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 = 3 kN/mP = 55 kNABMA​ = ?1.5 m2.5 m

The cantilever beam is fixed to the wall at A. It carries a uniformly distributed load w along its whole length and a point load P at 1.5 m from the wall. Find the magnitude of the reaction moment MA at the wall.

L = 4 mP = 55 kN at 1.5 mw = 3 kN/m from 0 to 4 m
MA = kN·m
2.Beam support reactionsHard
w = 3 kN/mP = 80 kNABCRB​ = ?1.5 m0.5 m0.5 m1.5 m

The beam has a pin at A and a roller at B, 2.5 m from A, and overhangs B to the free end C. It carries a point load P at 1.5 m from A and a uniformly distributed load w from 2 m to the free end at 4 m. Find the vertical reaction RB, taking upward as positive.

AB = 2.5 mAC = 4 mP = 80 kN at 1.5 mw = 3 kN/m from 2 to 4 m
RB = kN
3.Truss: method of jointsMedium
ABBCACACB25 kN4 m1 m4 m

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

span = 4 mheight = 4 mB is 1 m from Avertical load = 25 kN
FAB = kN
4.Truss: method of jointsHard
ABBCACACB50 kN30 kN8 m2 m3 m

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

span = 8 mheight = 3 mB is 2 m from Avertical load = 50 kNhorizontal load = 30 kN ←
FAB = kN
5.Shear force & bending momentMedium
M0​ = 15 kN·mAB8 m2 m

The simply supported beam carries a clockwise couple M0 = 15 kN·m at x = 8 m from A, and no other load. Find the bending moment Mx just to the right of the couple. Use sagging moments positive and upward shear on the left face positive.

L = 10 mM0 = 15 kN·m clockwise, at 8 m
Mx = kN·m
6.Shear force & bending momentHard
12 kN/m55 kN20 kNABCDEFG1 m1 m1 m1 m1 m1 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 m20 kN @ 2 m12 kN/m, 0–4 m
  1. 1A (x = 0 m)
  2. 2B (x = 1 m)
  3. 3C (x = 2 m)
  4. 4D (x = 3 m)
  5. 5E (x = 4 m)
  6. 6F (x = 5 m)
  7. 7G (x = 6 m)
7.Beam deflectionMedium
w = 15 kN/mP = 4 kNABδ4 m

A cantilever carries a uniformly distributed load w over its whole length and a point load P at its free end. Using superposition, find the deflection δ at the free end.

P = 4 kNw = 15 kN/mL = 4 mE = 200 GPa (steel)I = 84 × 10⁶ mm⁴
δ = mm
8.Beam deflectionHard
w = 4 kN/mABδ5 m

A simply supported timber beam of rectangular section, 150 mm wide, carries a uniformly distributed load w over its whole span. Its midspan deflection may not exceed span/250. Find the smallest depth hreq of the section.

w = 4 kN/mL = 5 mE = 11 GPa (timber)b = 150 mm
hreq = mm
9.Column bucklingMedium
PL = 5 md = 40 mmcross-section

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

L = 5 mE = 70 GPa (aluminium)d = 40 mm
Pcr = kN
10.Column bucklingHard
P = 150 kNL = 6 md = ?cross-section

A solid round column of length L made of steel is fixed at both ends. It must carry 150 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.

P = 150 kNn = 3L = 6 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
1703802010xdimensions in mm

A symmetric I-section has flanges 170 mm wide and 20 mm thick, an overall depth of 380 mm and a web 10 mm thick. Find its elastic section modulus Sx for bending about the horizontal centroidal axis x.

B = 170 mmH = 380 mmtf = 20 mmtw = 10 mm
Sx = × 10³ mm³
12.Centroid & second moment of areaHard
130290203002416xdimensions in mm

A welded I-section has a top flange 130 × 20 mm, a web 300 mm high and 16 mm thick, and a bottom flange 290 × 24 mm (width × thickness). Find its second moment of area Ix about the horizontal axis x through its centroid.

top flange: 130 × 20 mmweb: 16 × 300 mmbottom flange: 290 × 24 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
sandγd​ = 15 kN/m³γsat​ = 19.5 kN/m³8 mwater tableXz = 5 m

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

z = 5 mzw = 3 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 19.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 15 kN/m³γsat​ = 19 kN/m³6 mclayγsat​ = 19 kN/m³7 mwater tableXz = 9.5 m

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

z = 9.5 mzw = 4 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 19 kN/m³clay: γsat = 19 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 240 kPasandclayCc​ = 0.25, Cr​ = 0.02e0​ = 1σ′0​ = 100 kPaσ′p​ = 210 kPa4.5 mwater table

A 4.5 m thick overconsolidated clay layer has Cc = 0.25, Cr = 0.02 and e₀ = 1. At its mid-depth the effective vertical stress is 100 kPa and the preconsolidation pressure is 210 kPa. A new building adds 240 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 4.5 mCc = 0.25Cr = 0.02e0 = 1σ′0 = 100 kPaσ′p = 210 kPaΔσ = 240 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 8 mcv​ = 3 m²/year8 msandwater table

A clay layer 8 m thick has a coefficient of consolidation cv = 3 m²/year. It lies between two sand layers, so water drains out at the top and the bottom. For 50% average consolidation the time factor is Tv = 0.197. How many years t does the layer take to reach 50% consolidation?

H = 8 mcv = 3 m²/yearU = 50%Tv = 0.197double drainage
t = years
17.Hydrostatic forceMedium
gated = 2 mH = 2.5 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of water, with its top edge 2 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 2 mH = 2.5 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 3 mH = 1 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of oil, with its top edge 3 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 3 mH = 1 mb = 1.5 mρ = 880 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
Q = 3 L/sD = 50 mmL = 200 mf = 0.03

Water flows at 3 L/s through a pipe 200 m long with an inside diameter of 50 mm. Use the Darcy friction factor f = 0.03 and g = 9.81 m/s². Find the friction head loss hf.

Q = 3 L/sL = 200 mD = 50 mmf = 0.03g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 5Δz = ?L = 150 m, D = 300 mm, f = 0.0222× bend (K = 0.3)

Two open reservoirs are joined by a pipe 150 m long with an inside diameter of 300 mm and a Darcy friction factor f = 0.022. 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 100 L/s?

Q = 100 L/sL = 150 mD = 300 mmf = 0.022Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 5Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
b = 5.5 my = 1.1 m1.5 : 1n = 0.015, S = 0.002

A trapezoidal brickwork channel has a bottom width of 5.5 m and side slopes of 1.5:1 (horizontal:vertical). Water flows uniformly 1.1 m deep. Manning n = 0.015 and the bed slope is S = 0.002. Find the flow rate Q in m³/s.

b = 5.5 my = 1.1 mz = 1.5n = 0.015S = 0.002
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 4 my = 2 m3 : 1n = 0.03, Q = 53 m³/s

A trapezoidal grass-lined earth channel with a bottom width of 4 m and side slopes of 3:1 (horizontal:vertical) must carry 53 m³/s in uniform flow at a depth of 2 m. Manning n = 0.03. Find the required bed slope S (in m/m).

Q = 53 m³/sb = 4 my = 2 mz = 3n = 0.03
S = m/m
23.Pumps & pump powerMedium
PQ = 100 L/sH = 50 m

A pump with an efficiency of 70% delivers 100 L/s of water (ρ = 1000 kg/m³) against a head of 50 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 100 L/sH = 50 mη = 70%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
300 kPa (gauge)PQ = 50 L/sΔz = 19 mL = 300 m, D = 150 mm, f = 0.018, ΣK = 5

A pump moves 50 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 19 m higher. The pipe is 300 m long with an inside diameter of 150 mm and a Darcy friction factor f = 0.018; the minor-loss coefficients add up to ΣK = 5 (entrance and exit included). Use g = 9.81 m/s². The upper tank is closed and the air above its water is at a gauge pressure of 300 kPa. Find the head H the pump must add.

Q = 50 L/sΔz = 19 mL = 300 mD = 150 mmf = 0.018ΣK = 5ptank = 300 kPa
H = m
25.Time value of moneyMedium
years0123…10PV = ?€20 000

You need €20 000 in 10 years. An account pays 6% per year, compounded monthly. How much must you deposit today? Find the present value PV.

FV = €20 0006% / 12n = 10
PV = €
26.Time value of moneyHard
months0123…60€25 000A?AAA

A loan of €25 000 is repaid with equal monthly payments over 5 years. The interest rate is 5.4% per year, compounded monthly. Find the monthly payment A.

P = €25 0005.4% / 12N = 60
A = €
27.NPV & IRRMedium
years0123…9−100 0006 000+4%+4%…r = 9%, NPV = ?

A project costs €100 000 today. It generates €6 000 at the end of the first year, and the cash flow then grows by 4% per year forever. The cost of capital is 9%. Find the net present value NPV.

C0 = €100 000CF1 = €6 000g = 4%r = 9%
NPV = €
28.NPV & IRRHard
years0123−40 00023 50024 00018 500

A project costs €40 000 and returns €23 500, €24 000, €18 500 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −40 000CF1 = 23 500CF2 = 24 000CF3 = 18 500
IRR = %
29.Normal distributionMedium
−3−2−10123zshaded area between −z and z = 0.6424

Drag z so that the shaded area between −z and z under the standard normal curve is 0.6424. Find z to two decimals.

A = 0.6424
z =
30.Normal distributionHard
380420460500540580620htop 30%

The battery lifetimes are normally distributed with mean 500 h and standard deviation 40 h. Drag the cut-off so the shaded top 30% is to the right of it. Find the cut-off x.

μ = 500 hσ = 40 h30%
x = h

3Solutions

1.Beam support reactions

Answer: MA = 106.5 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 = 3·4 = 12 kN, x̄ = 2 m

Moment about the wall

MA = P·a + W·x̄ = 55·1.5 + 12·2 = 106.5 kN·m

Answer

MA = 106.5 kN·m
2.Beam support reactions

Answer: RB = 55.2 kN

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.

Resultant of the distributed load

W = 3·2 = 6 kN, x̄ = (2 + 4)/2 = 3 m

Equilibrium

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

ΣMA = 0: RB·2.5 = 80·1.5 + 6·3
RB = 138/2.5 = 55.2 kN
RA = 86 − 55.2 = 30.8 kN

Answer

RB = 55.2 kN
3.Truss: method of joints

Answer: FAB = −19.33 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.

ABBCACACB25 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·4 = 25·1 → Cy = 6.25 kN
ΣFy = 0: Ay = 25 − 6.25 = 18.75 kN

Joint A

Assume every member is in tension (pulling away from the joint). Only AB has a vertical component at A.

sin α = 4/4.123 = 0.9701
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −18.75/0.9701 = −19.33 kN

Answer

FAB = −19.33 kN (compression)
4.Truss: method of joints

Answer: FAB = −58.59 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.

ABBCACACB50 kN30 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·8 = 50·2 − 30·3 → Cy = 1.25 kN
ΣFy = 0: Ay = 50 − 1.25 = 48.75 kN
ΣFx = 0: Ax = 30 kN

Joint A

Assume every member is in tension (pulling away from the joint). Only AB has a vertical component at A.

sin α = 3/3.606 = 0.8321
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −48.75/0.8321 = −58.59 kN

Answer

FAB = −58.59 kN (compression)
5.Shear force & bending moment

Answer: Mx = 3 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. An applied couple makes the bending moment diagram jump by the size of the couple.

Support reactions

Moments about A, counter-clockwise positive: RB·L − M0 = 0. Vertical balance: RA + RB = 0.

RB = M0/L = 15/10 = 1.5 kN (upward)
RA = −RB = −1.5 kN (downward)

Cut just right of the couple

The left part now contains RA and the couple.

Mx = RA·a + M0 = −1.5·8 + 15 = 3 kN·m

Answer

Mx = 3 kN·m
6.Shear force & bending moment

Answer: E (x = 4 m)

Largest bending moment: M changes slope wherever the shear force changes, so its peaks sit where the shear force crosses zero: under a point load, inside a distributed load, or over a support of an overhang. At a fixed support of a cantilever the moment is largest at the wall. Compare the size of M at those places, sagging or hogging.

Support reactions

Take moments about one support, then use the vertical force balance.

R1 = 6.5 kN, R2 = 116.5 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 = 0.5, MC = −11, MD = −54.5, ME = −110 kN·m, MF = −55, MG = 0

Answer

Mark E: ME = −110 kN·m
7.Beam deflection

Answer: δ = 33.65 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 = 15 N/mm, L = 4000 mm
EI = 1.68 × 10¹³ N·mm²

Each load on its own

δP = PL³/(3EI) = 4000·4000³/(3·1.68 × 10¹³) = 5.079 mm
δw = wL⁴/(8EI) = 15·4000⁴/(8·1.68 × 10¹³) = 28.57 mm

Add them

δ = 5.079 + 28.57 = 33.65 mm

Answer

δ = 33.65 mm
8.Beam deflection

Answer: hreq = 227.9 mm

Beam deflection: deflections come from integrating the curvature M/(EI) twice. Standard cases are tabulated, for example PL³/(3EI) for a cantilever with an end load and 5wL⁴/(384EI) for a simply supported beam under a full uniform load. Deflections from separate loads add (superposition).

Consistent units

Work in N and mm: P in N, w in N/mm (kN/m = N/mm), L in mm, E in N/mm² (GPa × 1000), I in mm⁴.

w = 4 N/mm, L = 5000 mm, E = 11000 N/mm²

Deflection limit

δallow = L/250 = 5000/250 = 20 mm

Required second moment of area

Ireq = 5wL⁴/(384·E·δallow) = 5·4·5000⁴/(384·11000·20) = 1.48 × 10⁸ mm⁴

Required depth

bh³/12 = Ireq → h = (12·1.48 × 10⁸/150)1/3 = 227.9 mm

Answer

hreq = 227.9 mm

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

9.Column buckling

Answer: Pcr = 3.473 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·40⁴/64 = 125664 mm⁴

Effective length

KL = 1·5000 = 5000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·125664/5000² = 3473 N = 3.473 kN

Answer

Pcr = 3.473 kN
10.Column buckling

Answer: d = 80.41 mm

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

Required critical load

Pcr = n·P = 3·150000 = 450000 N
KL = 0.5·6000 = 3000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·450000·3000²/(π³·200000))^(1/4) = 80.41 mm

Answer

d = 80.41 mm

Check: the slenderness KL/r is 149.2, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: Sx = 1333 × 10³ mm³

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

Outer rectangle minus the two side cut-outs

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

hw = 380 − 2·20 = 340 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (170·380³ − 160·340³)/12
Ix = 2.533 × 10⁸ mm⁴

Section modulus

c = H/2 = 190 mm
Sx = I/c = 2.533 × 10⁸/190
Sx = 1.333 × 10⁶ mm³ = 1333 × 10³ mm³

Answer

Sx = 1333 × 10³ mm³
12.Centroid & second moment of area

Answer: Ix = 250.4 × 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 three rectangles

Measure every y from the bottom edge.

top flange: A = 2600 mm², y = 334 mm
web: A = 4800 mm², y = 174 mm
bottom flange: A = 6960 mm², y = 12 mm

Centroid

ȳ = (2600·334 + 4800·174 + 6960·12)/14360 = 124.5 mm

Parallel-axis theorem

top flange: 130·20³/12 + 2600·209.5² = 1.143 × 10⁸ mm⁴
web: 16·300³/12 + 4800·49.55² = 4.778 × 10⁷ mm⁴
bottom flange: 290·24³/12 + 6960·112.5² = 8.835 × 10⁷ mm⁴
Ix = 1.143 × 10⁸ + 4.778 × 10⁷ + 8.835 × 10⁷
Ix = 2.504 × 10⁸ mm⁴ = 250.4 × 10⁶ mm⁴

Answer

Ix = 250.4 × 10⁶ mm⁴
13.Effective stress in soil

Answer: σ′ = 64.38 kPa

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

Total stress

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

σ = γd·zw + γsat·(z − zw) = 15·3 + 19.5·2 = 84 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·2 = 19.62 kPa

Effective stress

σ′ = σ − u = 84 − 19.62 = 64.38 kPa

Answer

σ′ = 64.38 kPa
14.Effective stress in soil

Answer: σ′ = 110.5 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·4 + γsat,sand·2 + γsat,clay·3.5
σ = 15·4 + 19·2 + 19·3.5 = 164.5 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 = 164.5 − 53.96 = 110.5 kPa

Answer

σ′ = 110.5 kPa
15.Consolidation settlement

Answer: S = 132.2 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 = 100 + 240 = 340 kPa > 210 kPa

Settlement

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

S = 0.02·4.5/(1 + 1)·log₁₀(210/100) + 0.25·4.5/(1 + 1)·log₁₀(340/210)
S = 14.5 + 117.7 = 132.2 mm

Answer

S = 132.2 mm
16.Consolidation settlement

Answer: t = 1.051 years

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

Drainage path

Hdr = H/2 = 8/2 = 4 m

Time

t = Tv·Hdr²/cv = 0.197·4²/3 = 1.051 years

Answer

t = 1.051 years
17.Hydrostatic force

Answer: F = 239.1 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 + 2.5/2 = 3.25 m
A = H·b = 2.5·3 = 7.5 m²
gated = 2 mH = 2.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3.25·7.5 = 239.1 kN

Answer

F = 239.1 kN
18.Hydrostatic force

Answer: F = 45.32 kN

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

Centroid depth and area

yc = d + H/2 = 3 + 1/2 = 3.5 m
A = H·b = 1·1.5 = 1.5 m²
gated = 3 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 880·9.81·3.5·1.5 = 45.32 kN

Answer

F = 45.32 kN
19.Pipe friction & head loss

Answer: hf = 14.28 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.

Mean velocity

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

Velocity head

V²/(2g) = 1.528²/(2·9.81) = 0.119 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.03·(200/0.05)·1.528²/(2·9.81) = 14.28 m

Answer

hf = 14.28 m
20.Pipe friction & head loss

Answer: Δz = 1.846 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 = 0.1/0.07069 = 1.415 m/s
V²/(2g) = 0.102 m

Loss coefficients

f·L/D = 0.022·150/0.3 = 11
ΣK = 0.5 + 2·0.3 + 5 + 1.0 = 7.1

Total head loss

hf = 11·0.102 = 1.122 m
hm = 7.1·0.102 = 0.7243 m
Δz = hf + hm = 1.846 m

Answer

Δz = 1.846 m
21.Open-channel flow (Manning)

Answer: Q = 20.72 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 = (5.5 + 1.5·1.1)·1.1 = 7.865 m²
P = b + 2y·√(1 + z²) = 5.5 + 2·1.1·√(1 + 1.5²) = 9.466 m
R = A/P = 0.8309 m

Velocity

V = (1/0.015)·0.83092/3·0.0021/2 = 2.635 m/s

Flow rate

Q = A·V = 7.865·2.635 = 20.72 m³/s

Answer

Q = 20.72 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.004949 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 + z·y)·y = (4 + 3·2)·2 = 20 m²
P = b + 2y·√(1 + z²) = 4 + 2·2·√(1 + 3²) = 16.65 m
R = A/P = 1.201 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.03·53/(20·1.13) = 0.07035
S = 0.07035² = 0.004949

Answer

S = 0.004949

That is a fall of 4.949 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 70.07 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 = 1000·9.81·0.1·50 = 49.05 kW

Shaft power

Pshaft = Ph/η = 49.05/0.7 = 70.07 kW

Answer

Pshaft = 70.07 kW
24.Pumps & pump power

Answer: H = 66.31 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 = 0.05/0.01767 = 2.829 m/s
V²/(2g) = 0.408 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (36 + 5)·0.408 = 16.73 m

Pressure head

p/(ρ·g) = 300000/(1000·9.81) = 30.58 m

Pump head

Both surfaces are practically at rest, so there is no velocity head term.

H = Δz + p/(ρ·g) + hL = 19 + 30.58 + 16.73 = 66.31 m

Answer

H = 66.31 m
25.Time value of money

Answer: PV = 10993 €

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 = 0.06/12 = 0.005
N = 12·10 = 120

Present value

PV = FV/(1 + i)N = 20 000/1.819 = €10 992.65

Answer

PV = €10 992.65
26.Time value of money

Answer: A = 476.4 €

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

Monthly rate and number of payments

i = 0.054000000000000006/12 = 0.0045
N = 12·5 = 60

Payment

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

(1 + i)−N = 0.7638
A = 25 000·0.0045/(1 − 0.7638) = €476.38

Answer

A = €476.38
27.NPV & IRR

Answer: NPV = 20000 €

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.

Value of the cash flows

PV = 6 000/(0.09 − 0.04) = 120 000.00

NPV

NPV = 120 000.00 − 100 000 = €20 000.00

Answer

NPV = €20 000.00

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

28.NPV & IRR

Answer: IRR = 31.29 %

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%) = 698.68
NPV(35%) = −1 904.69

Narrow down

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

IRR ≈ 30 + 5·698.68/(698.68 − (−1 904.69)) = 31.34%
exact: NPV(31.29%) = 0 → IRR = 31.29%

Answer

IRR = 31.29%
29.Normal distribution

Answer: z = 0.92

From an area back to z: Φ(z) is the area to the left of z. For a left-tail area A, find z with Φ(z) = A in the table. A right-tail area A means Φ(z) = 1 − A. A central area A between −z and z leaves (1 − A)/2 in each tail, so Φ(z) = (1 + A)/2. For a value x, use x = μ + zσ.

Area to the left of z

Φ(z) = (1 + 0.6424)/2 = 0.8212

Read the z-table backwards

Find 0.8212 inside the table and read off z.

z = 0.92

Answer

z = 0.92
30.Normal distribution

Answer: x = 521 h

From an area back to z: Φ(z) is the area to the left of z. For a left-tail area A, find z with Φ(z) = A in the table. A right-tail area A means Φ(z) = 1 − A. A central area A between −z and z leaves (1 − A)/2 in each tail, so Φ(z) = (1 + A)/2. For a value x, use x = μ + zσ.

Area to the left

Φ(z) = 0.7

z from the table

z ≈ 0.52

Back to the original units

x = 500 + 0.52·40 = 521 h

Answer

x = 521 h

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