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
P1​ = 45 kNP2​ = 40 kNABRA​RB​ = ?1 m6 m1 m

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

L = 8 mP1 = 45 kN at 1 mP2 = 40 kN at 7 m
RB = kN
2.Beam support reactionsHard
w = 5 kN/mP = 10 kNABRA​ = ?RB​2 m1 m1 m

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

L = 4 mP = 10 kN at 3 mw = 5 kN/m from 0 to 2 m
RA = kN
3.Truss: method of jointsMedium
ABCDEFGH10 kN30 kN15 kN4 × 4 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 ↓C: 30 kN ↓D: 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 FC
  13. 13member HC
4.Truss: method of jointsHard
ABBCACACB40 kN20 kN4 m1 m4 m

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

span = 4 mheight = 4 mB is 1 m from Avertical load = 40 kNhorizontal load = 20 kN ←
FBC = kN
5.Shear force & bending momentMedium
12 kN/m10 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 @ 10 m12 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 = 3 kN/mP = 30 kNABsection1 m3 m6 m

Find the bending moment Mx at the section x = 4 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 10 mP = 30 kN at 1 mw = 3 kN/m from 0 to 10 mx = 4 m
Mx = kN·m
7.Beam deflectionMedium
w = 5 kN/mδL = 5 m

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

w = 5 kN/mL = 5 mE = 70 GPa (aluminium)I = 57 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 12 kN/mP = 8 kNδL = 6 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 = 8 kNw = 12 kN/mL = 6 mE = 200 GPa (steel)I = 57 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 1.5 md = 25 mmcross-section

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

L = 1.5 mE = 200 GPa (steel)d = 25 mm
Pcr = kN
10.Column bucklingHard
PL = 2.5 md = 50 mmcross-section

A column of length L made of steel is fixed at the base and free at the top. Find its slenderness and the critical buckling stress σcr from Euler’s formula.

L = 2.5 mE = 200 GPa (steel)d = 50 mm
σcr = MPa
11.Centroid & second moment of areaMedium
150 mm240 mm156 mmØ40xIx​ = ?

A 150 mm × 240 mm plate has a circular hole of diameter 40 mm on its vertical centre line, with its centre 156 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 150 mmh = 240 mmd = 40 mmhole centre: y = 156 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
140302408xM = 15 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 15 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 140 mmtf = 30 mmtw = 8 mmhw = 240 mmM = 15 kN·m
σtop = MPa
13.Effective stress in soilMedium
sandγd​ = 16.5 kN/m³γsat​ = 19.5 kN/m³9 mwater tableXz = 6 m

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

z = 6 mzw = 3 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 19.5 kN/m³
u = kPa
14.Effective stress in soilHard
sandγd​ = 17 kN/m³γsat​ = 20 kN/m³5 mclayγsat​ = 18.5 kN/m³5 mwater tableXz = 7.5 m

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

z = 7.5 mzw = 2 mγw = 9.81 kN/m³sand: γd = 17 kN/m³sand: γsat = 20 kN/m³clay: γsat = 18.5 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 110 kPasandclayCc​ = 0.45, Cr​ = 0.05e0​ = 0.9σ′0​ = 70 kPaσ′p​ = 160 kPa7 mwater table

A 7 m thick overconsolidated clay layer has Cc = 0.45, Cr = 0.05 and e₀ = 0.9. At its mid-depth the effective vertical stress is 70 kPa and the preconsolidation pressure is 160 kPa. A new building adds 110 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 7 mCc = 0.45Cr = 0.05e0 = 0.9σ′0 = 70 kPaσ′p = 160 kPaΔσ = 110 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 5.5 m5.5 mimpervious rockwater table

In a laboratory oedometer test, a clay specimen 20 mm thick, drained at the top and bottom, reaches 50% consolidation in 8 min. In the field the same clay forms a layer 5.5 m thick. It lies on impervious rock, with sand above it, so water drains out only at the top. How many days t does the field layer take to reach 50% consolidation?

hlab = 20 mmtlab = 8 minH = 5.5 mfield: single drainage
t = days
17.Hydrostatic forceMedium
gated = 1 mH = 1.5 m

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

d = 1 mH = 1.5 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 2.5 mH = 1 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of water, with its top edge 2.5 m below the surface. Find the depth ycp of the centre of pressure below the surface.

d = 2.5 mH = 1 mb = 2 mρ = 1000 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
V = 2.8 m/sD = 250 mmL = 300 mf = 0.015

Water (ρ = 1000 kg/m³) flows at 2.8 m/s through a horizontal pipe, 300 m long, with an inside diameter of 250 mm. Use the Darcy friction factor f = 0.015 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 2.8 m/sL = 300 mD = 250 mmf = 0.015ρ = 1000 kg/m³
Δp = kPa
20.Pipe friction & head lossHard
K = 5Δz = ?L = 150 m, D = 150 mm, f = 0.0252× bend (K = 0.3)

Two open reservoirs are joined by a pipe 150 m long with an inside diameter of 150 mm and a Darcy friction factor f = 0.025. The minor losses are a square-edged entrance (K = 0.5), 2 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 30 L/s?

Q = 30 L/sL = 150 mD = 150 mmf = 0.025Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 5Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
D = 900 mmn = 0.013, S = 0.005

A concrete storm sewer with an inside diameter of 900 mm flows just full (as an open channel, not under pressure). Manning n = 0.013 and the slope is S = 0.005. Find the flow rate Q in m³/s.

D = 900 mmn = 0.013S = 0.005
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 5 my = 1.7 mn = 0.03, Q = 6.4 m³/s

A rectangular grass-lined earth channel 5 m wide must carry 6.4 m³/s in uniform flow at a depth of 1.7 m. Manning n = 0.03. Find the required bed slope S (in m/m).

Q = 6.4 m³/sb = 5 my = 1.7 mn = 0.03
S = m/m
23.Pumps & pump powerMedium
PQ = 25 L/sH = 34 m

A pump delivers 25 L/s of water (ρ = 1000 kg/m³) against a head of 34 m. The pump efficiency is 78% and the electric motor driving it has an efficiency of 90%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 25 L/sH = 34 mηpump = 78%ηmotor = 90%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
PQ = 50 L/sΔz = 5 mL = 300 m, D = 250 mm, f = 0.025, ΣK = 8

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 300 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.025; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². Find the head H the pump must add.

Q = 50 L/sΔz = 5 mL = 300 mD = 250 mmf = 0.025ΣK = 8
H = m
25.Time value of moneyMedium
years012PV = ?€15 000

You need €15 000 in 2 years. An account pays 3.6% per year, compounded monthly. How much must you deposit today? Find the present value PV.

FV = €15 0003.6% / 12n = 2
PV = €
26.Time value of moneyHard
months0123…312€250€250€250FV = ?

You save €250 at the end of every month for 26 years. The account pays 2.4% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €2502.4% / 12N = 312
FV = €
27.NPV & IRRMedium
years01234−20 0006 0004 0008 0006 000

An investment of €20 000 gives these cash flows at the end of years 1 to 4: €6 000, €4 000, €8 000, €6 000. The cost of capital is 10%. Find the net present value NPV.

r = 10%CF0 = −20 000CF1 = 6 000CF2 = 4 000CF3 = 8 000CF4 = 6 000
NPV = €
28.NPV & IRRHard
years0123−50 00034 00021 50028 000

A project costs €50 000 and returns €34 000, €21 500, €28 000 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −50 000CF1 = 34 000CF2 = 21 500CF3 = 28 000
IRR = %
29.Normal distributionMedium
30.538.3P = ?

The delivery times are normally distributed with mean 32 min and standard deviation 6 min. What fraction lies between 30.5 and 38.3 min? Give P as a decimal.

μ = 32σ = 6x1 = 30.5x2 = 38.3
P =
30.Normal distributionHard
10 g0X − Y?

The mass X of a product from line 1 and Y from line 2 are independent and normal: X has mean 500 g and standard deviation 8 g, Y has mean 490 g and standard deviation 6 g. Find the probability P that X is greater than Y. Round z to two decimals.

μX = 500 g, σX = 8 gμY = 490 g, σY = 6 g
P =

3Solutions

1.Beam support reactions

Answer: RB = 40.63 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​ = 45 kNP2​ = 40 kNABRA​RB​1 m6 m1 m

Free-body diagram

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

Equilibrium

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

ΣMA = 0: RB·8 = 45·1 + 40·7
RB = 325/8 = 40.63 kN
ΣFy = 0: RA = 85 − 40.63 = 44.38 kN

Answer

RB = 40.63 kN
2.Beam support reactions

Answer: RA = 10 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 = 10 kNABRA​RB​2 m1 m1 m

Free-body diagram

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

Equilibrium

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

UDL resultant: W = w·ℓ = 5·2 = 10 kN, acting at x̄ = 1 m
ΣMA = 0: RB·4 = 10·3 + 5·2·1
RB = 40/4 = 10 kN
ΣFy = 0: RA = 20 − 10 = 10 kN

Answer

RA = 10 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 G

FG and GH 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: 35 kN (T), BC: 35 kN (T), CD: 38.33 kN (T), DE: 38.33 kN (T), FG: 56.67 kN (C), GH: 56.67 kN (C), AF: 43.75 kN (C), HE: 47.92 kN (C), BF: 10 kN (T), CG: 0, DH: 15 kN (T), FC: 27.08 kN (T), HC: 22.92 kN (T)

Answer

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

Answer: FBC = 12.5 kN

Method of joints: every pin of a truss is in equilibrium, so ΣFx = 0 and ΣFy = 0 at each joint. Start at a joint with at most two unknown member forces. A negative result means the member is in compression.

ABBCACACB40 kN20 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·4 = 40·1 − 20·4 → Cy = −10 kN
ΣFy = 0: Ay = 40 − −10 = 50 kN
ΣFx = 0: Ax = 20 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 = 4/5 = 0.8, cos γ = 3/5 = 0.6
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −−10/0.8 = 12.5 kN

Answer

FBC = 12.5 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 = 73.67 kN, R2 = 80.33 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 = 123.3, MC = 198.7, MD = 226 kN·m, ME = 205.3, MF = 136.7, MG = 0

Answer

Mark D: MD = 226 kN·m
6.Shear force & bending moment

Answer: Mx = 54 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 = 3·10 = 30 kN, acting at x̄ = 5 m
ΣMA = 0: RB·10 = 30·1 + 3·10·5
RB = 180/10 = 18 kN
ΣFy = 0: RA = 60 − 18 = 42 kN
w = 3 kN/mP = 30 kNABRA​ = 42RB​ = 18section1 m3 m6 m

Cut at x = 4 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 = 42·4 − 30·(4 − 1) − 3·4·2 = 54 kN·m

Answer

Mx = 54 kN·m
7.Beam deflection

Answer: δmax = 10.2 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 = 5 N/mm, L = 5000 mm
EI = 3.99 × 10¹² N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·5·5000⁴/(384·3.99 × 10¹²) = 10.2 mm

Answer

δmax = 10.2 mm
8.Beam deflection

Answer: δmax = 20.92 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 = 8000 N, w = 12 N/mm, L = 6000 mm, EI = 1.14 × 10¹³ N·mm²

Each load on its own

δP = PL³/(48EI) = 8000·6000³/(48·1.14 × 10¹³) = 3.158 mm
δw = 5wL⁴/(384EI) = 5·12·6000⁴/(384·1.14 × 10¹³) = 17.76 mm

Add them

δmax = 3.158 + 17.76 = 20.92 mm

Answer

δmax = 20.92 mm
9.Column buckling

Answer: Pcr = 16.82 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·25⁴/64 = 19175 mm⁴

Effective length

KL = 1·1500 = 1500 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·19175/1500² = 16822 N = 16.82 kN

Answer

Pcr = 16.82 kN
10.Column buckling

Answer: σcr = 12.34 MPa

Euler buckling: a slender column becomes unstable at Pcr = π²EI/(KL)², where KL is the effective length: K = 1 for pinned–pinned, 2 for fixed–free, 0.7 for fixed–pinned and 0.5 for fixed–fixed. It buckles about the axis with the smallest I. The formula holds for slender columns, whose critical stress stays below the yield stress.

Smallest second moment of area

A round section has the same I about every axis.

I = πd⁴/64 = π·50⁴/64 = 306796 mm⁴

Radius of gyration and slenderness

A = 1963 mm²
r = √(I/A) = √(306796/1963) = 12.5 mm
KL = 2·2500 = 5000 mm
KL/r = 5000/12.5 = 400

Critical stress

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

Answer

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

Answer: Ix = 171 × 10⁶ mm⁴

Sections with holes: treat a hole as a negative area. The centroid is ȳ = (A₁y₁ − A₂y₂)/(A₁ − A₂), with A₁, y₁ for the full plate and A₂, y₂ for the hole. For the second moment of area about the centroidal axis, use the parallel-axis theorem for each part and subtract the hole: I = (Ic1 + A₁d₁²) − (Ic2 + A₂d₂²), where d is the distance from each part's own centroid to the axis through ȳ. A rectangle has Ic = bh³/12 and a circle Ic = πd⁴/64.

Centroid

ȳ = (36000·120 − 1257·156)/(36000 − 1257) = 118.7 mm

Full plate about ȳ

150·240³/12 + 36000·1.302² = 172.9 × 10⁶ mm⁴

Hole about ȳ

π·40⁴/64 + 1257·37.3² = 1.874 × 10⁶ mm⁴

Subtract

Ix = 171 × 10⁶ mm⁴

Answer

Ix = 171 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 25.65 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 = 140·30 = 4200 mm², yf = 240 + 30/2 = 255 mm
web: Aw = 8·240 = 1920 mm², yw = 240/2 = 120 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (4200·255 + 1920·120)/6120 = 212.6 mm

Parallel-axis theorem

flange: 140·30³/12 + 4200·(255 − 212.6)² = 7.849 × 10⁶ mm⁴
web: 8·240³/12 + 1920·(120 − 212.6)² = 2.57 × 10⁷ mm⁴
Ix = 7.849 × 10⁶ + 2.57 × 10⁷ = 3.355 × 10⁷ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 270 − 212.6 = 57.35 mm
σ = M·y/I = 1.5 × 10⁷·57.35/3.355 × 10⁷ = 25.65 MPa

Answer

σtop = 25.65 MPa
13.Effective stress in soil

Answer: u = 29.43 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) = 9.81·3 = 29.43 kPa

Answer

u = 29.43 kPa
14.Effective stress in soil

Answer: σ′ = 86.29 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·3 + γsat,clay·2.5
σ = 17·2 + 20·3 + 18.5·2.5 = 140.3 kPa

Pore water pressure

Water pressure grows with depth below the water table.

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

Effective stress

σ′ = σ − u = 140.3 − 53.96 = 86.29 kPa

Answer

σ′ = 86.29 kPa
15.Consolidation settlement

Answer: S = 150.9 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 = 70 + 110 = 180 kPa > 160 kPa

Settlement

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

S = 0.05·7/(1 + 0.9)·log₁₀(160/70) + 0.45·7/(1 + 0.9)·log₁₀(180/160)
S = 66.14 + 84.81 = 150.9 mm

Answer

S = 150.9 mm
16.Consolidation settlement

Answer: t = 1681 days

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 paths

Hdr,lab = 20/2 = 10 mm = 0.01 m
Hdr,field = 5.5 m

Scale the time

t = Tv·Hdr²/cv with the same T_v and cv in the lab and the field.

tfield = 8·(5.5/0.01)² = 2.42 × 10⁶ min
tfield = 2.42 × 10⁶/1440 = 1681 days

Answer

t = 1681 days
17.Hydrostatic force

Answer: F = 25.75 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 + 1.5/2 = 1.75 m
A = H·b = 1.5·1 = 1.5 m²
gated = 1 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·1.75·1.5 = 25.75 kN

Answer

F = 25.75 kN
18.Hydrostatic force

Answer: ycp = 3.028 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 = 2.5 + 1/2 = 3 m
A = H·b = 1·2 = 2 m²
gated = 2.5 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3·2 = 58.86 kN

Centre of pressure

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

Ic = b·H³/12 = 2·1³/12 = 0.1667 m⁴
ycp = yc + Ic/(yc·A) = 3 + 0.1667/(3·2) = 3.028 m

Answer

ycp = 3.028 m
19.Pipe friction & head loss

Answer: Δp = 70.56 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) = 0.015·(300/0.25)·2.8²/(2·9.81) = 7.193 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 = 1000·9.81·7.193 = 70560 Pa = 70.56 kPa

Answer

Δp = 70.56 kPa
20.Pipe friction & head loss

Answer: Δz = 4.715 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 = 0.03/0.01767 = 1.698 m/s
V²/(2g) = 0.1469 m

Loss coefficients

f·L/D = 0.025·150/0.15 = 25
ΣK = 0.5 + 2·0.3 + 5 + 1.0 = 7.1

Total head loss

hf = 25·0.1469 = 3.672 m
hm = 7.1·0.1469 = 1.043 m
Δz = hf + hm = 4.715 m

Answer

Δz = 4.715 m
21.Open-channel flow (Manning)

Answer: Q = 1.28 m³/s

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

Geometry

A = 0.6362 m², R = D/4 = 0.225 m

Velocity

V = (1/0.013)·0.2252/3·0.0051/2 = 2.012 m/s

Flow rate

Q = A·V = 0.6362·2.012 = 1.28 m³/s

Answer

Q = 1.28 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.0005022 m/m

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

Geometry

A = b·y = 5·1.7 = 8.5 m²
P = b + 2y = 5 + 2·1.7 = 8.4 m
R = A/P = 1.012 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.03·6.4/(8.5·1.008) = 0.02241
S = 0.02241² = 0.0005022

Answer

S = 0.0005022

That is a fall of 0.5022 m per kilometre.

23.Pumps & pump power

Answer: Pel = 11.88 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 = 1000·9.81·0.025·34 = 8.338 kW

Shaft power

Pshaft = 8.338/0.78 = 10.69 kW

Electrical power

Pel = 10.69/0.9 = 11.88 kW

Answer

Pel = 11.88 kW
24.Pumps & pump power

Answer: H = 7.009 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 = 0.05/0.04909 = 1.019 m/s
V²/(2g) = 0.05288 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (30 + 8)·0.05288 = 2.009 m

Pump head

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

H = Δz + hL = 5 + 2.009 = 7.009 m

Answer

H = 7.009 m
25.Time value of money

Answer: PV = 13959 €

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

Rate and number of periods

i = 0.036000000000000004/12 = 0.003
N = 12·2 = 24

Present value

PV = FV/(1 + i)N = 15 000/1.075 = €13 959.47

Answer

PV = €13 959.47
26.Time value of money

Answer: FV = 108152 €

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

Monthly rate and number of deposits

i = 0.024/12 = 0.002
N = 12·26 = 312

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 250·(1.865 − 1)/0.002 = €108 151.99

Answer

FV = €108 151.99

You paid in €78 000 yourself; the rest is interest.

27.NPV & IRR

Answer: NPV = −1131 €

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 = −20 000
CF1/(1 + 0.1)1 = 6 000/1.1 = 5 454.55
CF2/(1 + 0.1)2 = 4 000/1.21 = 3 305.79
CF3/(1 + 0.1)3 = 8 000/1.331 = 6 010.52
CF4/(1 + 0.1)4 = 6 000/1.464 = 4 098.08

Add them up

NPV = €−1 131.07

Answer

NPV = €−1 131.07

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

28.NPV & IRR

Answer: IRR = 32.41 %

Net present value: discount every cash flow back to today with the required rate of return r, then add them up: NPV = Σ CFₜ/(1 + r)ᵗ. A project with NPV > 0 earns more than r and adds value. The internal rate of return (IRR) is the rate at which NPV = 0.

Bracket the IRR

NPV falls as the rate rises, so the IRR lies between a rate with positive NPV and one with negative NPV.

NPV(30%) = 1 620.39
NPV(35%) = −1 637.45

Narrow down

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

IRR ≈ 30 + 5·1 620.39/(1 620.39 − (−1 637.45)) = 32.49%
exact: NPV(32.41%) = 0 → IRR = 32.41%

Answer

IRR = 32.41%
29.Normal distribution

Answer: P = 0.4518

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 = (30.5 − 32)/6 = −0.25
z₂ = (38.3 − 32)/6 = 1.05

Area between

P = Φ(1.05) − Φ(−0.25) = 0.8531 − 0.4013 = 0.4518

Answer

P = 0.4518
30.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 difference

μ = 500 − 490 = 10 g, σ = 10 g

Standardise

z = (0 − 10)/10 = −1

Probability

P = 1 − Φ(−1) = 0.8413

Answer

P = 0.8413

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