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 = 10 kN/mP = 10 kNABMA​ = ?1.5 m1.5 m1 m

The cantilever beam is fixed to the wall at A. It carries a uniformly distributed load w from the wall to 3 m 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 = 10 kN at 1.5 mw = 10 kN/m from 0 to 3 m
MA = kN·m
2.Beam support reactionsHard
w = 6 kN/mP = 10 kNABRA​ = ?RB​2 m8 m

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

L = 10 mP = 10 kN at 2 mw = 6 kN/m from 2 to 10 m
RA = kN
3.Truss: method of jointsMedium
ABBCACACB25 kN5 m3 m2 m

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

span = 5 mheight = 2 mB is 3 m from Avertical load = 25 kN
FAB = kN
4.Truss: method of jointsHard
ABBCACACB20 kN20 kN8 m7 m4 m

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

span = 8 mheight = 4 mB is 7 m from Avertical load = 20 kNhorizontal load = 20 kN ←
FBC = kN
5.Shear force & bending momentMedium
w = 5 kN/mABsection2.5 m1.5 m

Find the bending moment Mx at the section x = 2.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 4 mw = 5 kN/m from 0 to 4 mx = 2.5 m
Mx = kN·m
6.Shear force & bending momentHard
w = 4 kN/mP = 25 kNAB7 m1 m

The simply supported beam carries a uniformly distributed load w over its whole span and a point load P. Find the maximum bending moment Mmax in the beam.

L = 8 mP = 25 kN at 7 mw = 4 kN/m from 0 to 8 m
Mmax = kN·m
7.Beam deflectionMedium
w = 10 kN/mδL = 3 m

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

w = 10 kN/mL = 3 mE = 70 GPa (aluminium)I = 36 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 10 kN/mδL = 5 m

A simply supported beam carries a uniformly distributed load w. Its deflection may not exceed span/360. Find the smallest second moment of area Ireq that meets this limit.

w = 10 kN/mL = 5 mE = 70 GPa (aluminium)
Ireq = × 10⁶ mm⁴
9.Column bucklingMedium
PL = 2 m30 × 80 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 = 2 mE = 200 GPa (steel)b × h = 30 × 80 mm
Pcr = kN
10.Column bucklingHard
P = 90 kNL = 5 md = ?cross-section

A solid round column of length L made of steel is fixed at the base and free at the top. It must carry 90 kN with a factor of safety of 2 against buckling. Find the smallest diameter d.

P = 90 kNn = 2L = 5 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
xD = 260d = 240dimensions in mm

A circular tube has outside diameter D = 260 mm and inside diameter d = 240 mm. Find its radius of gyration r about the horizontal centroidal axis.

D = 260 mmd = 240 mm
r = mm
12.Centroid & second moment of areaHard
1002526020xM = 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 bending stress σbottom at the bottom edge.

bf = 100 mmtf = 25 mmtw = 20 mmhw = 260 mmM = 15 kN·m
σbottom = MPa
13.Effective stress in soilMedium
sandγd​ = 15.5 kN/m³γsat​ = 20.5 kN/m³14 mwater tableXz = 3 m

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

z = 3 mzw = 1 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 20.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 17 kN/m³γsat​ = 20.5 kN/m³5 mclayγsat​ = 17.5 kN/m³6 mwater tableXz = 8 m

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

z = 8 mzw = 4 mγw = 9.81 kN/m³sand: γd = 17 kN/m³sand: γsat = 20.5 kN/m³clay: γsat = 17.5 kN/m³
u = kPa
15.Consolidation settlementMedium
Δσ = 150 kPasandclayCc​ = 0.35, Cr​ = 0.04e0​ = 0.6σ′0​ = 50 kPaσ′p​ = 100 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 100 kPa. A new building adds 150 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 = 100 kPaΔσ = 150 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 4 mcv​ = 0.8 m²/year4 msandwater table

A clay layer 4 m thick has a coefficient of consolidation cv = 0.8 m²/year. It lies between two sand layers, so water drains out at the top and the bottom. For 70% average consolidation the time factor is Tv = 0.403. How many years t does the layer take to reach 70% consolidation?

H = 4 mcv = 0.8 m²/yearU = 70%Tv = 0.403double drainage
t = years
17.Hydrostatic forceMedium
gated = 1 mH = 2 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 = 2 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 2 mH = 1.5 m

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

d = 2 mH = 1.5 mb = 3 mρ = 1025 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
V = 1.7 m/sD = 300 mmL = 800 mf = 0.015

Water flows at a mean velocity of 1.7 m/s through a pipe 800 m long with an inside diameter of 300 mm. Use the Darcy friction factor f = 0.015 and g = 9.81 m/s². Find the friction head loss hf.

V = 1.7 m/sL = 800 mD = 300 mmf = 0.015g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 10free outletH = ?L = 300 m, D = 200 mm, f = 0.024× bend (K = 0.3)

A pipe 300 m long with an inside diameter of 200 mm (Darcy friction factor f = 0.02) runs from an open reservoir and discharges as a free jet into the air. The minor losses are a square-edged entrance (K = 0.5), 4 bends (K = 0.3 each) and a valve (K = 10). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 100 L/s?

Q = 100 L/sL = 300 mD = 200 mmf = 0.02Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 10
H = m
21.Open-channel flow (Manning)Medium
D = 300 mmn = 0.013, S = 0.0015

A concrete storm sewer with an inside diameter of 300 mm flows just full (as an open channel, not under pressure). Manning n = 0.013 and the slope is S = 0.0015. Find the flow rate Q in m³/s.

D = 300 mmn = 0.013S = 0.0015
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 1.5 my = 0.9 mn = 0.012, Q = 2.4 m³/s

A rectangular finished concrete channel 1.5 m wide must carry 2.4 m³/s in uniform flow at a depth of 0.9 m. Manning n = 0.012. Find the required bed slope S (in m/m).

Q = 2.4 m³/sb = 1.5 my = 0.9 mn = 0.012
S = m/m
23.Pumps & pump powerMedium
PQ = 60 L/sH = 76 m

A pump with an efficiency of 70% delivers 60 L/s of water (ρ = 1000 kg/m³) against a head of 76 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 60 L/sH = 76 mη = 70%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
200 kPa (gauge)PQ = 60 L/sΔz = 6 mL = 300 m, D = 200 mm, f = 0.018, ΣK = 4

A pump moves 60 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 300 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.018; the minor-loss coefficients add up to ΣK = 4 (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 200 kPa. Find the head H the pump must add.

Q = 60 L/sΔz = 6 mL = 300 mD = 200 mmf = 0.018ΣK = 4ptank = 200 kPa
H = m
25.Time value of moneyMedium
years0123…8PV = ?€10 000

You need €10 000 in 8 years. An account pays 5% per year, compounded quarterly. How much must you deposit today? Find the present value PV.

FV = €10 0005% / 4n = 8
PV = €
26.Time value of moneyHard
months0123…132A?AA€100 000

You want €100 000 in 11 years. You save the same amount at the end of every month in an account paying 6% per year, compounded monthly. Find the monthly deposit A.

FV = €100 0006% / 12N = 132
A = €
27.NPV & IRRMedium
years01234−60 00016 00026 00014 00021 000

An investment of €60 000 gives these cash flows at the end of years 1 to 4: €16 000, €26 000, €14 000, €21 000. The cost of capital is 9%. Find the net present value NPV.

r = 9%CF0 = −60 000CF1 = 16 000CF2 = 26 000CF3 = 14 000CF4 = 21 000
NPV = €
28.NPV & IRRHard
years0123…8−10 0002 0002 0002 0002 000

An investment of €10 000 returns €2 000 at the end of each year for 8 years. Find its internal rate of return IRR in percent.

C0 = €10 000CF = €2 000n = 8
IRR = %
29.Normal distributionMedium
32 min33.3 minX + Y?

X is normal with mean 12 min and standard deviation 1.5 min; Y is independent and normal with mean 20 min and standard deviation 2 min. Find the probability P that X + Y is more than 33.3 min. Round z to two decimals.

μX = 12, σX = 1.5μY = 20, σY = 2X + Y > 33.3 min
P =
30.Normal distributionHard
235240245250255260265gtop 30%

The bag weights are normally distributed with mean 250 g and standard deviation 5 g. Drag the cut-off so the shaded top 30% is to the right of it. Find the cut-off x.

μ = 250 gσ = 5 g30%
x = g

3Solutions

1.Beam support reactions

Answer: MA = 60 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 = 10·3 = 30 kN, x̄ = 1.5 m

Moment about the wall

MA = P·a + W·x̄ = 10·1.5 + 30·1.5 = 60 kN·m

Answer

MA = 60 kN·m
2.Beam support reactions

Answer: RA = 27.2 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 = 6 kN/mP = 10 kNABRA​RB​2 m8 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 = 6·8 = 48 kN, acting at x̄ = 6 m
ΣMA = 0: RB·10 = 10·2 + 6·8·6
RB = 308/10 = 30.8 kN
ΣFy = 0: RA = 58 − 30.8 = 27.2 kN

Answer

RA = 27.2 kN
3.Truss: method of joints

Answer: FAB = −18.03 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·5 = 25·3 → Cy = 15 kN
ΣFy = 0: Ay = 25 − 15 = 10 kN

Joint A

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

sin α = 2/3.606 = 0.5547
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −10/0.5547 = −18.03 kN

Answer

FAB = −18.03 kN (compression)
4.Truss: method of joints

Answer: FBC = −7.731 kN

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

ABBCACACB20 kN20 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·8 = 20·7 − 20·4 → Cy = 7.5 kN
ΣFy = 0: Ay = 20 − 7.5 = 12.5 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 = 4/4.123 = 0.9701, cos γ = 1/4.123 = 0.2425
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −7.5/0.9701 = −7.731 kN

Answer

FBC = −7.731 kN (compression)
5.Shear force & bending moment

Answer: Mx = 9.375 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 = 5·4 = 20 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 5·4·2
RB = 40/4 = 10 kN
ΣFy = 0: RA = 20 − 10 = 10 kN
w = 5 kN/mABRA​ = 10RB​ = 10section2.5 m1.5 m

Cut at x = 2.5 m and keep the left part

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

M = RA·x − (each load left of the cut × its distance to the cut)
Mx = 10·2.5 − 5·2.5·1.25 = 9.375 kN·m

Answer

Mx = 9.375 kN·m
6.Shear force & bending moment

Answer: Mmax = 45.72 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. Maximum moment: since dM/dx = V, the bending moment has its peak where the shear force passes through zero, either at a point load or inside a distributed load.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 4·8 = 32 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 25·7 + 4·8·4
RB = 303/8 = 37.88 kN
ΣFy = 0: RA = 57 − 37.88 = 19.13 kN

Where is V = 0?

RA − w·x0 = 0 → x0 = 19.13/4 = 4.781 m

Maximum moment

Mmax = RA·x0 − w·x0²/2 = 19.13·4.781 − 4·4.781²/2 = 45.72 kN·m

Answer

Mmax = 45.72 kN·m

It occurs at x = 4.781 m from A.

7.Beam deflection

Answer: δmax = 4.185 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 = 10 N/mm, L = 3000 mm
EI = 2.52 × 10¹² N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·10·3000⁴/(384·2.52 × 10¹²) = 4.185 mm

Answer

δmax = 4.185 mm
8.Beam deflection

Answer: Ireq = 83.71 × 10⁶ mm⁴

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).

Deflection limit

δallow = L/360 = 5000/360 = 13.89 mm

Required second moment of area

I = 5wL⁴/(384·E·δallow) = 5·10·5000⁴/(384·70000·13.89) = 8.371 × 10⁷ mm⁴
Ireq = 83.71 × 10⁶ mm⁴

Answer

Ireq = 83.71 × 10⁶ mm⁴
9.Column buckling

Answer: Pcr = 88.83 kN

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

Smallest second moment of area

A rectangle buckles about its weak axis, using the smaller dimension cubed.

Imin = h·b³/12 = 80·30³/12 = 180000 mm⁴

Effective length

KL = 1·2000 = 2000 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·180000/2000² = 88826 N = 88.83 kN

Answer

Pcr = 88.83 kN
10.Column buckling

Answer: d = 116.7 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 = 2·90000 = 180000 N
KL = 2·5000 = 10000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·180000·10000²/(π³·200000))^(1/4) = 116.7 mm

Answer

d = 116.7 mm

Check: the slenderness KL/r is 342.6, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: r = 88.46 mm

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. The radius of gyration r = √(I/A) is the distance at which the whole area would give the same I; it is used in column buckling.

Net area and second moment of area

A = π(D² − d²)/4 = 7854 mm²
I = π(D⁴ − d⁴)/64 = 6.146 × 10⁷ mm⁴

Radius of gyration

r = √(I/A) = √(6.146 × 10⁷/7854) = 88.46 mm

Answer

r = 88.46 mm
12.Centroid & second moment of area

Answer: σbottom = 41.5 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 = 100·25 = 2500 mm², yf = 260 + 25/2 = 272.5 mm
web: Aw = 20·260 = 5200 mm², yw = 260/2 = 130 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2500·272.5 + 5200·130)/7700 = 176.3 mm

Parallel-axis theorem

flange: 100·25³/12 + 2500·(272.5 − 176.3)² = 2.328 × 10⁷ mm⁴
web: 20·260³/12 + 5200·(130 − 176.3)² = 4.042 × 10⁷ mm⁴
Ix = 2.328 × 10⁷ + 4.042 × 10⁷ = 6.371 × 10⁷ mm⁴

Bending stress

The bottom edge is ȳ from the axis.

y = 176.3 mm
σ = M·y/I = 1.5 × 10⁷·176.3/6.371 × 10⁷ = 41.5 MPa

Answer

σbottom = 41.5 MPa
13.Effective stress in soil

Answer: σ′ = 36.88 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) = 15.5·1 + 20.5·2 = 56.5 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 = 56.5 − 19.62 = 36.88 kPa

Answer

σ′ = 36.88 kPa
14.Effective stress in soil

Answer: u = 39.24 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) = 9.81·4 = 39.24 kPa

Answer

u = 39.24 kPa
15.Consolidation settlement

Answer: S = 366.9 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 = 50 + 150 = 200 kPa > 100 kPa

Settlement

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

S = 0.04·5/(1 + 0.6)·log₁₀(100/50) + 0.35·5/(1 + 0.6)·log₁₀(200/100)
S = 37.63 + 329.3 = 366.9 mm

Answer

S = 366.9 mm
16.Consolidation settlement

Answer: t = 2.015 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 = 4/2 = 2 m

Time

t = Tv·Hdr²/cv = 0.403·2²/0.8 = 2.015 years

Answer

t = 2.015 years
17.Hydrostatic force

Answer: F = 39.24 kN

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

Centroid depth and area

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

Resultant force

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

Answer

F = 39.24 kN
18.Hydrostatic force

Answer: F = 124.4 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 + 1.5/2 = 2.75 m
A = H·b = 1.5·3 = 4.5 m²
gated = 2 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1025·9.81·2.75·4.5 = 124.4 kN

Answer

F = 124.4 kN
19.Pipe friction & head loss

Answer: hf = 5.892 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) = 1.7²/(2·9.81) = 0.1473 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.015·(800/0.3)·1.7²/(2·9.81) = 5.892 m

Answer

hf = 5.892 m
20.Pipe friction & head loss

Answer: H = 22.05 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 = 0.1/0.03142 = 3.183 m/s
V²/(2g) = 0.5164 m

Loss coefficients

f·L/D = 0.02·300/0.2 = 30
ΣK = 0.5 + 4·0.3 + 10 = 11.7

Energy equation

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

H = (1 + 30 + 11.7)·0.5164 = 22.05 m

Answer

H = 22.05 m
21.Open-channel flow (Manning)

Answer: Q = 0.03745 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 = 0.07069 m², R = D/4 = 0.075 m

Velocity

V = (1/0.013)·0.0752/3·0.00151/2 = 0.5298 m/s

Flow rate

Q = A·V = 0.07069·0.5298 = 0.03745 m³/s

Answer

Q = 0.03745 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.001499 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 = 1.5·0.9 = 1.35 m²
P = b + 2y = 1.5 + 2·0.9 = 3.3 m
R = A/P = 0.4091 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.012·2.4/(1.35·0.5511) = 0.03871
S = 0.03871² = 0.001499

Answer

S = 0.001499

That is a fall of 1.499 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 63.91 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 = 1000·9.81·0.06·76 = 44.73 kW

Shaft power

Pshaft = Ph/η = 44.73/0.7 = 63.91 kW

Answer

Pshaft = 63.91 kW
24.Pumps & pump power

Answer: H = 32.15 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 = 0.06/0.03142 = 1.91 m/s
V²/(2g) = 0.1859 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (27 + 4)·0.1859 = 5.763 m

Pressure head

p/(ρ·g) = 200000/(1000·9.81) = 20.39 m

Pump head

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

H = Δz + p/(ρ·g) + hL = 6 + 20.39 + 5.763 = 32.15 m

Answer

H = 32.15 m
25.Time value of money

Answer: PV = 6720 €

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 = 0.05/4 = 0.0125
N = 4·8 = 32

Present value

PV = FV/(1 + i)N = 10 000/1.488 = €6 719.84

Answer

PV = €6 719.84
26.Time value of money

Answer: A = 536.7 €

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 = 12·11 = 132

Deposit

A = FV·i/((1 + i)N − 1) = 100 000·0.005/(1.932 − 1) = €536.70

Answer

A = €536.70
27.NPV & IRR

Answer: NPV = 2250 €

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

Present value of each cash flow

CF0 = −60 000
CF1/(1 + 0.09)1 = 16 000/1.09 = 14 678.90
CF2/(1 + 0.09)2 = 26 000/1.188 = 21 883.68
CF3/(1 + 0.09)3 = 14 000/1.295 = 10 810.57
CF4/(1 + 0.09)4 = 21 000/1.412 = 14 876.93

Add them up

NPV = €2 250.08

Answer

NPV = €2 250.08

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

28.NPV & IRR

Answer: IRR = 11.81 %

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

Required annuity factor

(1 − (1 + i)−8)/i = 10 000/2 000 = 5

Solve for the rate

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

i = 11%: 5.146
i = 12%: 4.968
IRR = 11.81%

Answer

IRR = 11.81%
29.Normal distribution

Answer: P = 0.3015

Sums and differences of normal variables: if X and Y are independent and normal, X + Y and X − Y are normal too. Means add or subtract: E(X ± Y) = μX ± μY. Variances always add, also for a difference: Var(X ± Y) = σX² + σY², so σ = √(σX² + σY²). Standard deviations never add directly. The total of n independent items with the same distribution has mean n·μ and standard deviation σ·√n. Then standardise as usual: z = (x − mean)/σ and read Φ(z).

Distribution of the sum

μ = 32 min, σ = √(1.5² + 2²) = 2.5 min

Standardise

z = (33.3 − 32)/2.5 = 0.52

Upper tail

P = 1 − Φ(0.52) = 1 − 0.6985 = 0.3015

Answer

P = 0.3015
30.Normal distribution

Answer: x = 252.6 g

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 = 250 + 0.52·5 = 252.6 g

Answer

x = 252.6 g

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