

d = 4 mH = 1.5 mb = 2 mρ = 880 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
Q = 20 L/sD = 200 mmL = 500 mf = 0.03

Water flows at 20 L/s through a pipe 500 m long with an inside diameter of 200 mm. Use the Darcy friction factor f = 0.03 and g = 9.81 m/s². Find the friction head loss hf.

Q = 20 L/sL = 500 mD = 200 mmf = 0.03g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 5free outletH = ?L = 200 m, D = 150 mm, f = 0.0222× bend (K = 0.3)

A pipe 200 m long with an inside diameter of 150 mm (Darcy friction factor f = 0.022) runs from an open reservoir and discharges as a free jet into the air. The minor losses are a square-edged entrance (K = 0.5), 2 bends (K = 0.3 each) and a valve (K = 5). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 40 L/s?

Q = 40 L/sL = 200 mD = 150 mmf = 0.022Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 5
H = m
21.Open-channel flow (Manning)Medium
D = 300 mmn = 0.013, S = 0.004

A concrete storm sewer with an inside diameter of 300 mm flows just full (as an open channel, not under pressure). Manning n = 0.013 and the slope is S = 0.004. Find the flow rate Q in m³/s.

D = 300 mmn = 0.013S = 0.004
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 3.5 my = 2.2 m2 : 1n = 0.03, Q = 49 m³/s

A trapezoidal grass-lined earth channel with a bottom width of 3.5 m and side slopes of 2:1 (horizontal:vertical) must carry 49 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 = 49 m³/sb = 3.5 my = 2.2 mz = 2n = 0.03
S = m/m
23.Pumps & pump powerMedium
PQ = 10 L/sH = 22 m

In a test, a pump delivers 10 L/s of water (ρ = 1000 kg/m³) against a head of 22 m while its shaft takes 3.3 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.

Q = 10 L/sH = 22 mPshaft = 3.3 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
PQ = 100 L/sΔz = 13 mL = 600 m, D = 250 mm, f = 0.02, ΣK = 6

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 13 m higher. The pipe is 600 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.02; the minor-loss coefficients add up to ΣK = 6 (entrance and exit included). Use g = 9.81 m/s². Find the head H the pump must add.

Q = 100 L/sΔz = 13 mL = 600 mD = 250 mmf = 0.02ΣK = 6
H = m
25.Time value of moneyMedium
years012345PV = ?€15 000

You need €15 000 in 5 years. An account pays 3.6% per year, compounded monthly. How much must you deposit today? Find the present value PV.

FV = €15 0003.6% / 12n = 5
PV = €
26.Time value of moneyHard
months0123…348€100€100€100FV = ?

You save €100 at the end of every month for 29 years. The account pays 7.2% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €1007.2% / 12N = 348
FV = €
27.NPV & IRRMedium
years0123456€60 000€2 000€2 000€2 000€2 000€2 000€2 000r = 8%, EAC = ?

A machine costs €60 000 today, lasts 6 years and costs €2 000 per year to run (paid at the end of each year). The cost of capital is 8%. Find its equivalent annual cost EAC.

C0 = €60 000M = €2 000n = 6r = 8%
EAC = €
28.NPV & IRRHard
r (%)NPVABr* = ?0

Project A costs €20 000 and returns €10 500, €8 000, €5 000 at the end of years 1 to 3. Project B costs €22 000 and returns €5 500, €9 000, €12 000. Find the crossover rate r* at which both projects have the same NPV, in percent.

A: −20 000, 10 500, 8 000, 5 000B: −22 000, 5 500, 9 000, 12 000
r* = %
29.Normal distributionMedium
49.567.5P = ?

The exam scores are normally distributed with mean 65 points and standard deviation 10 points. What fraction lies between 49.5 and 67.5 points? Give P as a decimal.

μ = 65σ = 10x1 = 49.5x2 = 67.5
P =
30.Normal distributionHard
35455565758595pointstop 95%

The exam scores are normally distributed with mean 65 points and standard deviation 10 points. Drag the cut-off so the shaded top 95% is to the right of it. Find the cut-off x.

μ = 65 pointsσ = 10 points95%
x = points

3Solutions

1.Beam support reactions

Answer: MA = 360 kN·m

Cantilever equilibrium: a fixed support can push up and also resist rotation, so it gives a vertical reaction RA and a reaction moment MA. ΣFy = 0 gives RA, and moments about the wall give MA = Σ(load × distance from the wall). A distributed load acts as its resultant at the centroid of the load diagram.

Resultant of the distributed load

W = 5·6 = 30 kN, x̄ = 3 m

Moment about the wall

MA = P·a + W·x̄ = 45·6 + 30·3 = 360 kN·m

Answer

MA = 360 kN·m
2.Beam support reactions

Answer: MA = 146.3 kN·m

Cantilever equilibrium: a fixed support can push up and also resist rotation, so it gives a vertical reaction RA and a reaction moment MA. ΣFy = 0 gives RA, and moments about the wall give MA = Σ(load × distance from the wall). A distributed load acts as its resultant at the centroid of the load diagram.

Resultant of the triangular load

W = ½·4·4 = 8 kN
x̄ = 2L/3 = 2.667 m

Moment about the wall

MA = W·x̄ + P·a = 8·2.667 + 50·2.5 = 146.3 kN·m

Answer

MA = 146.3 kN·m
3.Truss: method of joints

Answer: member CG

Zero-force members: at a joint, the forces must balance in every direction. If a joint has no load and no support, and two of its three members are in line, then the balance across that line involves only the third member, so its force is zero. If only two members meet at an unloaded joint and they are not in line, both are zero.

Joint C

BC and CD lie on one straight line and the joint carries no load. Balancing forces across that line leaves only CG.

ΣF⊥ = 0 → FCG = 0

Check with the method of joints

Solving all joints gives these member forces (T = tension, C = compression).

AB: 5 kN (T), BC: 10 kN (T), CD: 10 kN (T), DE: 5 kN (T), FG: 5 kN (C), GH: 5 kN (C), AF: 7.071 kN (C), HE: 7.071 kN (C), BF: 5 kN (T), CG: 0, DH: 5 kN (T), BG: 7.071 kN (C), DG: 7.071 kN (C)

Answer

Zero-force member: CG
4.Truss: method of joints

Answer: member BF

Zero-force members: at a joint, the forces must balance in every direction. If a joint has no load and no support, and two of its three members are in line, then the balance across that line involves only the third member, so its force is zero. If only two members meet at an unloaded joint and they are not in line, both are zero.

Joint B

AB and BC lie on one straight line and the joint carries no load. Balancing forces across that line leaves only BF.

ΣF⊥ = 0 → FBF = 0

Check with the method of joints

Solving all joints gives these member forces (T = tension, C = compression).

AB: 59.06 kN (T), BC: 59.06 kN (T), CD: 52.19 kN (T), DE: 52.19 kN (T), FG: 66.88 kN (C), GH: 66.88 kN (C), AF: 31.77 kN (C), HE: 86.98 kN (C), BF: 0, CG: 30 kN (C), DH: 15 kN (T), FC: 13.02 kN (T), HC: 24.48 kN (T)

Answer

Zero-force member: BF
5.Shear force & bending moment

Answer: Mx = 18.75 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 = 10·4 = 40 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 10·4·2
RB = 80/4 = 20 kN
ΣFy = 0: RA = 40 − 20 = 20 kN
w = 10 kN/mABRA​ = 20RB​ = 20section1.5 m2.5 m

Cut at x = 1.5 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 = 20·1.5 − 10·1.5·0.75 = 18.75 kN·m

Answer

Mx = 18.75 kN·m
6.Shear force & bending moment

Answer: Mx = 143.5 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 = 8·10 = 80 kN, acting at x̄ = 5 m
ΣMA = 0: RB·10 = 50·7 + 8·10·5
RB = 750/10 = 75 kN
ΣFy = 0: RA = 130 − 75 = 55 kN
w = 8 kN/mP = 50 kNABRA​ = 55RB​ = 75section3.5 m3.5 m3 m

Cut at x = 3.5 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 = 55·3.5 − 8·3.5·1.75 = 143.5 kN·m

Answer

Mx = 143.5 kN·m
7.Beam deflection

Answer: δmax = 2.084 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 = 8 N/mm, L = 1500 mm
EI = 2.53 × 10¹¹ N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·8·1500⁴/(384·2.53 × 10¹¹) = 2.084 mm

Answer

δmax = 2.084 mm
8.Beam deflection

Answer: δmax = 5.965 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 = 21000 N, w = 12 N/mm, L = 4000 mm, EI = 1.14 × 10¹³ N·mm²

Each load on its own

δP = PL³/(48EI) = 21000·4000³/(48·1.14 × 10¹³) = 2.456 mm
δw = 5wL⁴/(384EI) = 5·12·4000⁴/(384·1.14 × 10¹³) = 3.509 mm

Add them

δmax = 2.456 + 3.509 = 5.965 mm

Answer

δmax = 5.965 mm
9.Column buckling

Answer: Pcr = 62.01 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 = 2·4000 = 8000 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·2.011 × 10⁶/8000² = 62013 N = 62.01 kN

Answer

Pcr = 62.01 kN
10.Column buckling

Answer: σcr = 7.896 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·40⁴/64 = 125664 mm⁴

Radius of gyration and slenderness

A = 1257 mm²
r = √(I/A) = √(125664/1257) = 10 mm
KL = 2·2500 = 5000 mm
KL/r = 5000/10 = 500

Critical stress

σcr = π²E/(KL/r)² = π²·200000/500² = 7.896 MPa

Answer

σcr = 7.896 MPa
11.Centroid & second moment of area

Answer: Ix = 11.73 × 10⁶ mm⁴

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 = 140·30 = 4200 mm², yf = 140 + 30/2 = 155 mm
web: Aw = 12·140 = 1680 mm², yw = 140/2 = 70 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (4200·155 + 1680·70)/5880 = 130.7 mm

Parallel-axis theorem

flange: 140·30³/12 + 4200·(155 − 130.7)² = 2.792 × 10⁶ mm⁴
web: 12·140³/12 + 1680·(70 − 130.7)² = 8.937 × 10⁶ mm⁴
Ix = 2.792 × 10⁶ + 8.937 × 10⁶ = 1.173 × 10⁷ mm⁴ = 11.73 × 10⁶ mm⁴

Answer

Ix = 11.73 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 66.96 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 = 240·20 = 4800 mm², yf = 160 + 20/2 = 170 mm
web: Aw = 14·160 = 2240 mm², yw = 160/2 = 80 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (4800·170 + 2240·80)/7040 = 141.4 mm

Parallel-axis theorem

flange: 240·20³/12 + 4800·(170 − 141.4)² = 4.096 × 10⁶ mm⁴
web: 14·160³/12 + 2240·(80 − 141.4)² = 1.321 × 10⁷ mm⁴
Ix = 4.096 × 10⁶ + 1.321 × 10⁷ = 1.731 × 10⁷ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 180 − 141.4 = 38.64 mm
σ = M·y/I = 3 × 10⁷·38.64/1.731 × 10⁷ = 66.96 MPa

Answer

σtop = 66.96 MPa
13.Effective stress in soil

Answer: u = 68.67 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) = 9.81·7 = 68.67 kPa

Answer

u = 68.67 kPa
14.Effective stress in soil

Answer: σ′ = 74.73 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·1 + γsat,sand·4 + γsat,clay·2.5
σ = 15·1 + 19·4 + 19·2.5 = 138.5 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·6.5 = 63.77 kPa

Effective stress

σ′ = σ − u = 138.5 − 63.77 = 74.73 kPa

Answer

σ′ = 74.73 kPa
15.Consolidation settlement

Answer: S = 213.5 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.

Preconsolidation pressure

σ′p = OCR·σ′0 = 1.5·75 = 112.5 kPa

Compare with the preconsolidation pressure

σ′f = 75 + 200 = 275 kPa > 112.5 kPa

Settlement

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

S = 0.04·4/(1 + 0.95)·log₁₀(112.5/75) + 0.25·4/(1 + 0.95)·log₁₀(275/112.5)
S = 14.45 + 199.1 = 213.5 mm

Answer

S = 213.5 mm
16.Consolidation settlement

Answer: t = 1477 days

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 paths

Hdr,lab = 19/2 = 9.5 mm = 0.0095 m
Hdr,field = 8/2 = 4 m

Scale the time

t = Tv·Hdr²/cv with the same T_v and cv in the lab and the field.

tfield = 12·(4/0.0095)² = 2.127 × 10⁶ min
tfield = 2.127 × 10⁶/1440 = 1477 days

Answer

t = 1477 days
17.Hydrostatic force

Answer: F = 19.62 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 + 1/2 = 2 m
A = H·b = 1·1 = 1 m²
gated = 1.5 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2·1 = 19.62 kN

Answer

F = 19.62 kN
18.Hydrostatic force

Answer: ycp = 4.789 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 = 4 + 1.5/2 = 4.75 m
A = H·b = 1.5·2 = 3 m²
gated = 4 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 880·9.81·4.75·3 = 123 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) = 4.75 + 0.5625/(4.75·3) = 4.789 m

Answer

ycp = 4.789 m
19.Pipe friction & head loss

Answer: hf = 1.549 m

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.

Mean velocity

A = π·0.2²/4 = 0.03142 m²
V = Q/A = 0.02/0.03142 = 0.6366 m/s

Velocity head

V²/(2g) = 0.6366²/(2·9.81) = 0.02066 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.03·(500/0.2)·0.6366²/(2·9.81) = 1.549 m

Answer

hf = 1.549 m
20.Pipe friction & head loss

Answer: H = 9.514 m

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.

Velocity

V = Q/A = 0.04/0.01767 = 2.264 m/s
V²/(2g) = 0.2611 m

Loss coefficients

f·L/D = 0.022·200/0.15 = 29.33
ΣK = 0.5 + 2·0.3 + 5 = 6.1

Energy equation

The outlet jet still carries its velocity head; it is not a loss but it has to be supplied.

H = (1 + 29.33 + 6.1)·0.2611 = 9.514 m

Answer

H = 9.514 m
21.Open-channel flow (Manning)

Answer: Q = 0.06116 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 = 0.07069 m², R = D/4 = 0.075 m

Velocity

V = (1/0.013)·0.0752/3·0.0041/2 = 0.8652 m/s

Flow rate

Q = A·V = 0.07069·0.8652 = 0.06116 m³/s

Answer

Q = 0.06116 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.005027 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 + z·y)·y = (3.5 + 2·2.2)·2.2 = 17.38 m²
P = b + 2y·√(1 + z²) = 3.5 + 2·2.2·√(1 + 2²) = 13.34 m
R = A/P = 1.303 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.03·49/(17.38·1.193) = 0.0709
S = 0.0709² = 0.005027

Answer

S = 0.005027

That is a fall of 5.027 m per kilometre.

23.Pumps & pump power

Answer: η = 65.4 %

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 = 1000·9.81·0.01·22 = 2.158 kW

Efficiency

η = Ph/Pshaft = 2.158/3.3 = 65.4%

Answer

η = 65.4%
24.Pumps & pump power

Answer: H = 24.42 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) = (48 + 6)·0.2115 = 11.42 m

Pump head

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

H = Δz + hL = 13 + 11.42 = 24.42 m

Answer

H = 24.42 m
25.Time value of money

Answer: PV = 12532 €

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 = 0.036000000000000004/12 = 0.003
N = 12·5 = 60

Present value

PV = FV/(1 + i)N = 15 000/1.197 = €12 532.43

Answer

PV = €12 532.43
26.Time value of money

Answer: FV = 116976 €

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 = 0.07200000000000001/12 = 0.006
N = 12·29 = 348

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 100·(8.019 − 1)/0.006 = €116 976.28

Answer

FV = €116 976.28

You paid in €34 800 yourself; the rest is interest.

27.NPV & IRR

Answer: EAC = 14979 €

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 − 1.08−6)/0.08 = 4.623

Annualised purchase price

60 000/4.623 = 12 978.92

EAC

EAC = 12 978.92 + 2 000 = €14 978.92

Answer

EAC = €14 978.92
28.NPV & IRR

Answer: r* = 6.366 %

Crossover rate: the discount rate at which two projects have the same NPV. It is the IRR of the difference in their cash flows (B − A). Below it the project with the later, larger cash flows has the higher NPV; above it the other one wins.

Difference in cash flows

ΔCF0 = −22 000 − (−20 000) = −2 000
ΔCF1 = 5 500 − 10 500 = −5 000
ΔCF2 = 9 000 − 8 000 = 1 000
ΔCF3 = 12 000 − 5 000 = 7 000

IRR of the difference

NPVΔ(6%) = 50.35
NPVΔ(7%) = −85.37
r* = 6.366%

Answer

r* = 6.366%

Check: at 6.366% both NPVs are €1 097.53.

29.Normal distribution

Answer: P = 0.5381

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 = (49.5 − 65)/10 = −1.55
z₂ = (67.5 − 65)/10 = 0.25

Area between

P = Φ(0.25) − Φ(−1.55) = 0.5987 − 0.06057 = 0.5381

Answer

P = 0.5381
30.Normal distribution

Answer: x = 48.6 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) = 0.05

z from the table

z ≈ −1.64

Back to the original units

x = 65 − 1.64·10 = 48.6 points

Answer

x = 48.6 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