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​ = 40 kNP2​ = 15 kNABRA​RB​ = ?3 m0.5 m2.5 m

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

L = 6 mP1 = 40 kN at 3 mP2 = 15 kN at 3.5 m
RB = kN
2.Beam support reactionsHard
w = 5 kN/mP = 20 kNABRA​ = ?RB​3 m3 m1 m3 m

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

L = 10 mP = 20 kN at 6 mw = 5 kN/m from 3 to 7 m
RA = kN
3.Truss: method of jointsMedium
ABBCACACB60 kN5 m2 m2 m

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

span = 5 mheight = 2 mB is 2 m from Avertical load = 60 kN
FBC = kN
4.Truss: method of jointsHard
ABCDEFGH40 kN15 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: 40 kN →G: 15 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 = 4 kN/mABsection5.5 m0.5 m

Find the bending moment Mx at the section x = 5.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 6 mw = 4 kN/m from 0 to 6 mx = 5.5 m
Mx = kN·m
6.Shear force & bending momentHard
6 kN/m10 kN45 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 @ 12 m45 kN @ 4 m6 kN/m, 0–10 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 = 4 kN/mδL = 2.5 m

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

w = 4 kN/mL = 2.5 mE = 11 GPa (timber)I = 36 × 10⁶ mm⁴
δ = mm
8.Beam deflectionHard
w = 1 kN/mABδ4.5 m

A simply supported timber beam of rectangular section, 100 mm wide, carries a uniformly distributed load w over its whole span. Its midspan deflection may not exceed span/250. Find the smallest depth hreq of the section.

w = 1 kN/mL = 4.5 mE = 11 GPa (timber)b = 100 mm
hreq = mm
9.Column bucklingMedium
PL = 2 m40 × 80 mmcross-section

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

L = 2 mE = 70 GPa (aluminium)b × h = 40 × 80 mm
Pcr = kN
10.Column bucklingHard
P = 10 kNL = 3 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 10 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.

P = 10 kNn = 3L = 3 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
240110t = 16xdimensions in mm

A channel section lies with its open side up: a base plate 240 mm wide with two upright legs, 110 mm high overall. Base and legs are all 16 mm thick. Find its second moment of area Ix about the horizontal axis x through its centroid.

b = 240 mmh = 110 mmt = 16 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
140420106xM = 50 kN·mdimensions in mm

A symmetric I-section has flanges 140 mm wide and 10 mm thick, an overall depth of 420 mm and a web 6 mm thick. It carries a bending moment of 50 kN·m about the axis x. Find the size of the bending stress σj at the junction of the web and the top flange.

B = 140 mmH = 420 mmtf = 10 mmtw = 6 mmM = 50 kN·m
σj = MPa
13.Effective stress in soilMedium
sandγd​ = 17 kN/m³γsat​ = 20 kN/m³8 mwater tableXz = 6 m

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

z = 6 mzw = 4 mγw = 9.81 kN/m³sand: γd = 17 kN/m³sand: γsat = 20 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 15 kN/m³γsat​ = 20 kN/m³3 mclayγsat​ = 19 kN/m³8 mwater tableXz = 7 m

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

z = 7 mzw = 2 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 20 kN/m³clay: γsat = 19 kN/m³
σ = kPa
15.Consolidation settlementMedium
Δσ = 25 kPasandclayCc​ = 0.35, Cr​ = 0.05e0​ = 0.7σ′0​ = 55 kPaσ′p​ = 115 kPa3.5 mwater table

A 3.5 m thick overconsolidated clay layer has Cc = 0.35, Cr = 0.05 and e₀ = 0.7. At its mid-depth the effective vertical stress is 55 kPa and the preconsolidation pressure is 115 kPa. A new building adds 25 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 3.5 mCc = 0.35Cr = 0.05e0 = 0.7σ′0 = 55 kPaσ′p = 115 kPaΔσ = 25 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 2.5 mcv​ = 4 m²/year2.5 mimpervious rockwater table

A clay layer 2.5 m thick has a coefficient of consolidation cv = 4 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 = 2.5 mcv = 4 m²/yearU = 60%Tv = 0.287single drainage
t = years
17.Hydrostatic forceMedium
gated = 1.5 mH = 1 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of water, with its top edge 1.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 1.5 mH = 1 mb = 2 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 1.5 mH = 1.5 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of oil, with its top edge 1.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 1.5 mH = 1.5 mb = 2 mρ = 880 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
Q = 3 L/sD = 50 mmL = 100 mf = 0.028

Water flows at 3 L/s through a pipe 100 m long with an inside diameter of 50 mm. Use the Darcy friction factor f = 0.028 and g = 9.81 m/s². Find the friction head loss hf.

Q = 3 L/sL = 100 mD = 50 mmf = 0.028g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 2free outletH = ?L = 200 m, D = 250 mm, f = 0.0254× bend (K = 0.3)

A pipe 200 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), 4 bends (K = 0.3 each) and a valve (K = 2). 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 = 200 mD = 250 mmf = 0.025Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 2
H = m
21.Open-channel flow (Manning)Medium
b = 4 my = 2.4 m2 : 1n = 0.022, S = 0.003

A trapezoidal clean earth channel has a bottom width of 4 m and side slopes of 2:1 (horizontal:vertical). Water flows uniformly 2.4 m deep. Manning n = 0.022 and the bed slope is S = 0.003. Find the flow rate Q in m³/s.

b = 4 my = 2.4 mz = 2n = 0.022S = 0.003
Q = m³/s
22.Open-channel flow (Manning)Hard
D = 375 mmn = 0.013, V = 1 m/s

A concrete sewer with an inside diameter of 375 mm (Manning n = 0.013) must reach a self-cleansing velocity of 1 m/s when flowing just full. Find the minimum slope S (in m/m).

D = 375 mmn = 0.013V = 1 m/s
S = m/m
23.Pumps & pump powerMedium
PQ = 40 L/sH = 32 m

A pump with an efficiency of 72% delivers 40 L/s of water (ρ = 1000 kg/m³) against a head of 32 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 40 L/sH = 32 mη = 72%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 100 L/sΔz = 8 mL = 150 m, D = 250 mm, f = 0.015, ΣK = 4

A pump moves 100 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 8 m higher. The pipe is 150 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.015; the minor-loss coefficients add up to ΣK = 4 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 80%. Find the shaft power Pshaft in kW.

Q = 100 L/sΔz = 8 mL = 150 mD = 250 mmf = 0.015ΣK = 4η = 80%
Pshaft = kW
25.Time value of moneyMedium
years0123…17PV = ?€2 000€2 000€2 000€2 000

An annuity pays €2 000 at the end of each year for 17 years. The interest rate is 7% per year. Find the present value PV of the annuity.

A = €2 000i = 7%n = 17
PV = €
26.Time value of moneyHard
months0123…72€300€300€300FV = ?

You save €300 at the end of every month for 6 years. The account pays 7.2% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €3007.2% / 12N = 72
FV = €
27.NPV & IRRMedium
years0123−60 00021 00015 00013 000

An investment of €60 000 gives these cash flows at the end of years 1 to 3: €21 000, €15 000, €13 000. The cost of capital is 15%. Find the net present value NPV.

r = 15%CF0 = −60 000CF1 = 21 000CF2 = 15 000CF3 = 13 000
NPV = €
28.NPV & IRRHard
years0123−50 00031 00034 00034 000

A project costs €50 000 and returns €31 000, €34 000, €34 000 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −50 000CF1 = 31 000CF2 = 34 000CF3 = 34 000
IRR = %
29.Normal distributionMedium
502532P = ?

The battery lifetimes are normally distributed with mean 500 h and standard deviation 40 h. What fraction lies between 502 and 532 h? Give P as a decimal.

μ = 500σ = 40x1 = 502x2 = 532
P =
30.Normal distributionHard
μ = 32x = ?90%

The delivery times are normally distributed with mean 32 min and standard deviation 6 min. Find the value x below which 90% of them lie (the 90th percentile).

μ = 32σ = 6P = 90%
x = min

3Solutions

1.Beam support reactions

Answer: RB = 28.75 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​ = 40 kNP2​ = 15 kNABRA​RB​3 m0.5 m2.5 m

Free-body diagram

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

Equilibrium

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

ΣMA = 0: RB·6 = 40·3 + 15·3.5
RB = 172.5/6 = 28.75 kN
ΣFy = 0: RA = 55 − 28.75 = 26.25 kN

Answer

RB = 28.75 kN
2.Beam support reactions

Answer: RA = 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.

w = 5 kN/mP = 20 kNABRA​RB​3 m3 m1 m3 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 = 5·4 = 20 kN, acting at x̄ = 5 m
ΣMA = 0: RB·10 = 20·6 + 5·4·5
RB = 220/10 = 22 kN
ΣFy = 0: RA = 40 − 22 = 18 kN

Answer

RA = 18 kN
3.Truss: method of joints

Answer: FBC = −43.27 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.

ABBCACACB60 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·5 = 60·2 → Cy = 24 kN
ΣFy = 0: Ay = 60 − 24 = 36 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 = 2/3.606 = 0.5547, cos γ = 3/3.606 = 0.8321
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −24/0.5547 = −43.27 kN

Answer

FBC = −43.27 kN (compression)
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: 37.5 kN (T), BC: 35 kN (T), CD: 35 kN (T), DE: 17.5 kN (T), FG: 37.5 kN (C), GH: 17.5 kN (C), AF: 3.536 kN (T), HE: 24.75 kN (C), BF: 2.5 kN (C), CG: 0, DH: 17.5 kN (T), BG: 3.536 kN (T), DG: 24.75 kN (C)

Answer

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

Answer: Mx = 5.5 kN·m

Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 4·6 = 24 kN, acting at x̄ = 3 m
ΣMA = 0: RB·6 = 4·6·3
RB = 72/6 = 12 kN
ΣFy = 0: RA = 24 − 12 = 12 kN
w = 4 kN/mABRA​ = 12RB​ = 12section5.5 m0.5 m

Cut at x = 5.5 m and keep the left part

Only forces left of the cut appear. A UDL portion acts as one force at the middle of that portion.

M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 12·5.5 − 4·5.5·2.75 = 5.5 kN·m

Answer

Mx = 5.5 kN·m
6.Shear force & bending moment

Answer: C (x = 4 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 = 55 kN, R2 = 60 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 = 98, MC = 172 kN·m, MD = 132, ME = 68, MF = −20, MG = 0

Answer

Mark C: MC = 172 kN·m
7.Beam deflection

Answer: δ = 49.32 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 = 4 N/mm, L = 2500 mm
EI = 3.96 × 10¹¹ N·mm²

Deflection

δ = wL⁴/(8EI) = 4·2500⁴/(8·3.96 × 10¹¹) = 49.32 mm

Answer

δ = 49.32 mm
8.Beam deflection

Answer: hreq = 147.9 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 = 1 N/mm, L = 4500 mm, E = 11000 N/mm²

Deflection limit

δallow = L/250 = 4500/250 = 18 mm

Required second moment of area

Ireq = 5wL⁴/(384·E·δallow) = 5·1·4500⁴/(384·11000·18) = 2.697 × 10⁷ mm⁴

Required depth

bh³/12 = Ireq → h = (12·2.697 × 10⁷/100)1/3 = 147.9 mm

Answer

hreq = 147.9 mm

In practice, choose the next standard depth above this value.

9.Column buckling

Answer: Pcr = 150.4 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 = 0.7·2000 = 1400 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·426667/1400² = 150394 N = 150.4 kN

Answer

Pcr = 150.4 kN
10.Column buckling

Answer: d = 34.18 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 = 3·10000 = 30000 N
KL = 0.7·3000 = 2100 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·30000·2100²/(π³·200000))^(1/4) = 34.18 mm

Answer

d = 34.18 mm

Check: the slenderness KL/r is 245.7, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: Ix = 7.399 × 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 rectangles

Take the base at full width and the two legs above it (height h − t), so nothing is counted twice.

base: A1 = 240·16 = 3840 mm², y1 = 8 mm
two legs: A2 = 2·16·94 = 3008 mm², y2 = 16 + 94/2 = 63 mm

Centroid

ȳ = (3840·8 + 3008·63)/6848 = 32.16 mm

Parallel-axis theorem

base: 240·16³/12 + 3840·(8 − 32.16)² = 2.323 × 10⁶ mm⁴
two legs: 2·16·94³/12 + 3008·(63 − 32.16)² = 5.076 × 10⁶ mm⁴
Ix = 2.323 × 10⁶ + 5.076 × 10⁶
Ix = 7.399 × 10⁶ mm⁴ = 7.399 × 10⁶ mm⁴

Answer

Ix = 7.399 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σj = 66.8 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.

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 = 420 − 2·10 = 400 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (140·420³ − 134·400³)/12
Ix = 1.497 × 10⁸ mm⁴

Bending stress

y = 210 − 10 = 200 mm
σ = M·y/I = 5 × 10⁷·200/1.497 × 10⁸ = 66.8 MPa

Answer

σj = 66.8 MPa
13.Effective stress in soil

Answer: σ′ = 88.38 kPa

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

Total stress

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

σ = γd·zw + γsat·(z − zw) = 17·4 + 20·2 = 108 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·2 = 19.62 kPa

Effective stress

σ′ = σ − u = 108 − 19.62 = 88.38 kPa

Answer

σ′ = 88.38 kPa
14.Effective stress in soil

Answer: σ = 126 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·1 + γsat,clay·4
σ = 15·2 + 20·1 + 19·4 = 126 kPa

Answer

σ = 126 kPa
15.Consolidation settlement

Answer: S = 16.75 mm

Primary consolidation of a clay layer of thickness H, using the effective stress at the middle of the layer: σ′f = σ′0 + Δσ. Normally consolidated clay: S = Cc·H/(1 + e0)·log₁₀(σ′f/σ′0). Overconsolidated clay recompresses along Cr up to the preconsolidation pressure σ′p and follows Cc only beyond it. Time: t = Tv·Hdr²/cv, where the drainage path Hdr is H/2 when water can leave at the top and bottom, and H when only one side drains.

Compare with the preconsolidation pressure

σ′f = 55 + 25 = 80 kPa ≤ 115 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.05·3.5/(1 + 0.7)·log₁₀(80/55) = 16.75 mm

Answer

S = 16.75 mm
16.Consolidation settlement

Answer: t = 0.4484 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 = 0.287·2.5²/4 = 0.4484 years

Answer

t = 0.4484 years
17.Hydrostatic force

Answer: F = 39.24 kN

Hydrostatic force on a plane surface: F = ρ·g·yc·A. It acts at the centre of pressure, ycp = yc + Ic/(ycA), which always lies below the centroid.

Centroid depth and area

yc = d + H/2 = 1.5 + 1/2 = 2 m
A = H·b = 1·2 = 2 m²
gated = 1.5 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2·2 = 39.24 kN

Answer

F = 39.24 kN
18.Hydrostatic force

Answer: F = 58.27 kN

Hydrostatic force on a plane surface: F = ρ·g·yc·A. It acts at the centre of pressure, ycp = yc + Ic/(ycA), which always lies below the centroid.

Centroid depth and area

yc = d + H/2 = 1.5 + 1.5/2 = 2.25 m
A = H·b = 1.5·2 = 3 m²
gated = 1.5 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 880·9.81·2.25·3 = 58.27 kN

Answer

F = 58.27 kN
19.Pipe friction & head loss

Answer: hf = 6.663 m

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

Mean velocity

A = π·0.05²/4 = 0.001963 m²
V = Q/A = 0.003/0.001963 = 1.528 m/s

Velocity head

V²/(2g) = 1.528²/(2·9.81) = 0.119 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.028·(100/0.05)·1.528²/(2·9.81) = 6.663 m

Answer

hf = 6.663 m
20.Pipe friction & head loss

Answer: H = 1.306 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 = 0.025·200/0.25 = 20
ΣK = 0.5 + 4·0.3 + 2 = 3.7

Energy equation

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

H = (1 + 20 + 3.7)·0.05288 = 1.306 m

Answer

H = 1.306 m
21.Open-channel flow (Manning)

Answer: Q = 66.85 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 = (4 + 2·2.4)·2.4 = 21.12 m²
P = b + 2y·√(1 + z²) = 4 + 2·2.4·√(1 + 2²) = 14.73 m
R = A/P = 1.434 m

Velocity

V = (1/0.022)·1.4342/3·0.0031/2 = 3.165 m/s

Flow rate

Q = A·V = 21.12·3.165 = 66.85 m³/s

Answer

Q = 66.85 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.003968 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 = 0.375/4 = 0.09375 m

Solve Manning for S

S = (n·V/R2/3)² = (0.013·1/0.2064)² = 0.003968

Answer

S = 0.003968

That is a fall of 3.968 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 17.44 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 = 1000·9.81·0.04·32 = 12.56 kW

Shaft power

Pshaft = Ph/η = 12.56/0.72 = 17.44 kW

Answer

Pshaft = 17.44 kW
24.Pumps & pump power

Answer: Pshaft = 13.18 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 = 0.1/0.04909 = 2.037 m/s
V²/(2g) = 0.2115 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (9 + 4)·0.2115 = 2.75 m

Pump head

H = Δz + hL = 8 + 2.75 = 10.75 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.1·10.75/0.8 = 13.18 kW

Answer

Pshaft = 13.18 kW
25.Time value of money

Answer: PV = 19526 €

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.

Annuity factor

(1 − (1 + i)−n)/i = (1 − 0.3166)/0.07 = 9.763

Present value

PV = 2 000·9.763 = €19 526.45

Answer

PV = €19 526.45
26.Time value of money

Answer: FV = 26917 €

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

Monthly rate and number of deposits

i = 0.07200000000000001/12 = 0.006
N = 12·6 = 72

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 300·(1.538 − 1)/0.006 = €26 917.40

Answer

FV = €26 917.40

You paid in €21 600 yourself; the rest is interest.

27.NPV & IRR

Answer: NPV = −21849 €

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 = −60 000
CF1/(1 + 0.15)1 = 21 000/1.15 = 18 260.87
CF2/(1 + 0.15)2 = 15 000/1.322 = 11 342.16
CF3/(1 + 0.15)3 = 13 000/1.521 = 8 547.71

Add them up

NPV = €−21 849.26

Answer

NPV = €−21 849.26

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

28.NPV & IRR

Answer: IRR = 42.89 %

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(40%) = 1 880.47
NPV(45%) = −1 296.90

Narrow down

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

IRR ≈ 40 + 5·1 880.47/(1 880.47 − (−1 296.90)) = 42.96%
exact: NPV(42.89%) = 0 → IRR = 42.89%

Answer

IRR = 42.89%
29.Normal distribution

Answer: P = 0.2682

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 = (502 − 500)/40 = 0.05
z₂ = (532 − 500)/40 = 0.8

Area between

P = Φ(0.8) − Φ(0.05) = 0.7881 − 0.5199 = 0.2682

Answer

P = 0.2682
30.Normal distribution

Answer: x = 39.69 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) = 0.9 → z = 1.282

Back to x

x = 32 + 1.282·6 = 39.69 min

Answer

x = 39.69 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