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​ = 55 kNP2​ = 15 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 mP1 = 55 kN at 2 mP2 = 15 kN at 3 m
RA = kN
2.Beam support reactionsHard
w = 8 kN/mP = 30 kNABRA​ = ?RB​5 m1 m2 m

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

L = 8 mP = 30 kN at 5 mw = 8 kN/m from 5 to 6 m
RA = kN
3.Truss: method of jointsMedium
ABBCACACB55 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 = 55 kN
FBC = kN
4.Truss: method of jointsHard
ABBCACACB15 kN30 kN6 m1 m3 m

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

span = 6 mheight = 3 mB is 1 m from Avertical load = 15 kNhorizontal load = 30 kN →
FAC = kN
5.Shear force & bending momentMedium
10 kN25 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 m25 kN @ 6 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 = 45 kNABsection2.5 m0.5 m1 m

Find the bending moment Mx at the section x = 3 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 4 mP = 45 kN at 2.5 mw = 3 kN/m from 0 to 4 mx = 3 m
Mx = kN·m
7.Beam deflectionMedium
P = 21 kNABδ2 m2 m

A cantilever of length L is fixed at A and carries a point load P at a distance a = 2 m from A. Find the deflection δP under the load.

P = 21 kNa = 2 mL = 4 mE = 70 GPa (aluminium)I = 84 × 10⁶ mm⁴
δP = mm
8.Beam deflectionHard
w = 2 kN/mP = 4 kNδL = 5 m

A simply supported beam carries a uniformly distributed load w and a point load P at midspan. Using superposition, find the midspan deflection δmax.

P = 4 kNw = 2 kN/mL = 5 mE = 70 GPa (aluminium)I = 160 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 1.5 m25 × 60 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)b × h = 25 × 60 mm
Pcr = kN
10.Column bucklingHard
PL = 1 md = 30 mmcross-section

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

L = 1 mE = 200 GPa (steel)d = 30 mm
σcr = MPa
11.Centroid & second moment of areaMedium
26090t = 12xdimensions in mm

A channel section lies with its open side up: a base plate 260 mm wide with two upright legs, 90 mm high overall. Base and legs are all 12 mm thick. Find its second moment of area Ix about the horizontal axis x through its centroid.

b = 260 mmh = 90 mmt = 12 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
2002022010xhogging Mdimensions in mm

A cast-iron beam has the T-section shown, with the flange on top. The allowable stresses are 60 MPa in tension and 150 MPa in compression. Find the largest hogging bending moment Mallow the beam can carry (give its size).

bf = 200 mmtf = 20 mmtw = 10 mmhw = 220 mmσt,allow = 60 MPaσc,allow = 150 MPa
Mallow = kN·m
13.Effective stress in soilMedium
sandγd​ = 15.5 kN/m³γsat​ = 20.5 kN/m³13 mwater tableXz = 11 m

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

z = 11 mzw = 4 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 20.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 16.5 kN/m³γsat​ = 19.5 kN/m³5 mclayγsat​ = 18.5 kN/m³6 mwater tableXz = 8 m

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

z = 8 mzw = 2 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 19.5 kN/m³clay: γsat = 18.5 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 80 kPasandclayCc​ = 0.35, Cr​ = 0.04e0​ = 0.6σ′0​ = 50 kPaσ′p​ = 150 kPa5 mwater table

A 5 m thick overconsolidated clay layer has Cc = 0.35, Cr = 0.04 and e₀ = 0.6. At its mid-depth the effective vertical stress is 50 kPa and the preconsolidation pressure is 150 kPa. A new building adds 80 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 5 mCc = 0.35Cr = 0.04e0 = 0.6σ′0 = 50 kPaσ′p = 150 kPaΔσ = 80 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 5.5 mcv​ = 1.5 m²/year5.5 mimpervious rockwater table

A clay layer 5.5 m thick has a coefficient of consolidation cv = 1.5 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 80% average consolidation the time factor is Tv = 0.567. How many years t does the layer take to reach 80% consolidation?

H = 5.5 mcv = 1.5 m²/yearU = 80%Tv = 0.567single drainage
t = years
17.Hydrostatic forceMedium
gated = 1 mH = 2.5 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of water, with its top edge 1 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 1 mH = 2.5 mb = 1.5 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 0.5 mH = 1 m

A vertical rectangular gate 1 m wide sits in the wall of a tank of glycerin, with its top edge 0.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 0.5 mH = 1 mb = 1 mρ = 1260 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
V = 2.2 m/sD = 200 mmL = 100 mf = 0.022

Water flows at a mean velocity of 2.2 m/s through a pipe 100 m long with an inside diameter of 200 mm. Use the Darcy friction factor f = 0.022 and g = 9.81 m/s². Find the friction head loss hf.

V = 2.2 m/sL = 100 mD = 200 mmf = 0.022g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 2Δz = 5 mL = 150 m, D = 100 mm, f = 0.022× bend (K = 0.3)

Two open reservoirs are joined by a pipe 150 m long with an inside diameter of 100 mm and a Darcy friction factor f = 0.02. The water surface of the upper reservoir is 5 m above that of the lower one. The minor losses are a square-edged entrance (K = 0.5), 2 bends (K = 0.3 each), a valve (K = 2) and the exit into the lower reservoir (K = 1.0). Use g = 9.81 m/s². Find the flow rate Q in L/s.

Δz = 5 mL = 150 mD = 100 mmf = 0.02Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 2Kexit = 1.0
Q = L/s
21.Open-channel flow (Manning)Medium
b = 4 my = 1.5 mn = 0.03, S = 0.0005

A rectangular grass-lined earth channel is 4 m wide. Water flows uniformly 1.5 m deep. Manning n = 0.03 and the bed slope is S = 0.0005. Find the flow rate Q in m³/s.

b = 4 my = 1.5 mn = 0.03S = 0.0005
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 1.5 my = 0.5 mn = 0.012, Q = 1.3 m³/s

A rectangular finished concrete channel 1.5 m wide must carry 1.3 m³/s in uniform flow at a depth of 0.5 m. Manning n = 0.012. Find the required bed slope S (in m/m).

Q = 1.3 m³/sb = 1.5 my = 0.5 mn = 0.012
S = m/m
23.Pumps & pump powerMedium
PQ = 15 L/sH = 26 m

A pump with an efficiency of 82% delivers 15 L/s of water (ρ = 1000 kg/m³) against a head of 26 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 15 L/sH = 26 mη = 82%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 12 L/sΔz = 6 mL = 100 m, D = 100 mm, f = 0.022, ΣK = 5

A pump moves 12 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 6 m higher. The pipe is 100 m long with an inside diameter of 100 mm and a Darcy friction factor f = 0.022; the minor-loss coefficients add up to ΣK = 5 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 72%. Find the shaft power Pshaft in kW.

Q = 12 L/sΔz = 6 mL = 100 mD = 100 mmf = 0.022ΣK = 5η = 72%
Pshaft = kW
25.Time value of moneyMedium
years01234€5 000FV = ?

You invest €5 000 at a nominal rate of 4.8% per year, compounded monthly. Find the value FV of the investment after 4 years.

PV = €5 0004.8% / 12n = 4
FV = €
26.Time value of moneyHard
months0123…360€50€50€50FV = ?

You save €50 at the end of every month for 30 years. The account pays 6% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €506% / 12N = 360
FV = €
27.NPV & IRRMedium
years01234−30 00012 00012 00010 00014 000

An investment of €30 000 gives these cash flows at the end of years 1 to 4: €12 000, €12 000, €10 000, €14 000. The cost of capital is 8%. Find the net present value NPV.

r = 8%CF0 = −30 000CF1 = 12 000CF2 = 12 000CF3 = 10 000CF4 = 14 000
NPV = €
28.NPV & IRRHard
years0123−25 00011 00014 50010 000

A project costs €25 000 and returns €11 000, €14 500, €10 000 at the end of years 1 to 3. Cash flows can be reinvested at the cost of capital of 8%. Find the modified internal rate of return MIRR in percent.

r = 8%CF0 = −25 000CF1 = 11 000CF2 = 14 500CF3 = 10 000
MIRR = %
29.Normal distributionMedium
96.25127P = ?

The IQ scores are normally distributed with mean 100 points and standard deviation 15 points. What fraction lies between 96.25 and 127 points? Give P as a decimal.

μ = 100σ = 15x1 = 96.25x2 = 127
P =
30.Normal distributionHard
μ = 65x = ?25%

The exam scores are normally distributed with mean 65 points and standard deviation 10 points. Find the value x below which 25% of them lie (the 25th percentile).

μ = 65σ = 10P = 25%
x = points

3Solutions

1.Beam support reactions

Answer: RA = 31.25 kN

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

P1​ = 55 kNP2​ = 15 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.

ΣMA = 0: RB·4 = 55·2 + 15·3
RB = 155/4 = 38.75 kN
ΣFy = 0: RA = 70 − 38.75 = 31.25 kN

Answer

RA = 31.25 kN
2.Beam support reactions

Answer: RA = 13.75 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.

w = 8 kN/mP = 30 kNABRA​RB​5 m1 m2 m

Free-body diagram

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

Equilibrium

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

UDL resultant: W = w·ℓ = 8·1 = 8 kN, acting at x̄ = 5.5 m
ΣMA = 0: RB·8 = 30·5 + 8·1·5.5
RB = 194/8 = 24.25 kN
ΣFy = 0: RA = 38 − 24.25 = 13.75 kN

Answer

RA = 13.75 kN
3.Truss: method of joints

Answer: FBC = −39.66 kN

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

ABBCACACB55 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·5 = 55·2 → Cy = 22 kN
ΣFy = 0: Ay = 55 − 22 = 33 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 = −22/0.5547 = −39.66 kN

Answer

FBC = −39.66 kN (compression)
4.Truss: method of joints

Answer: FAC = 29.17 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.

ABBCACACB15 kN30 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·6 = 15·1 + 30·3 → Cy = 17.5 kN
ΣFy = 0: Ay = 15 − 17.5 = −2.5 kN
ΣFx = 0: Ax = −30 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 = 3/5.831 = 0.5145, cos γ = 5/5.831 = 0.8575
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −17.5/0.5145 = −34.01 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−34.01)·0.8575 = 29.17 kN

Answer

FAC = 29.17 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 = 14.17 kN, R2 = 20.83 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 = 28.33, MC = 56.67, MD = 85 kN·m, ME = 63.33, MF = 41.67, MG = 0

Answer

Mark D: MD = 85 kN·m
6.Shear force & bending moment

Answer: Mx = 32.63 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 = 3·4 = 12 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 45·2.5 + 3·4·2
RB = 136.5/4 = 34.13 kN
ΣFy = 0: RA = 57 − 34.13 = 22.88 kN
w = 3 kN/mP = 45 kNABRA​ = 22.88RB​ = 34.13section2.5 m0.5 m1 m

Cut at x = 3 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 = 22.88·3 − 45·(3 − 2.5) − 3·3·1.5 = 32.63 kN·m

Answer

Mx = 32.63 kN·m
7.Beam deflection

Answer: δP = 9.524 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 = 21000 N, a = 2000 mm, L = 4000 mm
EI = 5.88 × 10¹² N·mm²

Deflection under the load

δP = Pa³/(3EI) = 21000·2000³/(3·5.88 × 10¹²) = 9.524 mm

Answer

δP = 9.524 mm
8.Beam deflection

Answer: δmax = 2.383 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 = 4000 N, w = 2 N/mm, L = 5000 mm, EI = 1.12 × 10¹³ N·mm²

Each load on its own

δP = PL³/(48EI) = 4000·5000³/(48·1.12 × 10¹³) = 0.9301 mm
δw = 5wL⁴/(384EI) = 5·2·5000⁴/(384·1.12 × 10¹³) = 1.453 mm

Add them

δmax = 0.9301 + 1.453 = 2.383 mm

Answer

δmax = 2.383 mm
9.Column buckling

Answer: Pcr = 68.54 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 = 60·25³/12 = 78125 mm⁴

Effective length

KL = 1·1500 = 1500 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·78125/1500² = 68539 N = 68.54 kN

Answer

Pcr = 68.54 kN
10.Column buckling

Answer: σcr = 226.6 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·30⁴/64 = 39761 mm⁴

Radius of gyration and slenderness

A = 706.9 mm²
r = √(I/A) = √(39761/706.9) = 7.5 mm
KL = 0.7·1000 = 700 mm
KL/r = 700/7.5 = 93.33

Critical stress

σcr = π²E/(KL/r)² = π²·200000/93.33² = 226.6 MPa

Answer

σcr = 226.6 MPa
11.Centroid & second moment of area

Answer: Ix = 3.356 × 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 = 260·12 = 3120 mm², y1 = 6 mm
two legs: A2 = 2·12·78 = 1872 mm², y2 = 12 + 78/2 = 51 mm

Centroid

ȳ = (3120·6 + 1872·51)/4992 = 22.88 mm

Parallel-axis theorem

base: 260·12³/12 + 3120·(6 − 22.88)² = 925909 mm⁴
two legs: 2·12·78³/12 + 1872·(51 − 22.88)² = 2.43 × 10⁶ mm⁴
Ix = 925909 + 2.43 × 10⁶
Ix = 3.356 × 10⁶ mm⁴ = 3.356 × 10⁶ mm⁴

Answer

Ix = 3.356 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Mallow = 23.57 kN·m

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.

Centroid

ȳ = (4000·230 + 2200·110)/6200 = 187.4 mm
top edge: c = 240 − 187.4 = 52.58 mm

Second moment of area

I = 200·20³/12 + 4000·42.58² + 10·220³/12 + 2200·77.42² = 2.945 × 10⁷ mm⁴

Moment allowed by each edge

Hogging: the top is in tension, the bottom in compression.

top edge: M = 60·2.945 × 10⁷/52.58 = 33.6 kN·m
bottom edge: M = 150·2.945 × 10⁷/187.4 = 23.57 kN·m

Governing value

Mallow = min = 23.57 kN·m (bottom edge)

Answer

Mallow = 23.57 kN·m
13.Effective stress in soil

Answer: σ′ = 136.8 kPa

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

Total stress

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

σ = γd·zw + γsat·(z − zw) = 15.5·4 + 20.5·7 = 205.5 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·7 = 68.67 kPa

Effective stress

σ′ = σ − u = 205.5 − 68.67 = 136.8 kPa

Answer

σ′ = 136.8 kPa
14.Effective stress in soil

Answer: σ′ = 88.14 kPa

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

Total stress

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

σ = γd·2 + γsat,sand·3 + γsat,clay·3
σ = 16.5·2 + 19.5·3 + 18.5·3 = 147 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·6 = 58.86 kPa

Effective stress

σ′ = σ − u = 147 − 58.86 = 88.14 kPa

Answer

σ′ = 88.14 kPa
15.Consolidation settlement

Answer: S = 51.87 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 = 50 + 80 = 130 kPa ≤ 150 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.04·5/(1 + 0.6)·log₁₀(130/50) = 51.87 mm

Answer

S = 51.87 mm
16.Consolidation settlement

Answer: t = 11.43 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 = 5.5 m

Time

t = Tv·Hdr²/cv = 0.567·5.5²/1.5 = 11.43 years

Answer

t = 11.43 years
17.Hydrostatic force

Answer: F = 82.77 kN

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

Centroid depth and area

yc = d + H/2 = 1 + 2.5/2 = 2.25 m
A = H·b = 2.5·1.5 = 3.75 m²
gated = 1 mH = 2.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2.25·3.75 = 82.77 kN

Answer

F = 82.77 kN
18.Hydrostatic force

Answer: F = 12.36 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 = 0.5 + 1/2 = 1 m
A = H·b = 1·1 = 1 m²
gated = 0.5 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·1·1 = 12.36 kN

Answer

F = 12.36 kN
19.Pipe friction & head loss

Answer: hf = 2.714 m

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

Velocity head

V²/(2g) = 2.2²/(2·9.81) = 0.2467 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.022·(100/0.2)·2.2²/(2·9.81) = 2.714 m

Answer

hf = 2.714 m
20.Pipe friction & head loss

Answer: Q = 13.32 L/s

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.

Loss coefficients

f·L/D = 0.02·150/0.1 = 30
ΣK = 0.5 + 2·0.3 + 2 + 1.0 = 4.1

Energy equation

Both surfaces are open to the air and practically at rest, so all of Δz is lost in the pipe.

5 = (30 + 4.1)·V²/(2·9.81)
V = √(2·9.81·5/34.1) = 1.696 m/s

Flow rate

Q = V·π·D²/4 = 1.696·0.007854 = 0.01332 m³/s = 13.32 L/s

Answer

Q = 13.32 L/s
21.Open-channel flow (Manning)

Answer: Q = 4.035 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·y = 4·1.5 = 6 m²
P = b + 2y = 4 + 2·1.5 = 7 m
R = A/P = 0.8571 m

Velocity

V = (1/0.03)·0.85712/3·0.00051/2 = 0.6726 m/s

Flow rate

Q = A·V = 6·0.6726 = 4.035 m³/s

Answer

Q = 4.035 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.002154 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 = 1.5·0.5 = 0.75 m²
P = b + 2y = 1.5 + 2·0.5 = 2.5 m
R = A/P = 0.3 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.012·1.3/(0.75·0.4481) = 0.04641
S = 0.04641² = 0.002154

Answer

S = 0.002154

That is a fall of 2.154 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 4.666 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 = 1000·9.81·0.015·26 = 3.826 kW

Shaft power

Pshaft = Ph/η = 3.826/0.82 = 4.666 kW

Answer

Pshaft = 4.666 kW
24.Pumps & pump power

Answer: Pshaft = 1.506 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 = 0.012/0.007854 = 1.528 m/s
V²/(2g) = 0.119 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (22 + 5)·0.119 = 3.213 m

Pump head

H = Δz + hL = 6 + 3.213 = 9.213 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.012·9.213/0.72 = 1.506 kW

Answer

Pshaft = 1.506 kW
25.Time value of money

Answer: FV = 6056 €

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 = 0.048/12 = 0.004
N = m·n = 12·4 = 48

Future value

FV = 5 000·(1 + 0.004)48 = 5 000·1.211 = €6 056.03

Answer

FV = €6 056.03
26.Time value of money

Answer: FV = 50226 €

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 = 0.06/12 = 0.005
N = 12·30 = 360

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 50·(6.023 − 1)/0.005 = €50 225.75

Answer

FV = €50 225.75

You paid in €18 000 yourself; the rest is interest.

27.NPV & IRR

Answer: NPV = 9628 €

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

Present value of each cash flow

CF0 = −30 000
CF1/(1 + 0.08)1 = 12 000/1.08 = 11 111.11
CF2/(1 + 0.08)2 = 12 000/1.166 = 10 288.07
CF3/(1 + 0.08)3 = 10 000/1.26 = 7 938.32
CF4/(1 + 0.08)4 = 14 000/1.36 = 10 290.42

Add them up

NPV = €9 627.92

Answer

NPV = €9 627.92

NPV is positive, so the project earns more than the required return.

28.NPV & IRR

Answer: MIRR = 15.47 %

Modified IRR: compound every inflow forward to the end of the project at the reinvestment rate (usually the cost of capital) to get the terminal value TV. MIRR is the rate that turns the initial investment into TV: MIRR = (TV/C₀)^(1/n) − 1.

Terminal value of the inflows

11 000·1.082 = 12 830.40
14 500·1.081 = 15 660.00
10 000·1.080 = 10 000.00
TV = 38 490.40

MIRR

MIRR = (38 490.40/25 000)1/3 − 1 = 15.47%

Answer

MIRR = 15.47%
29.Normal distribution

Answer: P = 0.5628

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 = (96.25 − 100)/15 = −0.25
z₂ = (127 − 100)/15 = 1.8

Area between

P = Φ(1.8) − Φ(−0.25) = 0.9641 − 0.4013 = 0.5628

Answer

P = 0.5628
30.Normal distribution

Answer: x = 58.26 points

Normal distribution: convert a value x to a z-score, z = (x − μ)/σ, which counts standard deviations from the mean. A z-table (or Φ(z)) gives the area to the left of z, which is P(X < x). The area to the right is 1 − Φ(z), and the area between two values is the difference of their two areas.

z for the percentile

Φ(z) = 0.25 → z = −0.6745

Back to x

x = 65 + −0.6745·10 = 58.26 points

Answer

x = 58.26 points

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