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.

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1Formulas and methods

Beam support reactions

Equilibrium
ΣFx = 0, ΣFy = 0, ΣM = 0
Uniform load
resultant w·L at the middle of the load
Moment
M = F·d

Method

  1. Draw a free-body diagram and replace each support by its reactions.
  2. Replace every distributed load by a single force at its centroid.
  3. Take moments about one support to find the reaction at the other.
  4. Use ΣFy = 0 to find the remaining reaction, and check with a second moment equation.

Truss: method of joints

Method of joints
ΣFx = 0, ΣFy = 0 at each joint
Method of sections
ΣM = 0 about a cut point
Member force
positive = tension, negative = compression

Method

  1. Find the support reactions for the whole truss.
  2. Method of joints: start at a joint with at most two unknown member forces and use ΣFx = 0 and ΣFy = 0.
  3. Method of sections: cut through the member you need and take moments about a point where the other unknown members meet.
  4. Assume tension; a negative answer means compression.

Shear force & bending moment

Shear and moment
V = ΣF on one side, M = ΣF·d on one side
Bending stress
σ = M·y/I
Rectangle
I = bh³/12
Section modulus
W = I/ymax
Simply supported, uniform load
Mmax = wL²/8

Method

  1. Find the support reactions from equilibrium of the whole beam.
  2. Cut the beam at the section you need and keep one side.
  3. Shear force: sum of the vertical forces on that side. Bending moment: sum of their moments about the cut.
  4. For the maximum moment, find where the shear force is zero.

Beam deflection

Point load at midspan
δ = PL³/(48EI)
Uniform load, simply supported
δ = 5wL⁴/(384EI)
Cantilever, end load
δ = PL³/(3EI)
Cantilever, uniform load
δ = wL⁴/(8EI)
Superposition
δ = δ1 + δ2

Column buckling

Euler load
Pcr = π²EI/(KL)²
Effective length factor
K = 1 pinned–pinned, 0.5 fixed–fixed, 0.7 fixed–pinned, 2 fixed–free
Critical stress
σcr = Pcr/A
Slenderness
λ = KL/r, r = √(I/A)

Centroid & second moment of area

Centroid
ȳ = ΣAiyi/ΣAi
Rectangle
I = bh³/12
Parallel-axis theorem
I = Ic + A·d²
Composite section
I = Σ(Ic,i + Aidi²)

Effective stress in soil

Total stress
σ = Σγi·hi
Pore water pressure
u = γw·(z − zw)
Effective stress
σ′ = σ − u
Water
γw = 9.81 kN/m³

Consolidation settlement

Normally consolidated
S = Cc·H/(1 + e0)·log₁₀(σ′f/σ′0)
Final stress
σ′f = σ′0 + Δσ (at mid-depth of the layer)
Overconsolidated, σ′f ≤ σ′p
S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0)
Overconsolidated, σ′f > σ′p
S = H/(1 + e0)·[Cr·log₁₀(σ′p/σ′0) + Cc·log₁₀(σ′f/σ′p)]
Overconsolidation ratio
OCR = σ′p/σ′0
Time for consolidation
t = Tv·Hdr²/cv
Drainage path
Hdr = H/2 (double drainage), H (single drainage)
Time factors
U 50% → 0.197, 60% → 0.287, 70% → 0.403, 80% → 0.567, 90% → 0.848

Hydrostatic force

Pressure at depth
p = ρgh
Force on a vertical wall
F = ρg·hc·A
Centre of pressure
yp = yc + Ic/(ycA)
Rectangle
Ic = bH³/12

Pipe friction & head loss

Reynolds number
Re = V·D/ν = ρ·V·D/μ
Flow regime
laminar below Re ≈ 2000, turbulent above Re ≈ 4000
Mean velocity
V = Q/A, A = π·D²/4
Darcy–Weisbach
hf = f·(L/D)·V²/(2g)
Minor losses
hm = ΣK·V²/(2g)
Typical K values
entrance 0.5, exit 1.0, 90° bend ≈ 0.3
Pressure drop
Δp = ρ·g·hf
Two open reservoirs
Δz = (f·L/D + ΣK)·V²/(2g)
Free outlet
H = (1 + f·L/D + ΣK)·V²/(2g)

Open-channel flow (Manning)

Manning equation
V = (1/n)·R2/3·S1/2
Flow rate
Q = A·V
Hydraulic radius
R = A/P (P = wetted perimeter, free surface excluded)
Rectangle
A = b·y, P = b + 2y
Trapezoid (side slope z:1)
A = (b + z·y)·y, P = b + 2y·√(1 + z²)
Circular pipe, full or half full
R = D/4
Required slope
S = (n·Q/(A·R2/3))²

Pumps & pump power

Hydraulic power
Ph = ρ·g·Q·H = Q·Δp
Shaft power
Pshaft = Ph/ηpump
Electrical power
Pel = Pshaft/ηmotor
Pump head
H = Δz + Δp/(ρ·g) + hL
System losses
hL = (f·L/D + ΣK)·V²/(2g)

Time value of money

Future value
FV = PV·(1 + i)n
Present value
PV = FV/(1 + i)n
Several periods per year
i = r/m, N = m·n
Annuity, present value
PV = PMT·[1 − (1 + i)−n]/i
Annuity, future value
FV = PMT·[(1 + i)n − 1]/i

Method

  1. Draw a timeline with every cash flow and its timing.
  2. Match the rate to the period: a monthly rate for monthly payments.
  3. Use FV = PV·(1 + i)ⁿ for single amounts and the annuity formulas for equal payments.
  4. Check the sign and the order of magnitude of the answer.

NPV & IRR

Net present value
NPV = −C0 + Σ CFt/(1 + r)t
Equal cash flows
NPV = −C0 + CF·[1 − (1 + r)−n]/r
Internal rate of return
the r at which NPV = 0
Decision
accept when NPV > 0 (or IRR > required return)

Method

  1. List all cash flows with their year; the investment at year 0 is negative.
  2. Discount each cash flow: CFt/(1 + r)t.
  3. Add them up to get the NPV. Positive means the project earns more than r.
  4. For the IRR, find the rate that makes NPV zero by trial or interpolation.

Normal distribution

z-score
z = (x − μ)/σ
Below x
P(X < x) = Φ(z)
Above x
P(X > x) = 1 − Φ(z)
Between
Φ(z2) − Φ(z1)
Percentile
x = μ + z·σ

Method

  1. Convert the value to a z-score: z = (x − μ)/σ.
  2. Look up Φ(z), the area to the left of z.
  3. For the area to the right use 1 − Φ(z); for an interval subtract the two left areas.
  4. For a percentile, work backwards: find z for the area, then x = μ + z·σ.

2Practice problems

1.Beam support reactionsMedium
w = 12 kN/mP = 65 kNABMA​ = ?3 m3 m2 m

The cantilever beam is fixed to the wall at A. It carries a uniformly distributed load w from the wall to 6 m and a point load P at 3 m from the wall. Find the magnitude of the reaction moment MA at the wall.

L = 8 mP = 65 kN at 3 mw = 12 kN/m from 0 to 6 m
MA = kN·m
2.Beam support reactionsHard
P = 55 kN, 40°Q = 65 kNABα = ?2.5 m2 m1.5 m

The simply supported beam has a pin at A and a roller at B. A load P acts at 2.5 m from A, inclined at 40° to the horizontal, and a vertical load Q acts at 4.5 m from A. Find the angle α between the total reaction force at the pin A and the horizontal.

L = 6 mP = 55 kN at 2.5 m, θ = 40°Q = 65 kN at 4.5 m
α = °
3.Truss: method of jointsMedium
ABBCACACB30 kN8 m3 m4 m

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

span = 8 mheight = 4 mB is 3 m from Avertical load = 30 kN
FBC = kN
4.Truss: method of jointsHard
ABBCACACB20 kN10 kN5 m2 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 2 m from Avertical load = 20 kNhorizontal load = 10 kN ←
FAC = kN
5.Shear force & bending momentMedium
4 kN/m55 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.

55 kN @ 6 m4 kN/m, 0–12 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)
6.Shear force & bending momentHard
w = 4 kN/mP = 45 kNABsection3.5 m2.5 m

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

L = 6 mP = 45 kN at 3.5 mw = 4 kN/m from 0 to 6 mx = 3.5 m
Mx = kN·m
7.Beam deflectionMedium
w = 20 kN/mδL = 4 m

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

w = 20 kN/mL = 4 mE = 11 GPa (timber)I = 120 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 4 kN/mP = 13 kNδL = 2 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 = 13 kNw = 4 kN/mL = 2 mE = 11 GPa (timber)I = 23 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 1 md = 30 mmcross-section

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

L = 1 mE = 200 GPa (steel)d = 30 mm
Pcr = kN
10.Column bucklingHard
PL = 4 md = 60 mmcross-section

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

L = 4 mE = 70 GPa (aluminium)d = 60 mm
σcr = MPa
11.Centroid & second moment of areaMedium
2003030020xdimensions in mm

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

bf = 200 mmtf = 30 mmtw = 20 mmhw = 300 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
2601026020xM = 10 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 10 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 260 mmtf = 10 mmtw = 20 mmhw = 260 mmM = 10 kN·m
σtop = MPa
13.Effective stress in soilMedium
sandγd​ = 16.5 kN/m³γsat​ = 19 kN/m³12 mwater tableXz = 6 m

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

z = 6 mzw = 1 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 19 kN/m³
u = kPa
14.Effective stress in soilHard
sandγd​ = 17 kN/m³γsat​ = 18.5 kN/m³5 mclayγsat​ = 18.5 kN/m³5 mwater tableXz = 7.5 m

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

z = 7.5 mzw = 2 mγw = 9.81 kN/m³sand: γd = 17 kN/m³sand: γsat = 18.5 kN/m³clay: γsat = 18.5 kN/m³
u = kPa
15.Consolidation settlementMedium
Δσ = 15 kPasandclayCc​ = 0.2, Cr​ = 0.06e0​ = 1.05σ′0​ = 80 kPaσ′p​ = 150 kPa2 mwater table

A 2 m thick overconsolidated clay layer has Cc = 0.2, Cr = 0.06 and e₀ = 1.05. At its mid-depth the effective vertical stress is 80 kPa and the preconsolidation pressure is 150 kPa. A new building adds 15 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 2 mCc = 0.2Cr = 0.06e0 = 1.05σ′0 = 80 kPaσ′p = 150 kPaΔσ = 15 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 5 mcv​ = 5 m²/year5 mimpervious rockwater table

A clay layer 5 m thick has a coefficient of consolidation cv = 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 = 5 mcv = 5 m²/yearU = 60%Tv = 0.287single drainage
t = years
17.Hydrostatic forceMedium
gated = 2.5 mH = 1.5 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of water, with its top edge 2.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 2.5 mH = 1.5 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 3 mH = 1.5 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of oil, with its top edge 3 m below the surface. Find the depth ycp of the centre of pressure below the surface.

d = 3 mH = 1.5 mb = 2 mρ = 880 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
V = 1.9 m/sD = 150 mmL = 150 mf = 0.025

Water (ρ = 1000 kg/m³) flows at 1.9 m/s through a horizontal pipe, 150 m long, with an inside diameter of 150 mm. Use the Darcy friction factor f = 0.025 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 1.9 m/sL = 150 mD = 150 mmf = 0.025ρ = 1000 kg/m³
Δp = kPa
20.Pipe friction & head lossHard
K = 0.2Δz = ?L = 300 m, D = 250 mm, f = 0.0183× bend (K = 0.3)

Two open reservoirs are joined by a pipe 300 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.018. The minor losses are a square-edged entrance (K = 0.5), 3 bends (K = 0.3 each), a valve (K = 0.2) 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 50 L/s?

Q = 50 L/sL = 300 mD = 250 mmf = 0.018Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 0.2Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
b = 3 my = 0.6 m2 : 1n = 0.015, S = 0.005

A trapezoidal brickwork channel has a bottom width of 3 m and side slopes of 2:1 (horizontal:vertical). Water flows uniformly 0.6 m deep. Manning n = 0.015 and the bed slope is S = 0.005. Find the flow rate Q in m³/s.

b = 3 my = 0.6 mz = 2n = 0.015S = 0.005
Q = m³/s
22.Open-channel flow (Manning)Hard
D = 200 mmn = 0.013, V = 0.6 m/s

A concrete sewer with an inside diameter of 200 mm (Manning n = 0.013) must reach a self-cleansing velocity of 0.6 m/s when flowing just full. Find the minimum slope S (in m/m).

D = 200 mmn = 0.013V = 0.6 m/s
S = m/m
23.Pumps & pump powerMedium
PQ = 25 L/sH = 74 m

A pump with an efficiency of 82% delivers 25 L/s of water (ρ = 1000 kg/m³) against a head of 74 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 25 L/sH = 74 mη = 82%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 120 L/sΔz = 16 mL = 400 m, D = 250 mm, f = 0.015, ΣK = 5

A pump moves 120 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 16 m higher. The pipe is 400 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 = 5 (entrance and exit included). Use g = 9.81 m/s². Find the head H the pump must add.

Q = 120 L/sΔz = 16 mL = 400 mD = 250 mmf = 0.015ΣK = 5
H = m
25.Time value of moneyMedium
years0123…10€20 000FV = ?

You invest €20 000 at a nominal rate of 3.6% per year, compounded monthly. Find the value FV of the investment after 10 years.

PV = €20 0003.6% / 12n = 10
FV = €
26.Time value of moneyHard
months0123…N = ?€25 000€325€325€325€3252.4% / 12

You borrow €25 000 at 2.4% per year, compounded monthly, and repay €325 at the end of every month. How many months does it take until the loan is repaid (the last payment may be smaller)? Give the number of payments N.

P = €25 000A = €3252.4% / 12
N = payments
27.NPV & IRRMedium
years0123456−40 0008 50018 00010 50012 50012 00013 000

A project costs €40 000 today and returns €8 500, €18 000, €10 500, €12 500, €12 000, €13 000 at the end of years 1 to 6. The cost of capital is 5%. Assume cash flows arrive evenly through each year. Find the discounted payback period DPB in years.

r = 5%CF0 = −40 000CF1 = 8 500CF2 = 18 000CF3 = 10 500CF4 = 12 500CF5 = 12 000CF6 = 13 000
DPB = years
28.NPV & IRRHard
years012345−40 0009 5009 5009 5009 5009 500

An investment of €40 000 returns €9 500 at the end of each year for 5 years. Find its internal rate of return IRR in percent.

C0 = €40 000CF = €9 500n = 5
IRR = %
29.Normal distributionMedium
750 g754.9 gX + Y?

X is normal with mean 250 g and standard deviation 4 g; Y is independent and normal with mean 500 g and standard deviation 9 g. Find the probability P that X + Y is more than 754.9 g. Round z to two decimals.

μX = 250, σX = 4μY = 500, σY = 9X + Y > 754.9 g
P =
30.Normal distributionHard
μ = 250x = ?5%

The bag weights are normally distributed with mean 250 g and standard deviation 5 g. Find the value x below which 5% of them lie (the 5th percentile).

μ = 250σ = 5P = 5%
x = g

3Solutions

1.Beam support reactions

Answer: MA = 411 kN·m

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

Resultant of the distributed load

W = 12·6 = 72 kN, x̄ = 3 m

Moment about the wall

MA = P·a + W·x̄ = 65·3 + 72·3 = 411 kN·m

Answer

MA = 411 kN·m
2.Beam support reactions

Answer: α = 41.19 °

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

Components of P

Pv = 55·sin 40° = 35.35 kN
Ph = 55·cos 40° = 42.13 kN

Reactions

ΣMA = 0: RB·6 = 35.35·2.5 + 65·4.5 → RB = 63.48 kN
Ay = 35.35 + 65 − 63.48 = 36.87 kN
Ax = Ph = 42.13 kN

Direction at A

α = atan(Ay/Ax) = atan(36.87/42.13) = 41.19°

Answer

α = 41.19°
3.Truss: method of joints

Answer: FBC = −18.01 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.

ABBCACACB30 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·8 = 30·3 → Cy = 11.25 kN
ΣFy = 0: Ay = 30 − 11.25 = 18.75 kN

Joint C

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

sin γ = 4/6.403 = 0.6247, cos γ = 5/6.403 = 0.7809
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −11.25/0.6247 = −18.01 kN

Answer

FBC = −18.01 kN (compression)
4.Truss: method of joints

Answer: FAC = 6 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.

ABBCACACB20 kN10 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·5 = 20·2 − 10·2 → Cy = 4 kN
ΣFy = 0: Ay = 20 − 4 = 16 kN
ΣFx = 0: Ax = 10 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 = −4/0.5547 = −7.211 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−7.211)·0.8321 = 6 kN

Answer

FAC = 6 kN (tension)
5.Shear force & bending moment

Answer: D (x = 6 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 = 51.5 kN, R2 = 51.5 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 = 95, MC = 174, MD = 237 kN·m, ME = 174, MF = 95, MG = 0

Answer

Mark D: MD = 237 kN·m
6.Shear force & bending moment

Answer: Mx = 83.13 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 = 45·3.5 + 4·6·3
RB = 229.5/6 = 38.25 kN
ΣFy = 0: RA = 69 − 38.25 = 30.75 kN
w = 4 kN/mP = 45 kNABRA​ = 30.75RB​ = 38.25section3.5 m2.5 m

Cut at x = 3.5 m and keep the left part

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

M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 30.75·3.5 − 4·3.5·1.75 = 83.13 kN·m

Answer

Mx = 83.13 kN·m
7.Beam deflection

Answer: δmax = 50.51 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 = 4000 mm
EI = 1.32 × 10¹² N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·20·4000⁴/(384·1.32 × 10¹²) = 50.51 mm

Answer

δmax = 50.51 mm
8.Beam deflection

Answer: δmax = 11.86 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 = 13000 N, w = 4 N/mm, L = 2000 mm, EI = 2.53 × 10¹¹ N·mm²

Each load on its own

δP = PL³/(48EI) = 13000·2000³/(48·2.53 × 10¹¹) = 8.564 mm
δw = 5wL⁴/(384EI) = 5·4·2000⁴/(384·2.53 × 10¹¹) = 3.294 mm

Add them

δmax = 8.564 + 3.294 = 11.86 mm

Answer

δmax = 11.86 mm
9.Column buckling

Answer: Pcr = 160.2 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·30⁴/64 = 39761 mm⁴

Effective length

KL = 0.7·1000 = 700 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·39761/700² = 160173 N = 160.2 kN

Answer

Pcr = 160.2 kN
10.Column buckling

Answer: σcr = 38.86 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·60⁴/64 = 636173 mm⁴

Radius of gyration and slenderness

A = 2827 mm²
r = √(I/A) = √(636173/2827) = 15 mm
KL = 0.5·4000 = 2000 mm
KL/r = 2000/15 = 133.3

Critical stress

σcr = π²E/(KL/r)² = π²·70000/133.3² = 38.86 MPa

Answer

σcr = 38.86 MPa
11.Centroid & second moment of area

Answer: Ix = 127.1 × 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 = 200·30 = 6000 mm², yf = 300 + 30/2 = 315 mm
web: Aw = 20·300 = 6000 mm², yw = 300/2 = 150 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (6000·315 + 6000·150)/12000 = 232.5 mm

Parallel-axis theorem

flange: 200·30³/12 + 6000·(315 − 232.5)² = 4.129 × 10⁷ mm⁴
web: 20·300³/12 + 6000·(150 − 232.5)² = 8.584 × 10⁷ mm⁴
Ix = 4.129 × 10⁷ + 8.584 × 10⁷ = 1.271 × 10⁸ mm⁴ = 127.1 × 10⁶ mm⁴

Answer

Ix = 127.1 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 15.6 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 = 260·10 = 2600 mm², yf = 260 + 10/2 = 265 mm
web: Aw = 20·260 = 5200 mm², yw = 260/2 = 130 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2600·265 + 5200·130)/7800 = 175 mm

Parallel-axis theorem

flange: 260·10³/12 + 2600·(265 − 175)² = 2.108 × 10⁷ mm⁴
web: 20·260³/12 + 5200·(130 − 175)² = 3.982 × 10⁷ mm⁴
Ix = 2.108 × 10⁷ + 3.982 × 10⁷ = 6.09 × 10⁷ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 270 − 175 = 95 mm
σ = M·y/I = 1 × 10⁷·95/6.09 × 10⁷ = 15.6 MPa

Answer

σtop = 15.6 MPa
13.Effective stress in soil

Answer: u = 49.05 kPa

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

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·5 = 49.05 kPa

Answer

u = 49.05 kPa
14.Effective stress in soil

Answer: u = 53.96 kPa

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

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·5.5 = 53.96 kPa

Answer

u = 53.96 kPa
15.Consolidation settlement

Answer: S = 4.369 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 = 80 + 15 = 95 kPa ≤ 150 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.06·2/(1 + 1.05)·log₁₀(95/80) = 4.369 mm

Answer

S = 4.369 mm
16.Consolidation settlement

Answer: t = 1.435 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 = 5 m

Time

t = Tv·Hdr²/cv = 0.287·5²/5 = 1.435 years

Answer

t = 1.435 years
17.Hydrostatic force

Answer: F = 143.5 kN

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

Centroid depth and area

yc = d + H/2 = 2.5 + 1.5/2 = 3.25 m
A = H·b = 1.5·3 = 4.5 m²
gated = 2.5 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3.25·4.5 = 143.5 kN

Answer

F = 143.5 kN
18.Hydrostatic force

Answer: ycp = 3.8 m

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

Centroid depth and area

yc = d + H/2 = 3 + 1.5/2 = 3.75 m
A = H·b = 1.5·2 = 3 m²
gated = 3 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 880·9.81·3.75·3 = 97.12 kN

Centre of pressure

Pressure grows with depth, so the resultant acts below the centroid.

Ic = b·H³/12 = 2·1.5³/12 = 0.5625 m⁴
ycp = yc + Ic/(yc·A) = 3.75 + 0.5625/(3.75·3) = 3.8 m

Answer

ycp = 3.8 m
19.Pipe friction & head loss

Answer: Δp = 45.12 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) = 0.025·(150/0.15)·1.9²/(2·9.81) = 4.6 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 = 1000·9.81·4.6 = 45125 Pa = 45.12 kPa

Answer

Δp = 45.12 kPa
20.Pipe friction & head loss

Answer: Δz = 1.28 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 = 0.018·300/0.25 = 21.6
ΣK = 0.5 + 3·0.3 + 0.2 + 1.0 = 2.6

Total head loss

hf = 21.6·0.05288 = 1.142 m
hm = 2.6·0.05288 = 0.1375 m
Δz = hf + hm = 1.28 m

Answer

Δz = 1.28 m
21.Open-channel flow (Manning)

Answer: Q = 6.908 m³/s

Manning’s equation (SI): for uniform flow in an open channel V = (1/n)·R2/3·S1/2 and Q = A·V, with n the roughness coefficient, S the bed slope (m/m) and R = A/P the hydraulic radius: flow area divided by wetted perimeter. Only the boundary in contact with the water counts in P, not the free surface. Rectangle: A = b·y, P = b + 2y. Trapezoid with side slopes z:1 (horizontal:vertical): A = (b + z·y)·y, P = b + 2y·√(1 + z²). A circular pipe flowing full or half full has R = D/4.

Geometry

A = (b + z·y)·y = (3 + 2·0.6)·0.6 = 2.52 m²
P = b + 2y·√(1 + z²) = 3 + 2·0.6·√(1 + 2²) = 5.683 m
R = A/P = 0.4434 m

Velocity

V = (1/0.015)·0.44342/3·0.0051/2 = 2.741 m/s

Flow rate

Q = A·V = 2.52·2.741 = 6.908 m³/s

Answer

Q = 6.908 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.003303 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 = 0.2/4 = 0.05 m

Solve Manning for S

S = (n·V/R2/3)² = (0.013·0.6/0.1357)² = 0.003303

Answer

S = 0.003303

That is a fall of 3.303 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 22.13 kW

Pump power: the power given to the water is the hydraulic power Ph = ρ·g·Q·H = Q·Δp. The shaft must deliver more because the pump loses some: Pshaft = Ph/ηpump, and the motor draws Pel = Pshaft/ηmotor. The pump head H follows from the energy equation: static lift + pressure head + all friction and minor losses.

Hydraulic power

Ph = ρ·g·Q·H = 1000·9.81·0.025·74 = 18.15 kW

Shaft power

Pshaft = Ph/η = 18.15/0.82 = 22.13 kW

Answer

Pshaft = 22.13 kW
24.Pumps & pump power

Answer: H = 24.83 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 = 0.12/0.04909 = 2.445 m/s
V²/(2g) = 0.3046 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (24 + 5)·0.3046 = 8.833 m

Pump head

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

H = Δz + hL = 16 + 8.833 = 24.83 m

Answer

H = 24.83 m
25.Time value of money

Answer: FV = 28651 €

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

Rate and number of periods

i = r/m = 0.036000000000000004/12 = 0.003
N = m·n = 12·10 = 120

Future value

FV = 20 000·(1 + 0.003)120 = 20 000·1.433 = €28 651.14

Answer

FV = €28 651.14
26.Time value of money

Answer: N = 84 payments

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.

Rearrange the annuity formula

i = 0.002
(1 + i)−N = 1 − 25 000·0.002/325 = 0.8462

Solve with logarithms

N = −ln(0.8462)/ln(1.002) = 83.61

Round up to whole payments

83 full payments leave a small balance, which the last, smaller payment clears.

N = 84

Answer

N = 84 payments
27.NPV & IRR

Answer: DPB = 3.633 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: 8 500/1.05 = 8 095.24 → Σ = 8 095.24
year 2: 18 000/1.103 = 16 326.53 → Σ = 24 421.77
year 3: 10 500/1.158 = 9 070.29 → Σ = 33 492.06
year 4: 12 500/1.216 = 10 283.78 → Σ = 43 775.84

Fraction of the last year

DPB = 3 + 6 507.94/10 283.78 = 3.633

Answer

DPB = 3.633 years

The discounted payback is always longer than the simple payback (3.24 years).

28.NPV & IRR

Answer: IRR = 6.016 %

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.

Required annuity factor

(1 − (1 + i)−5)/i = 40 000/9 500 = 4.211

Solve for the rate

The annuity factor falls as the rate rises; bracket the rate and narrow down.

i = 6%: 4.212
i = 7%: 4.1
IRR = 6.016%

Answer

IRR = 6.016%
29.Normal distribution

Answer: P = 0.3085

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 = 750 g, σ = √(4² + 9²) = 9.849 g

Standardise

z = (754.9 − 750)/9.849 = 0.5

Upper tail

P = 1 − Φ(0.5) = 1 − 0.6915 = 0.3085

Answer

P = 0.3085
30.Normal distribution

Answer: x = 241.8 g

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) = 0.05 → z = −1.645

Back to x

x = 250 + −1.645·5 = 241.78 g

Answer

x = 241.78 g

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