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​ = 10 kNP2​ = 15 kNABRA​RB​ = ?7 m2 m1 m

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

L = 10 mP1 = 10 kN at 7 mP2 = 15 kN at 9 m
RB = kN
2.Beam support reactionsHard
P = 15 kNQ = 55 kNADCRD​ = ?2 m2 m2 m2 m

A compound beam is fixed to the wall at A, has an internal hinge at C (4 m from A) and rests on a roller at D (8 m from A). It carries a point load P at 6 m from A and a point load Q at 2 m from A. Find the reaction RD at the roller.

AC = 4 mAD = 8 mP = 15 kN at 6 mQ = 55 kN at 2 m
RD = kN
3.Truss: method of jointsMedium
ABBCACACB20 kN5 m1 m3 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 = 3 mB is 1 m from Avertical load = 20 kN
FAB = kN
4.Truss: method of jointsHard
ABBCACACB30 kN15 kN6 m4 m3 m

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

span = 6 mheight = 3 mB is 4 m from Avertical load = 30 kNhorizontal load = 15 kN →
FBC = kN
5.Shear force & bending momentMedium
w = 5 kN/mP = 35 kNABsection1 m0.5 m3.5 m

The cantilever is fixed at A. It carries a uniformly distributed load w over its whole length and a point load P at 1.5 m from A. Find the bending moment Mx at the section x = 1 m from the fixed support A. Use sagging moments positive and upward shear on the left face positive.

L = 5 mP = 35 kN at 1.5 mw = 5 kN/m from 0 to 5 mx = 1 m
Mx = kN·m
6.Shear force & bending momentHard
w = 3 kN/mP = 25 kNABsection1 m2 m5 m

Find the bending moment Mx at the section x = 1 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 8 mP = 25 kN at 3 mw = 3 kN/m from 0 to 8 mx = 1 m
Mx = kN·m
7.Beam deflectionMedium
w = 5 kN/mδL = 2.5 m

A cantilever carries a uniformly distributed load w over its whole length. Find the deflection δ at the free end.

w = 5 kN/mL = 2.5 mE = 70 GPa (aluminium)I = 160 × 10⁶ mm⁴
δ = mm
8.Beam deflectionHard
w = 4 kN/mδL = 3 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 = 4 kN/mL = 3 mE = 70 GPa (aluminium)
Ireq = × 10⁶ mm⁴
9.Column bucklingMedium
PL = 4 md = 80 mmcross-section

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

L = 4 mE = 200 GPa (steel)d = 80 mm
Pcr = kN
10.Column bucklingHard
P = 25 kNL = 1.5 md = ?cross-section

A solid round column of length L made of steel is pinned at both ends. It must carry 25 kN with a factor of safety of 2 against buckling. Find the smallest diameter d.

P = 25 kNn = 2L = 1.5 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
B = 240H = 400t = 20xdimensions in mm

A hollow rectangular (box) section has outer width B = 240 mm, outer height H = 400 mm and a uniform wall thickness t = 20 mm. Find its radius of gyration r about the horizontal centroidal axis.

B = 240 mmH = 400 mmt = 20 mm
r = mm
12.Centroid & second moment of areaHard
200 mm240 mm84 mm30 × 20xIx​ = ?

A 200 mm × 240 mm plate has a rectangular cut-out 30 mm wide and 20 mm high, centred on the vertical centre line with its centre 84 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 200 mmh = 240 mmcut-out: 30 × 20 mmhole centre: y = 84 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
sandγd​ = 16 kN/m³γsat​ = 20.5 kN/m³14 mwater tableXz = 11 m

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

z = 11 mzw = 3 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 20.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 16 kN/m³γsat​ = 20.5 kN/m³4 mclayγsat​ = 17 kN/m³6 mwater tableXz = 7 m

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

z = 7 mzw = 1 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 20.5 kN/m³clay: γsat = 17 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 50 kPasandclayCc​ = 0.5, Cr​ = 0.05e0​ = 0.85σ′0​ = 45 kPaOCR = 24.5 mwater table

A 4.5 m thick overconsolidated clay layer has Cc = 0.5, Cr = 0.05 and e₀ = 0.85. At its mid-depth the effective vertical stress is 45 kPa and the overconsolidation ratio is OCR = 2. A new building adds 50 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 4.5 mCc = 0.5Cr = 0.05e0 = 0.85σ′0 = 45 kPaOCR = 2Δσ = 50 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 10 mcv​ = 3 m²/year10 mimpervious rockwater table

A clay layer 10 m thick has a coefficient of consolidation cv = 3 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 70% average consolidation the time factor is Tv = 0.403. How many years t does the layer take to reach 70% consolidation?

H = 10 mcv = 3 m²/yearU = 70%Tv = 0.403single drainage
t = years
17.Hydrostatic forceMedium
gated = 4 mH = 3 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of water, with its top edge 4 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 4 mH = 3 mb = 2 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 2.5 mH = 2 m

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

d = 2.5 mH = 2 mb = 3 mρ = 1260 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
Q = 40 L/sD = 150 mmL = 150 mf = 0.015

Water flows at 40 L/s through a pipe 150 m long with an inside diameter of 150 mm. Use the Darcy friction factor f = 0.015 and g = 9.81 m/s². Find the friction head loss hf.

Q = 40 L/sL = 150 mD = 150 mmf = 0.015g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 2free outletH = ?L = 150 m, D = 100 mm, f = 0.0153× bend (K = 0.3)

A pipe 150 m long with an inside diameter of 100 mm (Darcy friction factor f = 0.015) 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), 3 bends (K = 0.3 each) and a valve (K = 2). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 20 L/s?

Q = 20 L/sL = 150 mD = 100 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 2
H = m
21.Open-channel flow (Manning)Medium
b = 3 my = 1.2 m2 : 1n = 0.015, S = 0.001

A trapezoidal brickwork channel has a bottom width of 3 m and side slopes of 2:1 (horizontal:vertical). Water flows uniformly 1.2 m deep. Manning n = 0.015 and the bed slope is S = 0.001. Find the flow rate Q in m³/s.

b = 3 my = 1.2 mz = 2n = 0.015S = 0.001
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 1.5 my = 2 mn = 0.025, Q = 3.6 m³/s

A rectangular gravel channel 1.5 m wide must carry 3.6 m³/s in uniform flow at a depth of 2 m. Manning n = 0.025. Find the required bed slope S (in m/m).

Q = 3.6 m³/sb = 1.5 my = 2 mn = 0.025
S = m/m
23.Pumps & pump powerMedium
PQ = 80 L/sH = 14 m

A pump delivers 80 L/s of water (ρ = 1000 kg/m³) against a head of 14 m. The pump efficiency is 80% and the electric motor driving it has an efficiency of 95%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 80 L/sH = 14 mηpump = 80%ηmotor = 95%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
PQ = 120 L/sΔz = 18 mL = 300 m, D = 250 mm, f = 0.025, ΣK = 6

A pump moves 120 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 18 m higher. The pipe is 300 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.025; the minor-loss coefficients add up to ΣK = 6 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 82%. Find the shaft power Pshaft in kW.

Q = 120 L/sΔz = 18 mL = 300 mD = 250 mmf = 0.025ΣK = 6η = 82%
Pshaft = kW
25.Time value of moneyMedium
years0123…9PV = ?€20 000+2%+2%…r = 5%

A property is expected to earn net rent of €20 000 next year. The rent is expected to grow by 2% per year forever. The required return is 5% per year. Find the value PV of the property today.

C1 = €20 000g = 2%r = 5%
PV = €
26.Time value of moneyHard
months0123…360€250 000A?AAA

A loan of €250 000 is repaid with equal monthly payments over 30 years. The interest rate is 4.2% per year, compounded monthly. Find the monthly payment A.

P = €250 0004.2% / 12N = 360
A = €
27.NPV & IRRMedium
years01234−45 00021 00015 00017 00014 000

An investment of €45 000 gives these cash flows at the end of years 1 to 4: €21 000, €15 000, €17 000, €14 000. The cost of capital is 5%. Find the net present value NPV.

r = 5%CF0 = −45 000CF1 = 21 000CF2 = 15 000CF3 = 17 000CF4 = 14 000
NPV = €
28.NPV & IRRHard
years0123−20 00011 00013 50012 000

A project costs €20 000 and returns €11 000, €13 500, €12 000 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −20 000CF1 = 11 000CF2 = 13 500CF3 = 12 000
IRR = %
29.Normal distributionMedium
−3−2−10123zshaded area between −z and z = 0.6778

Drag z so that the shaded area between −z and z under the standard normal curve is 0.6778. Find z to two decimals.

A = 0.6778
z =
30.Normal distributionHard
557085100115130145pointstop 10%

The IQ scores are normally distributed with mean 100 points and standard deviation 15 points. Drag the cut-off so the shaded top 10% is to the right of it. Find the cut-off x.

μ = 100 pointsσ = 15 points10%
x = points

3Solutions

1.Beam support reactions

Answer: RB = 20.5 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​ = 10 kNP2​ = 15 kNABRA​RB​7 m2 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·10 = 10·7 + 15·9
RB = 205/10 = 20.5 kN
ΣFy = 0: RA = 25 − 20.5 = 4.5 kN

Answer

RB = 20.5 kN
2.Beam support reactions

Answer: RD = 7.5 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. An internal hinge cannot carry a bending moment, which gives one extra equation: the moment about the hinge of the forces on either side is zero.

Part CD

The hinge has no moment, so moments about C on CD alone must balance.

ΣMC = 0: RD·4 = 15·2
RD = 7.5 kN
VC = 15 − 7.5 = 7.5 kN

Answer

RD = 7.5 kN
3.Truss: method of joints

Answer: FAB = −16.87 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 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·5 = 20·1 → Cy = 4 kN
ΣFy = 0: Ay = 20 − 4 = 16 kN

Joint A

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

sin α = 3/3.162 = 0.9487
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −16/0.9487 = −16.87 kN

Answer

FAB = −16.87 kN (compression)
4.Truss: method of joints

Answer: FBC = −33.05 kN

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

ABBCACACB30 kN15 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·6 = 30·4 + 15·3 → Cy = 27.5 kN
ΣFy = 0: Ay = 30 − 27.5 = 2.5 kN
ΣFx = 0: Ax = −15 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 = 3/3.606 = 0.8321, cos γ = 2/3.606 = 0.5547
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −27.5/0.8321 = −33.05 kN

Answer

FBC = −33.05 kN (compression)
5.Shear force & bending moment

Answer: Mx = −57.5 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.

Keep the free-end part

P: −35·0.5 = −17.5 kN·m
w: −5·4²/2 = −40 kN·m
Mx = −17.5 − 40 = −57.5 kN·m

Answer

Mx = −57.5 kN·m

Negative means hogging: tension on the top face.

6.Shear force & bending moment

Answer: Mx = 26.13 kN·m

Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 3·8 = 24 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 25·3 + 3·8·4
RB = 171/8 = 21.38 kN
ΣFy = 0: RA = 49 − 21.38 = 27.63 kN
w = 3 kN/mP = 25 kNABRA​ = 27.63RB​ = 21.38section1 m2 m5 m

Cut at x = 1 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 = 27.63·1 − 3·1·0.5 = 26.13 kN·m

Answer

Mx = 26.13 kN·m
7.Beam deflection

Answer: δ = 2.18 mm

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

Consistent units

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

w = 5 N/mm, L = 2500 mm
EI = 1.12 × 10¹³ N·mm²

Deflection

δ = wL⁴/(8EI) = 5·2500⁴/(8·1.12 × 10¹³) = 2.18 mm

Answer

δ = 2.18 mm
8.Beam deflection

Answer: Ireq = 7.232 × 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 = 3000/360 = 8.333 mm

Required second moment of area

I = 5wL⁴/(384·E·δallow) = 5·4·3000⁴/(384·70000·8.333) = 7.232 × 10⁶ mm⁴
Ireq = 7.232 × 10⁶ mm⁴

Answer

Ireq = 7.232 × 10⁶ mm⁴
9.Column buckling

Answer: Pcr = 506.2 kN

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

Smallest second moment of area

A round section has the same I about every axis.

I = πd⁴/64 = π·80⁴/64 = 2.011 × 10⁶ mm⁴

Effective length

KL = 0.7·4000 = 2800 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·2.011 × 10⁶/2800² = 506225 N = 506.2 kN

Answer

Pcr = 506.2 kN
10.Column buckling

Answer: d = 32.83 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 = 2·25000 = 50000 N
KL = 1·1500 = 1500 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·50000·1500²/(π³·200000))^(1/4) = 32.83 mm

Answer

d = 32.83 mm

Check: the slenderness KL/r is 182.8, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: r = 144.7 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

b = 200 mm, h = 360 mm
A = BH − bh = 240·400 − 200·360 = 24000 mm²
I = (BH³ − bh³)/12 = 5.024 × 10⁸ mm⁴

Radius of gyration

r = √(I/A) = √(5.024 × 10⁸/24000) = 144.7 mm

Answer

r = 144.7 mm
12.Centroid & second moment of area

Answer: Ix = 229.6 × 10⁶ mm⁴

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

Centroid

ȳ = (48000·120 − 600·84)/(48000 − 600) = 120.5 mm

Full plate about ȳ

200·240³/12 + 48000·−0.4557² = 230.4 × 10⁶ mm⁴

Hole about ȳ

30·20³/12 + 600·−36.46² = 0.8174 × 10⁶ mm⁴

Subtract

Ix = 229.6 × 10⁶ mm⁴

Answer

Ix = 229.6 × 10⁶ mm⁴
13.Effective stress in soil

Answer: σ′ = 133.5 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·zw + γsat·(z − zw) = 16·3 + 20.5·8 = 212 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·8 = 78.48 kPa

Effective stress

σ′ = σ − u = 212 − 78.48 = 133.5 kPa

Answer

σ′ = 133.5 kPa
14.Effective stress in soil

Answer: σ′ = 69.64 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·1 + γsat,sand·3 + γsat,clay·3
σ = 16·1 + 20.5·3 + 17·3 = 128.5 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 = 128.5 − 58.86 = 69.64 kPa

Answer

σ′ = 69.64 kPa
15.Consolidation settlement

Answer: S = 65.17 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.

Preconsolidation pressure

σ′p = OCR·σ′0 = 2·45 = 90 kPa

Compare with the preconsolidation pressure

σ′f = 45 + 50 = 95 kPa > 90 kPa

Settlement

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

S = 0.05·4.5/(1 + 0.85)·log₁₀(90/45) + 0.5·4.5/(1 + 0.85)·log₁₀(95/90)
S = 36.61 + 28.56 = 65.17 mm

Answer

S = 65.17 mm
16.Consolidation settlement

Answer: t = 13.43 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 = 10 m

Time

t = Tv·Hdr²/cv = 0.403·10²/3 = 13.43 years

Answer

t = 13.43 years
17.Hydrostatic force

Answer: F = 323.7 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 = 4 + 3/2 = 5.5 m
A = H·b = 3·2 = 6 m²
gated = 4 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·5.5·6 = 323.7 kN

Answer

F = 323.7 kN
18.Hydrostatic force

Answer: F = 259.6 kN

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

Centroid depth and area

yc = d + H/2 = 2.5 + 2/2 = 3.5 m
A = H·b = 2·3 = 6 m²
gated = 2.5 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·3.5·6 = 259.6 kN

Answer

F = 259.6 kN
19.Pipe friction & head loss

Answer: hf = 3.917 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·0.15²/4 = 0.01767 m²
V = Q/A = 0.04/0.01767 = 2.264 m/s

Velocity head

V²/(2g) = 2.264²/(2·9.81) = 0.2611 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.015·(150/0.15)·2.264²/(2·9.81) = 3.917 m

Answer

hf = 3.917 m
20.Pipe friction & head loss

Answer: H = 8.891 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 = 0.02/0.007854 = 2.546 m/s
V²/(2g) = 0.3305 m

Loss coefficients

f·L/D = 0.015·150/0.1 = 22.5
ΣK = 0.5 + 3·0.3 + 2 = 3.4

Energy equation

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

H = (1 + 22.5 + 3.4)·0.3305 = 8.891 m

Answer

H = 8.891 m
21.Open-channel flow (Manning)

Answer: Q = 11.52 m³/s

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

Geometry

A = (b + z·y)·y = (3 + 2·1.2)·1.2 = 6.48 m²
P = b + 2y·√(1 + z²) = 3 + 2·1.2·√(1 + 2²) = 8.367 m
R = A/P = 0.7745 m

Velocity

V = (1/0.015)·0.77452/3·0.0011/2 = 1.778 m/s

Flow rate

Q = A·V = 6.48·1.778 = 11.52 m³/s

Answer

Q = 11.52 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.002019 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 = 1.5·2 = 3 m²
P = b + 2y = 1.5 + 2·2 = 5.5 m
R = A/P = 0.5455 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.025·3.6/(3·0.6676) = 0.04494
S = 0.04494² = 0.002019

Answer

S = 0.002019

That is a fall of 2.019 m per kilometre.

23.Pumps & pump power

Answer: Pel = 14.46 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 = 1000·9.81·0.08·14 = 10.99 kW

Shaft power

Pshaft = 10.99/0.8 = 13.73 kW

Electrical power

Pel = 13.73/0.95 = 14.46 kW

Answer

Pel = 14.46 kW
24.Pumps & pump power

Answer: Pshaft = 41.58 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 = 0.12/0.04909 = 2.445 m/s
V²/(2g) = 0.3046 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (30 + 6)·0.3046 = 10.97 m

Pump head

H = Δz + hL = 18 + 10.97 = 28.97 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.12·28.97/0.82 = 41.58 kW

Answer

Pshaft = 41.58 kW
25.Time value of money

Answer: PV = 666667 €

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.

Growing perpetuity

PV = C1/(r − g) = 20 000/(0.05 − 0.02) = 20 000/0.03 = €666 666.67

Answer

PV = €666 666.67
26.Time value of money

Answer: A = 1223 €

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 = 0.042/12 = 0.0035
N = 12·30 = 360

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 = 0.2843
A = 250 000·0.0035/(1 − 0.2843) = €1 222.54

Answer

A = €1 222.54
27.NPV & IRR

Answer: NPV = 14809 €

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 = −45 000
CF1/(1 + 0.05)1 = 21 000/1.05 = 20 000.00
CF2/(1 + 0.05)2 = 15 000/1.103 = 13 605.44
CF3/(1 + 0.05)3 = 17 000/1.158 = 14 685.24
CF4/(1 + 0.05)4 = 14 000/1.216 = 11 517.83

Add them up

NPV = €14 808.52

Answer

NPV = €14 808.52

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

28.NPV & IRR

Answer: IRR = 36.58 %

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(35%) = 432.86
NPV(40%) = −881.92

Narrow down

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

IRR ≈ 35 + 5·432.86/(432.86 − (−881.92)) = 36.65%
exact: NPV(36.58%) = 0 → IRR = 36.58%

Answer

IRR = 36.58%
29.Normal distribution

Answer: z = 0.99

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 + 0.6778)/2 = 0.8389

Read the z-table backwards

Find 0.8389 inside the table and read off z.

z = 0.99

Answer

z = 0.99
30.Normal distribution

Answer: x = 119.2 points

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) = 0.9

z from the table

z ≈ 1.28

Back to the original units

x = 100 + 1.28·15 = 119.2 points

Answer

x = 119.2 points

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