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​ = 20 kNP2​ = 15 kNABRA​RB​ = ?3 m5 m2 m

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

L = 10 mP1 = 20 kN at 3 mP2 = 15 kN at 8 m
RB = kN
2.Beam support reactionsHard
w = 4 kN/mP = 45 kNABRA​ = ?RB​2 m1 m7 m

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

L = 10 mP = 45 kN at 3 mw = 4 kN/m from 2 to 3 m
RA = kN
3.Truss: method of jointsMedium
ABCDEFGH10 kN40 kN15 kN30 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: 10 kN ↓D: 40 kN ↓G: 15 kN ↓H: 30 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
ABBCACACB55 kN5 kN5 m3 m2 m

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

span = 5 mheight = 2 mB is 3 m from Avertical load = 55 kNhorizontal load = 5 kN →
FAC = kN
5.Shear force & bending momentMedium
P1​ = 55 kNP2​ = 80 kNABC1 m4 m2 m

The beam rests on a pin at A and a roller at B and overhangs B by 2 m to the free end C. It carries a point load P1 between the supports and a point load P2 at C. Find the bending moment Mx under the load P1. Use sagging moments positive and upward shear on the left face positive.

L = 7 mP1 = 55 kN at 1 mP2 = 80 kN at 7 msupports at x = 0 and x = 5 m
Mx = kN·m
6.Shear force & bending momentHard
w = 6 kN/mP = 65 kNAB4 m1 m

The simply supported beam carries a uniformly distributed load w over its whole span and a point load P. Find the maximum bending moment Mmax in the beam.

L = 5 mP = 65 kN at 4 mw = 6 kN/m from 0 to 5 m
Mmax = kN·m
7.Beam deflectionMedium
w = 20 kN/mδL = 3 m

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

w = 20 kN/mL = 3 mE = 200 GPa (steel)I = 160 × 10⁶ mm⁴
δ = mm
8.Beam deflectionHard
w = 4 kN/mP = 2 kNδL = 5 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 = 2 kNw = 4 kN/mL = 5 mE = 200 GPa (steel)I = 120 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 4 md = 60 mmcross-section

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

L = 4 mE = 70 GPa (aluminium)d = 60 mm
Pcr = kN
10.Column bucklingHard
PL = 2.5 md = 80 mmcross-section

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

L = 2.5 mE = 70 GPa (aluminium)d = 80 mm
σcr = MPa
11.Centroid & second moment of areaMedium
1804402414xdimensions in mm

A symmetric I-section has flanges 180 mm wide and 24 mm thick, an overall depth of 440 mm and a web 14 mm thick. Find its second moment of area Ix about the horizontal centroidal axis x.

B = 180 mmH = 440 mmtf = 24 mmtw = 14 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
1802528016xM = 25 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 25 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 180 mmtf = 25 mmtw = 16 mmhw = 280 mmM = 25 kN·m
σtop = MPa
13.Effective stress in soilMedium
sandγd​ = 15 kN/m³γsat​ = 20.5 kN/m³10 mwater tableXz = 8 m

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

z = 8 mzw = 4 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 20.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 16 kN/m³γsat​ = 20 kN/m³4 mclayγsat​ = 18.5 kN/m³8 mwater tableXz = 8 m

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

z = 8 mzw = 2 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 20 kN/m³clay: γsat = 18.5 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 170 kPasandclayCc​ = 0.25, Cr​ = 0.03e0​ = 0.85σ′0​ = 115 kPaOCR = 2.56 mwater table

A 6 m thick overconsolidated clay layer has Cc = 0.25, Cr = 0.03 and e₀ = 0.85. At its mid-depth the effective vertical stress is 115 kPa and the overconsolidation ratio is OCR = 2.5. A new building adds 170 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 6 mCc = 0.25Cr = 0.03e0 = 0.85σ′0 = 115 kPaOCR = 2.5Δσ = 170 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 6 mcv​ = 2.5 m²/year6 mimpervious rockwater table

A clay layer 6 m thick has a coefficient of consolidation cv = 2.5 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 60% average consolidation the time factor is Tv = 0.287. How many years t does the layer take to reach 60% consolidation?

H = 6 mcv = 2.5 m²/yearU = 60%Tv = 0.287single drainage
t = years
17.Hydrostatic forceMedium
gated = 1.5 mH = 2.5 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 = 2.5 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 3 mH = 1.5 m

A vertical rectangular gate 1 m wide sits in the wall of a tank of glycerin, with its top edge 3 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 3 mH = 1.5 mb = 1 mρ = 1260 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
V = 2.7 m/sD = 100 mmL = 1000 mf = 0.02

Water (ρ = 1000 kg/m³) flows at 2.7 m/s through a horizontal pipe, 1000 m long, with an inside diameter of 100 mm. Use the Darcy friction factor f = 0.02 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 2.7 m/sL = 1000 mD = 100 mmf = 0.02ρ = 1000 kg/m³
Δp = kPa
20.Pipe friction & head lossHard
K = 5Δz = ?L = 100 m, D = 250 mm, f = 0.024× bend (K = 0.3)

Two open reservoirs are joined by a pipe 100 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.02. The minor losses are a square-edged entrance (K = 0.5), 4 bends (K = 0.3 each), a valve (K = 5) and the exit into the lower reservoir (K = 1.0). Use g = 9.81 m/s². What difference in water level Δz between the reservoirs gives a flow rate of 60 L/s?

Q = 60 L/sL = 100 mD = 250 mmf = 0.02Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 5Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
b = 1 my = 2.1 m3 : 1n = 0.03, S = 0.002

A trapezoidal grass-lined earth channel has a bottom width of 1 m and side slopes of 3:1 (horizontal:vertical). Water flows uniformly 2.1 m deep. Manning n = 0.03 and the bed slope is S = 0.002. Find the flow rate Q in m³/s.

b = 1 my = 2.1 mz = 3n = 0.03S = 0.002
Q = m³/s
22.Open-channel flow (Manning)Hard
D = 450 mmn = 0.013, V = 0.9 m/s

A concrete sewer with an inside diameter of 450 mm (Manning n = 0.013) must reach a self-cleansing velocity of 0.9 m/s when flowing just full. Find the minimum slope S (in m/m).

D = 450 mmn = 0.013V = 0.9 m/s
S = m/m
23.Pumps & pump powerMedium
PQ = 60 L/sH = 44 m

In a test, a pump delivers 60 L/s of water (ρ = 1000 kg/m³) against a head of 44 m while its shaft takes 37 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.

Q = 60 L/sH = 44 mPshaft = 37 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
PQ = 50 L/sΔz = 5 mL = 200 m, D = 150 mm, f = 0.02, ΣK = 2.5

A pump moves 50 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 5 m higher. The pipe is 200 m long with an inside diameter of 150 mm and a Darcy friction factor f = 0.02; the minor-loss coefficients add up to ΣK = 2.5 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 75%. Find the shaft power Pshaft in kW.

Q = 50 L/sΔz = 5 mL = 200 mD = 150 mmf = 0.02ΣK = 2.5η = 75%
Pshaft = kW
25.Time value of moneyMedium
periods0123…36511 + EAR = ?22% / 365

A credit card charges a nominal interest rate of 22% per year, compounded daily. Find the effective annual rate EAR in percent.

r = 22%m = 365
EAR = %
26.Time value of moneyHard
months0123…48€12 000A?AAA

A loan of €12 000 is repaid with equal monthly payments over 4 years. The interest rate is 4.8% per year, compounded monthly. Find the monthly payment A.

P = €12 0004.8% / 12N = 48
A = €
27.NPV & IRRMedium
years012345−60 00019 50013 50016 00023 00012 500

A project costs €60 000 today and returns €19 500, €13 500, €16 000, €23 000, €12 500 at the end of years 1 to 5. The cost of capital is 12%. Assume cash flows arrive evenly through each year. Find the discounted payback period DPB in years.

r = 12%CF0 = −60 000CF1 = 19 500CF2 = 13 500CF3 = 16 000CF4 = 23 000CF5 = 12 500
DPB = years
28.NPV & IRRHard
years0123−50 00034 00030 00028 000

A project costs €50 000 and returns €34 000, €30 000, €28 000 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −50 000CF1 = 34 000CF2 = 30 000CF3 = 28 000
IRR = %
29.Normal distributionMedium
105 s98.6 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 98.6 s. Round z to two decimals.

μX = 60, σX = 5μY = 45, σY = 4X + Y > 98.6 s
P =
30.Normal distributionHard
0.04 mm0D − d?

Hole diameters D are normal with mean 25.04 mm and standard deviation 0.02 mm. Shaft diameters d are independent and normal with mean 25 mm and standard deviation 0.01 mm. A randomly chosen shaft fits when D − d > 0. Find the probability P that it fits. Round z to two decimals.

hole: μ = 25.04 mm, σ = 0.02 mmshaft: μ = 25 mm, σ = 0.01 mm
P =

3Solutions

1.Beam support reactions

Answer: RB = 18 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​ = 20 kNP2​ = 15 kNABRA​RB​3 m5 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·10 = 20·3 + 15·8
RB = 180/10 = 18 kN
ΣFy = 0: RA = 35 − 18 = 17 kN

Answer

RB = 18 kN
2.Beam support reactions

Answer: RA = 34.5 kN

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

w = 4 kN/mP = 45 kNABRA​RB​2 m1 m7 m

Free-body diagram

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

Equilibrium

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

UDL resultant: W = w·ℓ = 4·1 = 4 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·10 = 45·3 + 4·1·2.5
RB = 145/10 = 14.5 kN
ΣFy = 0: RA = 49 − 14.5 = 34.5 kN

Answer

RA = 34.5 kN
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: 32.5 kN (T), BC: 55 kN (T), CD: 55 kN (T), DE: 62.5 kN (T), FG: 32.5 kN (C), GH: 62.5 kN (C), AF: 45.96 kN (C), HE: 88.39 kN (C), BF: 32.5 kN (T), CG: 0, DH: 32.5 kN (T), BG: 31.82 kN (C), DG: 10.61 kN (T)

Answer

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

Answer: FAC = 35 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.

ABBCACACB55 kN5 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·5 = 55·3 + 5·2 → Cy = 35 kN
ΣFy = 0: Ay = 55 − 35 = 20 kN
ΣFx = 0: Ax = −5 kN

Joint C

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

sin γ = 2/2.828 = 0.7071, cos γ = 2/2.828 = 0.7071
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −35/0.7071 = −49.5 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−49.5)·0.7071 = 35 kN

Answer

FAC = 35 kN (tension)
5.Shear force & bending moment

Answer: Mx = 12 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. The overhang load also acts about A.

ΣMA = 0: RB·5 = 55·1 + 80·7
RB = 615/5 = 123 kN
ΣFy = 0: RA = 135 − 123 = 12 kN

Cut under P1 and keep the left part

Mx = RA·1 = 12·1 = 12 kN·m

Answer

Mx = 12 kN·m
6.Shear force & bending moment

Answer: Mmax = 64 kN·m

Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut. 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 = 6·5 = 30 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 65·4 + 6·5·2.5
RB = 335/5 = 67 kN
ΣFy = 0: RA = 95 − 67 = 28 kN

Where is V = 0?

V(4⁻) = RA − w·4 = 4 kN
V(4⁺) = 4 − 65 = −61 kN
The shear changes sign at the load, so the maximum is under the load.

Maximum moment

Mmax = RA·4 − w·4²/2 = 28·4 − 6·4²/2 = 64 kN·m

Answer

Mmax = 64 kN·m

It occurs at x = 4 m from A.

7.Beam deflection

Answer: δ = 6.328 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 = 20 N/mm, L = 3000 mm
EI = 3.2 × 10¹³ N·mm²

Deflection

δ = wL⁴/(8EI) = 20·3000⁴/(8·3.2 × 10¹³) = 6.328 mm

Answer

δ = 6.328 mm
8.Beam deflection

Answer: δmax = 1.573 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 = 2000 N, w = 4 N/mm, L = 5000 mm, EI = 2.4 × 10¹³ N·mm²

Each load on its own

δP = PL³/(48EI) = 2000·5000³/(48·2.4 × 10¹³) = 0.217 mm
δw = 5wL⁴/(384EI) = 5·4·5000⁴/(384·2.4 × 10¹³) = 1.356 mm

Add them

δmax = 0.217 + 1.356 = 1.573 mm

Answer

δmax = 1.573 mm
9.Column buckling

Answer: Pcr = 6.867 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·60⁴/64 = 636173 mm⁴

Effective length

KL = 2·4000 = 8000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·636173/8000² = 6867 N = 6.867 kN

Answer

Pcr = 6.867 kN
10.Column buckling

Answer: σcr = 44.22 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·80⁴/64 = 2.011 × 10⁶ mm⁴

Radius of gyration and slenderness

A = 5027 mm²
r = √(I/A) = √(2.011 × 10⁶/5027) = 20 mm
KL = 1·2500 = 2500 mm
KL/r = 2500/20 = 125

Critical stress

σcr = π²E/(KL/r)² = π²·70000/125² = 44.22 MPa

Answer

σcr = 44.22 MPa
11.Centroid & second moment of area

Answer: Ix = 444.5 × 10⁶ mm⁴

Second moment of area: for a rectangle about its own centroidal axis I = bh³/12, and about its base bh³/3 (parallel-axis theorem I = Ic + A·d²). A hole is handled by subtracting its I, as long as both parts share the same axis. The elastic section modulus is S = I/c, where c is the distance to the extreme fibre.

Outer rectangle minus the two side cut-outs

Both cut-outs together are (B − tw) wide and hw = H − 2tf high, and share the axis x.

hw = 440 − 2·24 = 392 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (180·440³ − 166·392³)/12
Ix = 4.445 × 10⁸ mm⁴ = 444.5 × 10⁶ mm⁴

Answer

Ix = 444.5 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 27.1 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 = 180·25 = 4500 mm², yf = 280 + 25/2 = 292.5 mm
web: Aw = 16·280 = 4480 mm², yw = 280/2 = 140 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (4500·292.5 + 4480·140)/8980 = 216.4 mm

Parallel-axis theorem

flange: 180·25³/12 + 4500·(292.5 − 216.4)² = 2.628 × 10⁷ mm⁴
web: 16·280³/12 + 4480·(140 − 216.4)² = 5.543 × 10⁷ mm⁴
Ix = 2.628 × 10⁷ + 5.543 × 10⁷ = 8.171 × 10⁷ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 305 − 216.4 = 88.58 mm
σ = M·y/I = 2.5 × 10⁷·88.58/8.171 × 10⁷ = 27.1 MPa

Answer

σtop = 27.1 MPa
13.Effective stress in soil

Answer: σ′ = 102.8 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) = 15·4 + 20.5·4 = 142 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·4 = 39.24 kPa

Effective stress

σ′ = σ − u = 142 − 39.24 = 102.8 kPa

Answer

σ′ = 102.8 kPa
14.Effective stress in soil

Answer: σ′ = 87.14 kPa

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

Total stress

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

σ = γd·2 + γsat,sand·2 + γsat,clay·4
σ = 16·2 + 20·2 + 18.5·4 = 146 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·6 = 58.86 kPa

Effective stress

σ′ = σ − u = 146 − 58.86 = 87.14 kPa

Answer

σ′ = 87.14 kPa
15.Consolidation settlement

Answer: S = 38.35 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 = 2.5·115 = 287.5 kPa

Compare with the preconsolidation pressure

σ′f = 115 + 170 = 285 kPa ≤ 287.5 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.03·6/(1 + 0.85)·log₁₀(285/115) = 38.35 mm

Answer

S = 38.35 mm
16.Consolidation settlement

Answer: t = 4.133 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 = 6 m

Time

t = Tv·Hdr²/cv = 0.287·6²/2.5 = 4.133 years

Answer

t = 4.133 years
17.Hydrostatic force

Answer: F = 67.44 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 + 2.5/2 = 2.75 m
A = H·b = 2.5·1 = 2.5 m²
gated = 1.5 mH = 2.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2.75·2.5 = 67.44 kN

Answer

F = 67.44 kN
18.Hydrostatic force

Answer: F = 69.53 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 = 3 + 1.5/2 = 3.75 m
A = H·b = 1.5·1 = 1.5 m²
gated = 3 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·3.75·1.5 = 69.53 kN

Answer

F = 69.53 kN
19.Pipe friction & head loss

Answer: Δp = 729 kPa

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

Head loss

hf = f·(L/D)·V²/(2g) = 0.02·(1000/0.1)·2.7²/(2·9.81) = 74.31 m

Pressure drop

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

Δp = ρ·g·hf = 1000·9.81·74.31 = 729000 Pa = 729 kPa

Answer

Δp = 729 kPa
20.Pipe friction & head loss

Answer: Δz = 1.196 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 = 0.06/0.04909 = 1.222 m/s
V²/(2g) = 0.07615 m

Loss coefficients

f·L/D = 0.02·100/0.25 = 8
ΣK = 0.5 + 4·0.3 + 5 + 1.0 = 7.7

Total head loss

hf = 8·0.07615 = 0.6092 m
hm = 7.7·0.07615 = 0.5863 m
Δz = hf + hm = 1.196 m

Answer

Δz = 1.196 m
21.Open-channel flow (Manning)

Answer: Q = 23.96 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 = (1 + 3·2.1)·2.1 = 15.33 m²
P = b + 2y·√(1 + z²) = 1 + 2·2.1·√(1 + 3²) = 14.28 m
R = A/P = 1.073 m

Velocity

V = (1/0.03)·1.0732/3·0.0021/2 = 1.563 m/s

Flow rate

Q = A·V = 15.33·1.563 = 23.96 m³/s

Answer

Q = 23.96 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.002521 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.

Hydraulic radius

R = D/4 = 0.45/4 = 0.1125 m

Solve Manning for S

S = (n·V/R2/3)² = (0.013·0.9/0.233)² = 0.002521

Answer

S = 0.002521

That is a fall of 2.521 m per kilometre.

23.Pumps & pump power

Answer: η = 70 %

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 = 1000·9.81·0.06·44 = 25.9 kW

Efficiency

η = Ph/Pshaft = 25.9/37 = 70%

Answer

η = 70%
24.Pumps & pump power

Answer: Pshaft = 11.05 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 = 0.05/0.01767 = 2.829 m/s
V²/(2g) = 0.408 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (26.67 + 2.5)·0.408 = 11.9 m

Pump head

H = Δz + hL = 5 + 11.9 = 16.9 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.05·16.9/0.75 = 11.05 kW

Answer

Pshaft = 11.05 kW
25.Time value of money

Answer: EAR = 24.6 %

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

Rate per period

r/m = 0.22/365 = 0.0006027

Compound over one year

EAR = (1 + 0.0006027)365 − 1 = 1.246 − 1 = 24.6%

Answer

EAR = 24.6%

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

26.Time value of money

Answer: A = 275.3 €

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 payments

i = 0.048/12 = 0.004
N = 12·4 = 48

Payment

The present value of N equal payments A is A·(1 − (1 + i)⁻ᴺ)/i. Set it equal to the loan and solve for A.

(1 + i)−N = 0.8256
A = 12 000·0.004/(1 − 0.8256) = €275.27

Answer

A = €275.27
27.NPV & IRR

Answer: DPB = 4.821 years

Payback period: the time until the cumulative cash flows repay the initial investment. Cash is assumed to come in evenly during each year, so the last part is a fraction of a year. The simple payback ignores the time value of money; the discounted payback period uses the discounted cash flows instead.

Discounted and cumulative cash flows

year 1: 19 500/1.12 = 17 410.71 → Σ = 17 410.71
year 2: 13 500/1.254 = 10 762.12 → Σ = 28 172.83
year 3: 16 000/1.405 = 11 388.48 → Σ = 39 561.32
year 4: 23 000/1.574 = 14 616.92 → Σ = 54 178.23
year 5: 12 500/1.762 = 7 092.84 → Σ = 61 271.07

Fraction of the last year

DPB = 4 + 5 821.77/7 092.84 = 4.821

Answer

DPB = 4.821 years

The discounted payback is always longer than the simple payback (3.478 years).

28.NPV & IRR

Answer: IRR = 39.67 %

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(35%) = 3 026.47
NPV(40%) = −204.08

Narrow down

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

IRR ≈ 35 + 5·3 026.47/(3 026.47 − (−204.08)) = 39.68%
exact: NPV(39.67%) = 0 → IRR = 39.67%

Answer

IRR = 39.67%
29.Normal distribution

Answer: P = 0.8413

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

Distribution of the sum

μ = 105 s, σ = √(5² + 4²) = 6.403 s

Standardise

z = (98.6 − 105)/6.403 = −1

Upper tail

P = 1 − Φ(−1) = 1 − 0.1587 = 0.8413

Answer

P = 0.8413
30.Normal distribution

Answer: P = 0.9633

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

Distribution of the difference

μ = 25.04 − 25 = 0.04 mm, σ = 0.02236 mm

Standardise

z = (0 − 0.04)/0.02236 = −1.79

Probability

P = 1 − Φ(−1.79) = 0.9633

Answer

P = 0.9633

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