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​ = 55 kNP2​ = 25 kNABRA​RB​ = ?3 m1 m2 m

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

L = 6 mP1 = 55 kN at 3 mP2 = 25 kN at 4 m
RB = kN
2.Beam support reactionsHard
w = 10 kN/mP = 25 kNABRA​RB​ = ?4 m1 m

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

L = 5 mP = 25 kN at 4 mw = 10 kN/m from 0 to 4 m
RB = kN
3.Truss: method of jointsMedium
ABCDEFGH30 kN40 kN25 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.

C: 30 kN ↓D: 40 kN ↓G: 25 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
4.Truss: method of jointsHard
ABCDEFGH10 kN30 kN10 kN40 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.

F: 10 kN ↓F: 30 kN →G: 10 kN ↓H: 40 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/mP = 50 kNAB5 m

The cantilever is fixed at A. It carries a uniformly distributed load w over its whole length and a point load P at 5 m from A. Find the bending moment MA at the fixed support A. Use sagging moments positive and upward shear on the left face positive.

L = 5 mP = 50 kN at 5 mw = 2 kN/m from 0 to 5 m
MA = kN·m
6.Shear force & bending momentHard
5 kN/m10 kN55 kN50 kNABCDEFG2 m2 m2 m2 m2 m2 m

The marks A to G split the beam into six equal parts. At which mark is the bending moment largest in size, sagging or hogging? Click it in the diagram.

10 kN @ 0 m55 kN @ 12 m50 kN @ 4 m5 kN/m, 2–8 m
  1. 1A (x = 0 m)
  2. 2B (x = 2 m)
  3. 3C (x = 4 m)
  4. 4D (x = 6 m)
  5. 5E (x = 8 m)
  6. 6F (x = 10 m)
  7. 7G (x = 12 m)
7.Beam deflectionMedium
w = 6 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 = 6 kN/mL = 1.5 mE = 11 GPa (timber)I = 8.5 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 6 kN/mδL = 8 m

A simply supported beam carries a uniformly distributed load w. Its deflection may not exceed span/360. Find the smallest second moment of area Ireq that meets this limit.

w = 6 kN/mL = 8 mE = 11 GPa (timber)
Ireq = × 10⁶ mm⁴
9.Column bucklingMedium
PL = 2 m40 × 50 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 = 2 mE = 200 GPa (steel)b × h = 40 × 50 mm
Pcr = kN
10.Column bucklingHard
PL = 4 md = 40 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 = 4 mE = 200 GPa (steel)d = 40 mm
σcr = MPa
11.Centroid & second moment of areaMedium
2201524016xdimensions in mm

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

bf = 220 mmtf = 15 mmtw = 16 mmhw = 240 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
180250162602216xdimensions in mm

A welded I-section has a top flange 180 × 16 mm, a web 260 mm high and 16 mm thick, and a bottom flange 250 × 22 mm (width × thickness). Find its second moment of area Ix about the horizontal axis x through its centroid.

top flange: 180 × 16 mmweb: 16 × 260 mmbottom flange: 250 × 22 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
sandγd​ = 15.5 kN/m³γsat​ = 19 kN/m³12 mwater tableXz = 12 m

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

z = 12 mzw = 4 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 19 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 15.5 kN/m³γsat​ = 18.5 kN/m³6 mclayγsat​ = 17 kN/m³8 mwater tableXz = 10 m

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

z = 10 mzw = 5 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 18.5 kN/m³clay: γsat = 17 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 140 kPasandclayCc​ = 0.5, Cr​ = 0.03e0​ = 0.9σ′0​ = 85 kPaOCR = 2.53.5 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 85 kPa and the overconsolidation ratio is OCR = 2.5. A new building adds 140 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 = 85 kPaOCR = 2.5Δσ = 140 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 2.5 mcv​ = 0.8 m²/year2.5 mimpervious rockwater table

A clay layer 2.5 m thick has a coefficient of consolidation cv = 0.8 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 90% average consolidation the time factor is Tv = 0.848. How many years t does the layer take to reach 90% consolidation?

H = 2.5 mcv = 0.8 m²/yearU = 90%Tv = 0.848single drainage
t = years
17.Hydrostatic forceMedium
gated = 1 mH = 2 m

A vertical rectangular gate 2 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 = 2 mb = 2 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 4 mH = 1.5 m

A vertical rectangular gate 1 m wide sits in the wall of a tank of glycerin, with its top edge 4 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 4 mH = 1.5 mb = 1 mρ = 1260 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
V = 1.6 m/sD = 300 mmL = 150 mf = 0.03

Water flows at a mean velocity of 1.6 m/s through a pipe 150 m long with an inside diameter of 300 mm. Use the Darcy friction factor f = 0.03 and g = 9.81 m/s². Find the friction head loss hf.

V = 1.6 m/sL = 150 mD = 300 mmf = 0.03g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 5free outletH = ?L = 400 m, D = 250 mm, f = 0.0153× bend (K = 0.3)

A pipe 400 m long with an inside diameter of 250 mm (Darcy friction factor f = 0.015) 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 = 5). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 120 L/s?

Q = 120 L/sL = 400 mD = 250 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 5
H = m
21.Open-channel flow (Manning)Medium
D = 750 mmn = 0.013, S = 0.0015

A concrete storm sewer with an inside diameter of 750 mm flows half full. Manning n = 0.013 and the slope is S = 0.0015. Find the flow rate Q in m³/s.

D = 750 mmn = 0.013S = 0.0015
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 1.5 my = 1.2 m3 : 1n = 0.022, Q = 4.8 m³/s

A trapezoidal clean earth channel with a bottom width of 1.5 m and side slopes of 3:1 (horizontal:vertical) must carry 4.8 m³/s in uniform flow at a depth of 1.2 m. Manning n = 0.022. Find the required bed slope S (in m/m).

Q = 4.8 m³/sb = 1.5 my = 1.2 mz = 3n = 0.022
S = m/m
23.Pumps & pump powerMedium
PQ = 50 L/sH = 72 m

In a test, a pump delivers 50 L/s of water (ρ = 1000 kg/m³) against a head of 72 m while its shaft takes 58.9 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.

Q = 50 L/sH = 72 mPshaft = 58.9 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
300 kPa (gauge)PQ = 40 L/sΔz = 10 mL = 150 m, D = 200 mm, f = 0.018, ΣK = 8

A pump moves 40 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 10 m higher. The pipe is 150 m long with an inside diameter of 200 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. The upper tank is closed and the air above its water is at a gauge pressure of 300 kPa. Find the head H the pump must add.

Q = 40 L/sΔz = 10 mL = 150 mD = 200 mmf = 0.018ΣK = 8ptank = 300 kPa
H = m
25.Time value of moneyMedium
years012345PV = ?€20 000

You need €20 000 in 5 years. An account pays 3.6% per year, compounded monthly. How much must you deposit today? Find the present value PV.

FV = €20 0003.6% / 12n = 5
PV = €
26.Time value of moneyHard
months0123…156A?AA€50 000

You want €50 000 in 13 years. You save the same amount at the end of every month in an account paying 2.4% per year, compounded monthly. Find the monthly deposit A.

FV = €50 0002.4% / 12N = 156
A = €
27.NPV & IRRMedium
years0123−30 0009 0009 00011 000

An investment of €30 000 gives these cash flows at the end of years 1 to 3: €9 000, €9 000, €11 000. The cost of capital is 12%. Find the net present value NPV.

r = 12%CF0 = −30 000CF1 = 9 000CF2 = 9 000CF3 = 11 000
NPV = €
28.NPV & IRRHard
years0123−10 0006 0004 5007 000

A project costs €10 000 and returns €6 000, €4 500, €7 000 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −10 000CF1 = 6 000CF2 = 4 500CF3 = 7 000
IRR = %
29.Normal distributionMedium
105 s113 sX + Y?

X is normal with mean 60 s and standard deviation 5 s; Y is independent and normal with mean 45 s and standard deviation 4 s. Find the probability P that X + Y is more than 113 s. Round z to two decimals.

μX = 60, σX = 5μY = 45, σY = 4X + Y > 113 s
P =
30.Normal distributionHard
μ = 65x = ?97.5%

The exam scores are normally distributed with mean 65 points and standard deviation 10 points. Find the value x below which 97.5% of them lie (the 97.5th percentile).

μ = 65σ = 10P = 97.5%
x = points

3Solutions

1.Beam support reactions

Answer: RB = 44.17 kN

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

P1​ = 55 kNP2​ = 25 kNABRA​RB​3 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.

ΣMA = 0: RB·6 = 55·3 + 25·4
RB = 265/6 = 44.17 kN
ΣFy = 0: RA = 80 − 44.17 = 35.83 kN

Answer

RB = 44.17 kN
2.Beam support reactions

Answer: RB = 36 kN

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

w = 10 kN/mP = 25 kNABRA​RB​4 m1 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 = 10·4 = 40 kN, acting at x̄ = 2 m
ΣMA = 0: RB·5 = 25·4 + 10·4·2
RB = 180/5 = 36 kN
ΣFy = 0: RA = 65 − 36 = 29 kN

Answer

RB = 36 kN
3.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: 37.5 kN (T), BC: 37.5 kN (T), CD: 57.5 kN (T), DE: 57.5 kN (T), FG: 75 kN (C), GH: 75 kN (C), AF: 53.03 kN (C), HE: 81.32 kN (C), BF: 0, CG: 25 kN (C), DH: 40 kN (T), FC: 53.03 kN (T), HC: 24.75 kN (T)

Answer

Zero-force member: BF
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: 45 kN (T), BC: 50 kN (T), CD: 50 kN (T), DE: 45 kN (T), FG: 45 kN (C), GH: 45 kN (C), AF: 21.21 kN (C), HE: 63.64 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
5.Shear force & bending moment

Answer: MA = −275 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: −50·5 = −250 kN·m
w: −2·5²/2 = −25 kN·m
MA = −250 − 25 = −275 kN·m

Answer

MA = −275 kN·m

Negative means hogging: tension on the top face.

6.Shear force & bending moment

Answer: E (x = 8 m)

Largest bending moment: M changes slope wherever the shear force changes, so its peaks sit where the shear force crosses zero: under a point load, inside a distributed load, or over a support of an overhang. At a fixed support of a cantilever the moment is largest at the wall. Compare the size of M at those places, sagging or hogging.

Support reactions

Take moments about one support, then use the vertical force balance.

R1 = 25 kN, R2 = 120 kN

Bending moment at every mark

Sum the moments of all forces on one side of the cut. Sagging is positive, hogging negative.

MA = 0, MB = −20, MC = 0, MD = −100, ME = −220 kN·m, MF = −110, MG = 0

Answer

Mark E: ME = −220 kN·m
7.Beam deflection

Answer: δmax = 4.23 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 = 6 N/mm, L = 1500 mm
EI = 9.35 × 10¹⁰ N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·6·1500⁴/(384·9.35 × 10¹⁰) = 4.23 mm

Answer

δmax = 4.23 mm
8.Beam deflection

Answer: Ireq = 1309 × 10⁶ mm⁴

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).

Deflection limit

δallow = L/360 = 8000/360 = 22.22 mm

Required second moment of area

I = 5wL⁴/(384·E·δallow) = 5·6·8000⁴/(384·11000·22.22) = 1.309 × 10⁹ mm⁴
Ireq = 1309 × 10⁶ mm⁴

Answer

Ireq = 1309 × 10⁶ mm⁴
9.Column buckling

Answer: Pcr = 131.6 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 = 50·40³/12 = 266667 mm⁴

Effective length

KL = 1·2000 = 2000 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·266667/2000² = 131595 N = 131.6 kN

Answer

Pcr = 131.6 kN
10.Column buckling

Answer: σcr = 12.34 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 = 1·4000 = 4000 mm
KL/r = 4000/10 = 400

Critical stress

σcr = π²E/(KL/r)² = π²·200000/400² = 12.34 MPa

Answer

σcr = 12.34 MPa
11.Centroid & second moment of area

Answer: Ix = 47.35 × 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 = 220·15 = 3300 mm², yf = 240 + 15/2 = 247.5 mm
web: Aw = 16·240 = 3840 mm², yw = 240/2 = 120 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (3300·247.5 + 3840·120)/7140 = 178.9 mm

Parallel-axis theorem

flange: 220·15³/12 + 3300·(247.5 − 178.9)² = 1.558 × 10⁷ mm⁴
web: 16·240³/12 + 3840·(120 − 178.9)² = 3.177 × 10⁷ mm⁴
Ix = 1.558 × 10⁷ + 3.177 × 10⁷ = 4.735 × 10⁷ mm⁴ = 47.35 × 10⁶ mm⁴

Answer

Ix = 47.35 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 176.5 × 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 three rectangles

Measure every y from the bottom edge.

top flange: A = 2880 mm², y = 290 mm
web: A = 4160 mm², y = 152 mm
bottom flange: A = 5500 mm², y = 11 mm

Centroid

ȳ = (2880·290 + 4160·152 + 5500·11)/12540 = 121.9 mm

Parallel-axis theorem

top flange: 180·16³/12 + 2880·168.1² = 8.149 × 10⁷ mm⁴
web: 16·260³/12 + 4160·30.15² = 2.722 × 10⁷ mm⁴
bottom flange: 250·22³/12 + 5500·110.9² = 6.781 × 10⁷ mm⁴
Ix = 8.149 × 10⁷ + 2.722 × 10⁷ + 6.781 × 10⁷
Ix = 1.765 × 10⁸ mm⁴ = 176.5 × 10⁶ mm⁴

Answer

Ix = 176.5 × 10⁶ mm⁴
13.Effective stress in soil

Answer: σ′ = 135.5 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·zw + γsat·(z − zw) = 15.5·4 + 19·8 = 214 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·8 = 78.48 kPa

Effective stress

σ′ = σ − u = 214 − 78.48 = 135.5 kPa

Answer

σ′ = 135.5 kPa
14.Effective stress in soil

Answer: σ′ = 114.9 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·5 + γsat,sand·1 + γsat,clay·4
σ = 15.5·5 + 18.5·1 + 17·4 = 164 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·5 = 49.05 kPa

Effective stress

σ′ = σ − u = 164 − 49.05 = 114.9 kPa

Answer

σ′ = 114.9 kPa
15.Consolidation settlement

Answer: S = 44.86 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 = 2.5·85 = 212.5 kPa

Compare with the preconsolidation pressure

σ′f = 85 + 140 = 225 kPa > 212.5 kPa

Settlement

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

S = 0.03·3.5/(1 + 0.9)·log₁₀(212.5/85) + 0.5·3.5/(1 + 0.9)·log₁₀(225/212.5)
S = 21.99 + 22.86 = 44.86 mm

Answer

S = 44.86 mm
16.Consolidation settlement

Answer: t = 6.625 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 = 2.5 m

Time

t = Tv·Hdr²/cv = 0.848·2.5²/0.8 = 6.625 years

Answer

t = 6.625 years
17.Hydrostatic force

Answer: F = 78.48 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 + 2/2 = 2 m
A = H·b = 2·2 = 4 m²
gated = 1 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2·4 = 78.48 kN

Answer

F = 78.48 kN
18.Hydrostatic force

Answer: F = 88.07 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 = 4 + 1.5/2 = 4.75 m
A = H·b = 1.5·1 = 1.5 m²
gated = 4 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·4.75·1.5 = 88.07 kN

Answer

F = 88.07 kN
19.Pipe friction & head loss

Answer: hf = 1.957 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) = 1.6²/(2·9.81) = 0.1305 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.03·(150/0.3)·1.6²/(2·9.81) = 1.957 m

Answer

hf = 1.957 m
20.Pipe friction & head loss

Answer: H = 9.564 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 = 0.12/0.04909 = 2.445 m/s
V²/(2g) = 0.3046 m

Loss coefficients

f·L/D = 0.015·400/0.25 = 24
ΣK = 0.5 + 3·0.3 + 5 = 6.4

Energy equation

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

H = (1 + 24 + 6.4)·0.3046 = 9.564 m

Answer

H = 9.564 m
21.Open-channel flow (Manning)

Answer: Q = 0.2156 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 = 0.2209 m², R = D/4 = 0.1875 m

Velocity

V = (1/0.013)·0.18752/3·0.00151/2 = 0.976 m/s

Flow rate

Q = A·V = 0.2209·0.976 = 0.2156 m³/s

Answer

Q = 0.2156 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.0005045 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 = (1.5 + 3·1.2)·1.2 = 6.12 m²
P = b + 2y·√(1 + z²) = 1.5 + 2·1.2·√(1 + 3²) = 9.089 m
R = A/P = 0.6733 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.022·4.8/(6.12·0.7682) = 0.02246
S = 0.02246² = 0.0005045

Answer

S = 0.0005045

That is a fall of 0.5045 m per kilometre.

23.Pumps & pump power

Answer: η = 59.96 %

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 = 1000·9.81·0.05·72 = 35.32 kW

Efficiency

η = Ph/Pshaft = 35.32/58.9 = 59.96%

Answer

η = 59.96%
24.Pumps & pump power

Answer: H = 42.36 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 = 0.04/0.03142 = 1.273 m/s
V²/(2g) = 0.08263 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (13.5 + 8)·0.08263 = 1.776 m

Pressure head

p/(ρ·g) = 300000/(1000·9.81) = 30.58 m

Pump head

Both surfaces are practically at rest, so there is no velocity head term.

H = Δz + p/(ρ·g) + hL = 10 + 30.58 + 1.776 = 42.36 m

Answer

H = 42.36 m
25.Time value of money

Answer: PV = 16710 €

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 = 20 000/1.197 = €16 709.91

Answer

PV = €16 709.91
26.Time value of money

Answer: A = 273.4 €

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 = 12·13 = 156

Deposit

A = FV·i/((1 + i)N − 1) = 50 000·0.002/(1.366 − 1) = €273.43

Answer

A = €273.43
27.NPV & IRR

Answer: NPV = −6960 €

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 + 0.12)1 = 9 000/1.12 = 8 035.71
CF2/(1 + 0.12)2 = 9 000/1.254 = 7 174.74
CF3/(1 + 0.12)3 = 11 000/1.405 = 7 829.58

Add them up

NPV = €−6 959.96

Answer

NPV = €−6 959.96

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

28.NPV & IRR

Answer: IRR = 33.22 %

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(30%) = 464.27
NPV(35%) = −241.33

Narrow down

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

IRR ≈ 30 + 5·464.27/(464.27 − (−241.33)) = 33.29%
exact: NPV(33.22%) = 0 → IRR = 33.22%

Answer

IRR = 33.22%
29.Normal distribution

Answer: P = 0.1056

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

Distribution of the sum

μ = 105 s, σ = √(5² + 4²) = 6.403 s

Standardise

z = (113 − 105)/6.403 = 1.25

Upper tail

P = 1 − Φ(1.25) = 1 − 0.8944 = 0.1056

Answer

P = 0.1056
30.Normal distribution

Answer: x = 84.6 points

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) = 0.975 → z = 1.96

Back to x

x = 65 + 1.96·10 = 84.6 points

Answer

x = 84.6 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