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​ = 25 kNP2​ = 80 kNABCRB​ = ?1.5 m2.5 m2 m

The beam has a pin at A and a roller at B, 4 m from A, and overhangs B to the free end C. Find the vertical reaction RB, taking upward as positive.

AB = 4 mAC = 6 mP1 = 25 kN at 1.5 mP2 = 80 kN at 6 m
RB = kN
2.Beam support reactionsHard
w = 12 kN/mP = 40 kNABRA​RB​ = ?7 m1 m2 m

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

L = 10 mP = 40 kN at 8 mw = 12 kN/m from 7 to 8 m
RB = kN
3.Truss: method of jointsMedium
ABBCACACB40 kN6 m4 m4 m

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

span = 6 mheight = 4 mB is 4 m from Avertical load = 40 kN
FAC = kN
4.Truss: method of jointsHard
ABCDEFGH20 kN35 kN15 kN35 kN35 kN4 × 3 m3 m

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

B: 20 kN ↓D: 35 kN ↓F: 15 kN ↓H: 35 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 BG
  13. 13member DG
5.Shear force & bending momentMedium
w = 2 kN/mABsection3 m1 m

Find the shear force Vx at the section x = 3 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 4 mw = 2 kN/m from 0 to 4 mx = 3 m
Vx = kN
6.Shear force & bending momentHard
w = 20 kN/mAB2 m4 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 = 6 mw = 20 kN/m from 2 to 6 m
Mmax = kN·m
7.Beam deflectionMedium
w = 15 kN/mδL = 4 m

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

w = 15 kN/mL = 4 mE = 200 GPa (steel)I = 36 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 10 kN/mP = 26 kNδL = 3 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 = 26 kNw = 10 kN/mL = 3 mE = 200 GPa (steel)I = 84 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 5 m40 × 80 mmcross-section

A column of length L made of steel is pinned at both ends. Using Euler’s formula, find its critical buckling load Pcr.

L = 5 mE = 200 GPa (steel)b × h = 40 × 80 mm
Pcr = kN
10.Column bucklingHard
P = 20 kNL = 1.5 md = ?cross-section

A solid round column of length L made of steel is fixed at the base and pinned at the top. It must carry 20 kN with a factor of safety of 2.5 against buckling. Find the smallest diameter d.

P = 20 kNn = 2.5L = 1.5 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
1402030014xdimensions in mm

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

bf = 140 mmtf = 20 mmtw = 14 mmhw = 300 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
1202510010xM = 5 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 5 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 120 mmtf = 25 mmtw = 10 mmhw = 100 mmM = 5 kN·m
σtop = MPa
13.Effective stress in soilMedium
sandγd​ = 16.5 kN/m³γsat​ = 19 kN/m³6 mwater tableXz = 6 m

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

z = 6 mzw = 4 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 19 kN/m³
u = kPa
14.Effective stress in soilHard
sandγd​ = 15 kN/m³γsat​ = 20 kN/m³6 mclayγsat​ = 19 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 = 20 kN/m³clay: γsat = 19 kN/m³
σ = kPa
15.Consolidation settlementMedium
Δσ = 20 kPasandclayCc​ = 0.5, Cr​ = 0.04e0​ = 0.85σ′0​ = 95 kPaOCR = 1.52.5 mwater table

A 2.5 m thick overconsolidated clay layer has Cc = 0.5, Cr = 0.04 and e₀ = 0.85. At its mid-depth the effective vertical stress is 95 kPa and the overconsolidation ratio is OCR = 1.5. A new building adds 20 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 2.5 mCc = 0.5Cr = 0.04e0 = 0.85σ′0 = 95 kPaOCR = 1.5Δσ = 20 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 4.5 mcv​ = 1.5 m²/year4.5 mimpervious rockwater table

A clay layer 4.5 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 80% average consolidation the time factor is Tv = 0.567. How many years t does the layer take to reach 80% consolidation?

H = 4.5 mcv = 1.5 m²/yearU = 80%Tv = 0.567single drainage
t = years
17.Hydrostatic forceMedium
gated = 2 mH = 1 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of water, with its top edge 2 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 2 mH = 1 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 0.5 mH = 1 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of seawater, with its top edge 0.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 0.5 mH = 1 mb = 2 mρ = 1025 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
V = 1 m/sD = 150 mmL = 400 mf = 0.025

Water flows at a mean velocity of 1 m/s through a pipe 400 m long with an inside diameter of 150 mm. Use the Darcy friction factor f = 0.025 and g = 9.81 m/s². Find the friction head loss hf.

V = 1 m/sL = 400 mD = 150 mmf = 0.025g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 10free outletH = ?L = 300 m, D = 250 mm, f = 0.0253× bend (K = 0.3)

A pipe 300 m long with an inside diameter of 250 mm (Darcy friction factor f = 0.025) 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), 3 bends (K = 0.3 each) and a valve (K = 10). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 50 L/s?

Q = 50 L/sL = 300 mD = 250 mmf = 0.025Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 10
H = m
21.Open-channel flow (Manning)Medium
b = 3.5 my = 2.5 m1.5 : 1n = 0.015, S = 0.003

A trapezoidal brickwork channel has a bottom width of 3.5 m and side slopes of 1.5:1 (horizontal:vertical). Water flows uniformly 2.5 m deep. Manning n = 0.015 and the bed slope is S = 0.003. Find the flow rate Q in m³/s.

b = 3.5 my = 2.5 mz = 1.5n = 0.015S = 0.003
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 3.5 my = 0.8 m2 : 1n = 0.03, Q = 3.6 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 3.6 m³/s in uniform flow at a depth of 0.8 m. Manning n = 0.03. Find the required bed slope S (in m/m).

Q = 3.6 m³/sb = 3.5 my = 0.8 mz = 2n = 0.03
S = m/m
23.Pumps & pump powerMedium
PQ = 80 L/sH = 46 m

A pump with an efficiency of 80% delivers 80 L/s of water (ρ = 1000 kg/m³) against a head of 46 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 80 L/sH = 46 mη = 80%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 75 L/sΔz = 34 mL = 100 m, D = 200 mm, f = 0.022, ΣK = 8

A pump moves 75 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 34 m higher. The pipe is 100 m long with an inside diameter of 200 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. The pump efficiency is 65%. Find the shaft power Pshaft in kW.

Q = 75 L/sΔz = 34 mL = 100 mD = 200 mmf = 0.022ΣK = 8η = 65%
Pshaft = kW
25.Time value of moneyMedium
years0123…10€5 000FV = ?

You invest €5 000 at a nominal rate of 6% per year, compounded monthly. Find the value FV of the investment after 10 years.

PV = €5 0006% / 12n = 10
FV = €
26.Time value of moneyHard
months0123…360€300€300€300FV = ?

You save €300 at the end of every month for 30 years. The account pays 2.4% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €3002.4% / 12N = 360
FV = €
27.NPV & IRRMedium
years0123−30 00013 0009 0009 000

An investment of €30 000 gives these cash flows at the end of years 1 to 3: €13 000, €9 000, €9 000. The cost of capital is 7.000000000000001%. Find the net present value NPV.

r = 7.000000000000001%CF0 = −30 000CF1 = 13 000CF2 = 9 000CF3 = 9 000
NPV = €
28.NPV & IRRHard
years012345−100 00018 000+3%+3%+3%+3%r = 10%, NPV = ?

A project costs €100 000 today. Its cash flow is €18 000 at the end of year 1 and grows by 3% per year until the last cash flow at the end of year 5. The cost of capital is 10%. Find the net present value NPV.

C0 = €100 000CF1 = €18 000g = 3%n = 5r = 10%
NPV = €
29.Normal distributionMedium
176.25179.4P = ?

The heights of adult men are normally distributed with mean 178 cm and standard deviation 7 cm. What fraction lies between 176.25 and 179.4 cm? Give P as a decimal.

μ = 178σ = 7x1 = 176.25x2 = 179.4
P =
30.Normal distributionHard
μ = 32x = ?80%

The delivery times are normally distributed with mean 32 min and standard deviation 6 min. Find the value x below which 80% of them lie (the 80th percentile).

μ = 32σ = 6P = 80%
x = min

3Solutions

1.Beam support reactions

Answer: RB = 129.4 kN

Static equilibrium: a body at rest has ΣFx = 0, ΣFy = 0 and ΣM = 0 about any point. Replace each distributed load by its resultant (its area) acting at the centroid of the load diagram, and take moments about a support to remove that support’s reaction from the equation.

Moments about A

Counter-clockwise positive.

ΣMA = 0: RB·4 = 25·1.5 + 80·6
RB = 517.5/4 = 129.4 kN

Vertical equilibrium

RA = 25 + 80 − 129.4 = −24.38 kN

Answer

RB = 129.4 kN

RA is negative: the pin at A has to hold the beam down.

2.Beam support reactions

Answer: RB = 41 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 = 12 kN/mP = 40 kNABRA​RB​7 m1 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 = 12·1 = 12 kN, acting at x̄ = 7.5 m
ΣMA = 0: RB·10 = 40·8 + 12·1·7.5
RB = 410/10 = 41 kN
ΣFy = 0: RA = 52 − 41 = 11 kN

Answer

RB = 41 kN
3.Truss: method of joints

Answer: FAC = 13.33 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 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·6 = 40·4 → Cy = 26.67 kN
ΣFy = 0: Ay = 40 − 26.67 = 13.33 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 = 4/4.472 = 0.8944, cos γ = 2/4.472 = 0.4472
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −26.67/0.8944 = −29.81 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−29.81)·0.4472 = 13.33 kN

Answer

FAC = 13.33 kN (tension)
4.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: 17.5 kN (T), BC: 35 kN (T), CD: 35 kN (T), DE: 52.5 kN (T), FG: 52.5 kN (C), GH: 87.5 kN (C), AF: 74.25 kN (C), HE: 74.25 kN (C), BF: 37.5 kN (T), CG: 0, DH: 17.5 kN (T), BG: 24.75 kN (C), DG: 24.75 kN (T)

Answer

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

Answer: Vx = −2 kN

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 = 2·4 = 8 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 2·4·2
RB = 16/4 = 4 kN
ΣFy = 0: RA = 8 − 4 = 4 kN
w = 2 kN/mABRA​ = 4RB​ = 4section3 m1 m

Cut at x = 3 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.

V = RA − (all downward loads left of the cut)
Vx = 4 − 2·3 = −2 kN

Answer

Vx = −2 kN
6.Shear force & bending moment

Answer: Mmax = 71.11 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 = 20·4 = 80 kN, acting at x̄ = 4 m
ΣMA = 0: RB·6 = 20·4·4
RB = 320/6 = 53.33 kN
ΣFy = 0: RA = 80 − 53.33 = 26.67 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 + 26.67/20 = 3.333 m

Maximum moment

Mmax = RA·x0 − w·(x0 − 2)²/2 = 26.67·3.333 − 20·1.333²/2 = 71.11 kN·m

Answer

Mmax = 71.11 kN·m
7.Beam deflection

Answer: δmax = 6.944 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 = 15 N/mm, L = 4000 mm
EI = 7.2 × 10¹² N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·15·4000⁴/(384·7.2 × 10¹²) = 6.944 mm

Answer

δmax = 6.944 mm
8.Beam deflection

Answer: δmax = 1.498 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 = 26000 N, w = 10 N/mm, L = 3000 mm, EI = 1.68 × 10¹³ N·mm²

Each load on its own

δP = PL³/(48EI) = 26000·3000³/(48·1.68 × 10¹³) = 0.8705 mm
δw = 5wL⁴/(384EI) = 5·10·3000⁴/(384·1.68 × 10¹³) = 0.6278 mm

Add them

δmax = 0.8705 + 0.6278 = 1.498 mm

Answer

δmax = 1.498 mm
9.Column buckling

Answer: Pcr = 33.69 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 rectangle buckles about its weak axis, using the smaller dimension cubed.

Imin = h·b³/12 = 80·40³/12 = 426667 mm⁴

Effective length

KL = 1·5000 = 5000 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·426667/5000² = 33688 N = 33.69 kN

Answer

Pcr = 33.69 kN
10.Column buckling

Answer: d = 27.46 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 = 2.5·20000 = 50000 N
KL = 0.7·1500 = 1050 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·50000·1050²/(π³·200000))^(1/4) = 27.46 mm

Answer

d = 27.46 mm

Check: the slenderness KL/r is 152.9, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: Ix = 74.6 × 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 = 140·20 = 2800 mm², yf = 300 + 20/2 = 310 mm
web: Aw = 14·300 = 4200 mm², yw = 300/2 = 150 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2800·310 + 4200·150)/7000 = 214 mm

Parallel-axis theorem

flange: 140·20³/12 + 2800·(310 − 214)² = 2.59 × 10⁷ mm⁴
web: 14·300³/12 + 4200·(150 − 214)² = 4.87 × 10⁷ mm⁴
Ix = 2.59 × 10⁷ + 4.87 × 10⁷ = 7.46 × 10⁷ mm⁴ = 74.6 × 10⁶ mm⁴

Answer

Ix = 74.6 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 35.88 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 = 120·25 = 3000 mm², yf = 100 + 25/2 = 112.5 mm
web: Aw = 10·100 = 1000 mm², yw = 100/2 = 50 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (3000·112.5 + 1000·50)/4000 = 96.88 mm

Parallel-axis theorem

flange: 120·25³/12 + 3000·(112.5 − 96.88)² = 888672 mm⁴
web: 10·100³/12 + 1000·(50 − 96.88)² = 3.031 × 10⁶ mm⁴
Ix = 888672 + 3.031 × 10⁶ = 3.919 × 10⁶ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 125 − 96.88 = 28.13 mm
σ = M·y/I = 5 × 10⁶·28.13/3.919 × 10⁶ = 35.88 MPa

Answer

σtop = 35.88 MPa
13.Effective stress in soil

Answer: u = 19.62 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) = 9.81·2 = 19.62 kPa

Answer

u = 19.62 kPa
14.Effective stress in soil

Answer: σ = 166.5 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 + 20·2 + 19·3.5 = 166.5 kPa

Answer

σ = 166.5 kPa
15.Consolidation settlement

Answer: S = 4.485 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 = 1.5·95 = 142.5 kPa

Compare with the preconsolidation pressure

σ′f = 95 + 20 = 115 kPa ≤ 142.5 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.04·2.5/(1 + 0.85)·log₁₀(115/95) = 4.485 mm

Answer

S = 4.485 mm
16.Consolidation settlement

Answer: t = 7.654 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 = 4.5 m

Time

t = Tv·Hdr²/cv = 0.567·4.5²/1.5 = 7.654 years

Answer

t = 7.654 years
17.Hydrostatic force

Answer: F = 73.58 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 = 2 + 1/2 = 2.5 m
A = H·b = 1·3 = 3 m²
gated = 2 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2.5·3 = 73.58 kN

Answer

F = 73.58 kN
18.Hydrostatic force

Answer: F = 20.11 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 = 0.5 + 1/2 = 1 m
A = H·b = 1·2 = 2 m²
gated = 0.5 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 1025·9.81·1·2 = 20.11 kN

Answer

F = 20.11 kN
19.Pipe friction & head loss

Answer: hf = 3.398 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 head

V²/(2g) = 1²/(2·9.81) = 0.05097 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.025·(400/0.15)·1²/(2·9.81) = 3.398 m

Answer

hf = 3.398 m
20.Pipe friction & head loss

Answer: H = 2.242 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 = 0.05/0.04909 = 1.019 m/s
V²/(2g) = 0.05288 m

Loss coefficients

f·L/D = 0.025·300/0.25 = 30
ΣK = 0.5 + 3·0.3 + 10 = 11.4

Energy equation

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

H = (1 + 30 + 11.4)·0.05288 = 2.242 m

Answer

H = 2.242 m
21.Open-channel flow (Manning)

Answer: Q = 84.72 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 + 1.5·2.5)·2.5 = 18.13 m²
P = b + 2y·√(1 + z²) = 3.5 + 2·2.5·√(1 + 1.5²) = 12.51 m
R = A/P = 1.448 m

Velocity

V = (1/0.015)·1.4482/3·0.0031/2 = 4.674 m/s

Flow rate

Q = A·V = 18.13·4.674 = 84.72 m³/s

Answer

Q = 84.72 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.001461 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 + 2·0.8)·0.8 = 4.08 m²
P = b + 2y·√(1 + z²) = 3.5 + 2·0.8·√(1 + 2²) = 7.078 m
R = A/P = 0.5765 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.03·3.6/(4.08·0.6926) = 0.03822
S = 0.03822² = 0.001461

Answer

S = 0.001461

That is a fall of 1.461 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 45.13 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 = 1000·9.81·0.08·46 = 36.1 kW

Shaft power

Pshaft = Ph/η = 36.1/0.8 = 45.13 kW

Answer

Pshaft = 45.13 kW
24.Pumps & pump power

Answer: Pshaft = 44.73 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.

Velocity

V = Q/A = 0.075/0.03142 = 2.387 m/s
V²/(2g) = 0.2905 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (11 + 8)·0.2905 = 5.519 m

Pump head

H = Δz + hL = 34 + 5.519 = 39.52 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.075·39.52/0.65 = 44.73 kW

Answer

Pshaft = 44.73 kW
25.Time value of money

Answer: FV = 9097 €

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 = r/m = 0.06/12 = 0.005
N = m·n = 12·10 = 120

Future value

FV = 5 000·(1 + 0.005)120 = 5 000·1.819 = €9 096.98

Answer

FV = €9 096.98
26.Time value of money

Answer: FV = 157943 €

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 = 0.024/12 = 0.002
N = 12·30 = 360

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 300·(2.053 − 1)/0.002 = €157 943.48

Answer

FV = €157 943.48

You paid in €108 000 yourself; the rest is interest.

27.NPV & IRR

Answer: NPV = −2643 €

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 = −30 000
CF1/(1 + 0.07)1 = 13 000/1.07 = 12 149.53
CF2/(1 + 0.07)2 = 9 000/1.145 = 7 860.95
CF3/(1 + 0.07)3 = 9 000/1.225 = 7 346.68

Add them up

NPV = €−2 642.84

Answer

NPV = €−2 642.84

NPV is negative, so the project earns less than the required return.

28.NPV & IRR

Answer: NPV = −27953 €

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 the growing annuity

((1.03)/(1.1))5 = 0.7198
PV = 18 000/(0.1 − 0.03)·(1 − 0.7198) = 72 046.80

NPV

NPV = 72 046.80 − 100 000 = −€27 953.20

Answer

NPV = −€27 953.20

NPV is negative, so the project earns less than the required return.

29.Normal distribution

Answer: P = 0.178

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 = (176.25 − 178)/7 = −0.25
z₂ = (179.4 − 178)/7 = 0.2

Area between

P = Φ(0.2) − Φ(−0.25) = 0.5793 − 0.4013 = 0.178

Answer

P = 0.178
30.Normal distribution

Answer: x = 37.05 min

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 for the percentile

Φ(z) = 0.8 → z = 0.8416

Back to x

x = 32 + 0.8416·6 = 37.05 min

Answer

x = 37.05 min

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