FE Civil exam practice: cram pack

Formula sheets, the key method steps for every topic and 30 practice problems, with full solutions at the back.

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1Formulas and methods

Beam support reactions

Equilibrium
ΣFx = 0, ΣFy = 0, ΣM = 0
Uniform load
resultant w·L at the middle of the load
Moment
M = F·d

Method

  1. Draw a free-body diagram and replace each support by its reactions.
  2. Replace every distributed load by a single force at its centroid.
  3. Take moments about one support to find the reaction at the other.
  4. Use ΣFy = 0 to find the remaining reaction, and check with a second moment equation.

Truss: method of joints

Method of joints
ΣFx = 0, ΣFy = 0 at each joint
Method of sections
ΣM = 0 about a cut point
Member force
positive = tension, negative = compression

Method

  1. Find the support reactions for the whole truss.
  2. Method of joints: start at a joint with at most two unknown member forces and use ΣFx = 0 and ΣFy = 0.
  3. Method of sections: cut through the member you need and take moments about a point where the other unknown members meet.
  4. Assume tension; a negative answer means compression.

Shear force & bending moment

Shear and moment
V = ΣF on one side, M = ΣF·d on one side
Bending stress
σ = M·y/I
Rectangle
I = bh³/12
Section modulus
W = I/ymax
Simply supported, uniform load
Mmax = wL²/8

Method

  1. Find the support reactions from equilibrium of the whole beam.
  2. Cut the beam at the section you need and keep one side.
  3. Shear force: sum of the vertical forces on that side. Bending moment: sum of their moments about the cut.
  4. For the maximum moment, find where the shear force is zero.

Beam deflection

Point load at midspan
δ = PL³/(48EI)
Uniform load, simply supported
δ = 5wL⁴/(384EI)
Cantilever, end load
δ = PL³/(3EI)
Cantilever, uniform load
δ = wL⁴/(8EI)
Superposition
δ = δ1 + δ2

Column buckling

Euler load
Pcr = π²EI/(KL)²
Effective length factor
K = 1 pinned–pinned, 0.5 fixed–fixed, 0.7 fixed–pinned, 2 fixed–free
Critical stress
σcr = Pcr/A
Slenderness
λ = KL/r, r = √(I/A)

Centroid & second moment of area

Centroid
ȳ = ΣAiyi/ΣAi
Rectangle
I = bh³/12
Parallel-axis theorem
I = Ic + A·d²
Composite section
I = Σ(Ic,i + Aidi²)

Effective stress in soil

Total stress
σ = Σγi·hi
Pore water pressure
u = γw·(z − zw)
Effective stress
σ′ = σ − u
Water
γw = 9.81 kN/m³

Consolidation settlement

Normally consolidated
S = Cc·H/(1 + e0)·log₁₀(σ′f/σ′0)
Final stress
σ′f = σ′0 + Δσ (at mid-depth of the layer)
Overconsolidated, σ′f ≤ σ′p
S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0)
Overconsolidated, σ′f > σ′p
S = H/(1 + e0)·[Cr·log₁₀(σ′p/σ′0) + Cc·log₁₀(σ′f/σ′p)]
Overconsolidation ratio
OCR = σ′p/σ′0
Time for consolidation
t = Tv·Hdr²/cv
Drainage path
Hdr = H/2 (double drainage), H (single drainage)
Time factors
U 50% → 0.197, 60% → 0.287, 70% → 0.403, 80% → 0.567, 90% → 0.848

Hydrostatic force

Pressure at depth
p = ρgh
Force on a vertical wall
F = ρg·hc·A
Centre of pressure
yp = yc + Ic/(ycA)
Rectangle
Ic = bH³/12

Pipe friction & head loss

Reynolds number
Re = V·D/ν = ρ·V·D/μ
Flow regime
laminar below Re ≈ 2000, turbulent above Re ≈ 4000
Mean velocity
V = Q/A, A = π·D²/4
Darcy–Weisbach
hf = f·(L/D)·V²/(2g)
Minor losses
hm = ΣK·V²/(2g)
Typical K values
entrance 0.5, exit 1.0, 90° bend ≈ 0.3
Pressure drop
Δp = ρ·g·hf
Two open reservoirs
Δz = (f·L/D + ΣK)·V²/(2g)
Free outlet
H = (1 + f·L/D + ΣK)·V²/(2g)

Open-channel flow (Manning)

Manning equation
V = (1/n)·R2/3·S1/2
Flow rate
Q = A·V
Hydraulic radius
R = A/P (P = wetted perimeter, free surface excluded)
Rectangle
A = b·y, P = b + 2y
Trapezoid (side slope z:1)
A = (b + z·y)·y, P = b + 2y·√(1 + z²)
Circular pipe, full or half full
R = D/4
Required slope
S = (n·Q/(A·R2/3))²

Pumps & pump power

Hydraulic power
Ph = ρ·g·Q·H = Q·Δp
Shaft power
Pshaft = Ph/ηpump
Electrical power
Pel = Pshaft/ηmotor
Pump head
H = Δz + Δp/(ρ·g) + hL
System losses
hL = (f·L/D + ΣK)·V²/(2g)

Time value of money

Future value
FV = PV·(1 + i)n
Present value
PV = FV/(1 + i)n
Several periods per year
i = r/m, N = m·n
Annuity, present value
PV = PMT·[1 − (1 + i)−n]/i
Annuity, future value
FV = PMT·[(1 + i)n − 1]/i

Method

  1. Draw a timeline with every cash flow and its timing.
  2. Match the rate to the period: a monthly rate for monthly payments.
  3. Use FV = PV·(1 + i)ⁿ for single amounts and the annuity formulas for equal payments.
  4. Check the sign and the order of magnitude of the answer.

NPV & IRR

Net present value
NPV = −C0 + Σ CFt/(1 + r)t
Equal cash flows
NPV = −C0 + CF·[1 − (1 + r)−n]/r
Internal rate of return
the r at which NPV = 0
Decision
accept when NPV > 0 (or IRR > required return)

Method

  1. List all cash flows with their year; the investment at year 0 is negative.
  2. Discount each cash flow: CFt/(1 + r)t.
  3. Add them up to get the NPV. Positive means the project earns more than r.
  4. For the IRR, find the rate that makes NPV zero by trial or interpolation.

Normal distribution

z-score
z = (x − μ)/σ
Below x
P(X < x) = Φ(z)
Above x
P(X > x) = 1 − Φ(z)
Between
Φ(z2) − Φ(z1)
Percentile
x = μ + z·σ

Method

  1. Convert the value to a z-score: z = (x − μ)/σ.
  2. Look up Φ(z), the area to the left of z.
  3. For the area to the right use 1 − Φ(z); for an interval subtract the two left areas.
  4. For a percentile, work backwards: find z for the area, then x = μ + z·σ.

2Practice problems

1.Beam support reactionsMedium
P1​ = 45 kNP2​ = 60 kNABRA​ = ?RB​2 m3 m3 m

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

L = 8 mP1 = 45 kN at 2 mP2 = 60 kN at 5 m
RA = kN
2.Beam support reactionsHard
w = 2 kN/mP = 10 kNABRA​ = ?RB​2 m1 m1 m

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

L = 4 mP = 10 kN at 3 mw = 2 kN/m from 2 to 4 m
RA = kN
3.Truss: method of jointsMedium
ABCDEFGH20 kN40 kN35 kN4 × 3 m4 m

Exactly one member of this truss carries no force under these loads. Which is the zero-force member? Click it in the diagram.

D: 20 kN ↓F: 40 kN ↓H: 35 kN ↓
  1. 1member AB
  2. 2member BC
  3. 3member CD
  4. 4member DE
  5. 5member FG
  6. 6member GH
  7. 7member AF
  8. 8member HE
  9. 9member BF
  10. 10member CG
  11. 11member DH
  12. 12member BG
  13. 13member DG
4.Truss: method of jointsHard
ABBCACACB10 kN10 kN5 m4 m4 m

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

span = 5 mheight = 4 mB is 4 m from Avertical load = 10 kNhorizontal load = 10 kN →
FBC = kN
5.Shear force & bending momentMedium
w = 3 kN/mABsection3.5 m1.5 m

Find the shear force Vx at the section x = 3.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 5 mw = 3 kN/m from 0 to 5 mx = 3.5 m
Vx = kN
6.Shear force & bending momentHard
w = 4 kN/mP = 40 kNABsection7 m1 m

Find the bending moment Mx at the section x = 7 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 8 mP = 40 kN at 7 mw = 4 kN/m from 0 to 8 mx = 7 m
Mx = kN·m
7.Beam deflectionMedium
w = 20 kN/mABθ4 m

A simply supported beam carries a uniformly distributed load w over its whole span. Find the slope θA of the beam at support A, in radians.

w = 20 kN/mL = 4 mE = 70 GPa (aluminium)I = 36 × 10⁶ mm⁴
θA = rad
8.Beam deflectionHard
w = 15 kN/mAB5 m

A propped cantilever is fixed at A and simply supported (propped) at B. It carries a uniformly distributed load w over its whole length. EI is constant. Find the size of the bending moment MA at the fixed end.

L = 5 mw = 15 kN/m
MA = kN·m
9.Column bucklingMedium
PL = 3 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 = 3 mE = 200 GPa (steel)d = 80 mm
Pcr = kN
10.Column bucklingHard
PL = 3 md = 40 mmcross-section

A column of length L made of aluminium is pinned at both ends. Find its slenderness and the critical buckling stress σcr from Euler’s formula.

L = 3 mE = 70 GPa (aluminium)d = 40 mm
σcr = MPa
11.Centroid & second moment of areaMedium
1802514012xdimensions in mm

Find the second moment of area Ix of the T-section about the horizontal axis x through its centroid.

bf = 180 mmtf = 25 mmtw = 12 mmhw = 140 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
150 mm150 mm97.5 mm80 × 30xIx​ = ?

A 150 mm × 150 mm plate has a rectangular cut-out 80 mm wide and 30 mm high, centred on the vertical centre line with its centre 97.5 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 150 mmh = 150 mmcut-out: 80 × 30 mmhole centre: y = 97.5 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
sandγd​ = 16 kN/m³γsat​ = 19.5 kN/m³12 mwater tableXz = 10 m

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

z = 10 mzw = 1 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 19.5 kN/m³
u = kPa
14.Effective stress in soilHard
sandγd​ = 17 kN/m³γsat​ = 20 kN/m³6 mclayγsat​ = 17 kN/m³5 mwater tableXz = 8.5 m

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

z = 8.5 mzw = 1 mγw = 9.81 kN/m³sand: γd = 17 kN/m³sand: γsat = 20 kN/m³clay: γsat = 17 kN/m³
u = kPa
15.Consolidation settlementMedium
Δσ = 80 kPasandclayCc​ = 0.25, Cr​ = 0.05e0​ = 0.65σ′0​ = 100 kPaσ′p​ = 150 kPa5.5 mwater table

A 5.5 m thick overconsolidated clay layer has Cc = 0.25, Cr = 0.05 and e₀ = 0.65. At its mid-depth the effective vertical stress is 100 kPa and the preconsolidation pressure is 150 kPa. A new building adds 80 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 5.5 mCc = 0.25Cr = 0.05e0 = 0.65σ′0 = 100 kPaσ′p = 150 kPaΔσ = 80 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 8.5 mcv​ = 0.5 m²/year8.5 mimpervious rockwater table

A clay layer 8.5 m thick has a coefficient of consolidation cv = 0.5 m²/year. It lies on impervious rock, with sand above it, so water drains out only at the top. For 50% average consolidation the time factor is Tv = 0.197. How many years t does the layer take to reach 50% consolidation?

H = 8.5 mcv = 0.5 m²/yearU = 50%Tv = 0.197single drainage
t = years
17.Hydrostatic forceMedium
gated = 1 mH = 1 m

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

d = 1 mH = 1 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 0.5 mH = 3 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of glycerin, with its top edge 0.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 0.5 mH = 3 mb = 2 mρ = 1260 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
Q = 75 L/sD = 200 mmL = 1000 mf = 0.03

Water flows at 75 L/s through a pipe 1000 m long with an inside diameter of 200 mm. Use the Darcy friction factor f = 0.03 and g = 9.81 m/s². Find the friction head loss hf.

Q = 75 L/sL = 1000 mD = 200 mmf = 0.03g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 5free outletH = ?L = 400 m, D = 250 mm, f = 0.0152× bend (K = 0.3)

A pipe 400 m long with an inside diameter of 250 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), 2 bends (K = 0.3 each) and a valve (K = 5). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 50 L/s?

Q = 50 L/sL = 400 mD = 250 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×2)Kvalve = 5
H = m
21.Open-channel flow (Manning)Medium
D = 750 mmn = 0.013, S = 0.0008

A concrete storm sewer with an inside diameter of 750 mm flows half full. Manning n = 0.013 and the slope is S = 0.0008. Find the flow rate Q in m³/s.

D = 750 mmn = 0.013S = 0.0008
Q = m³/s
22.Open-channel flow (Manning)Hard
D = 200 mmn = 0.013, V = 1.2 m/s

A concrete sewer with an inside diameter of 200 mm (Manning n = 0.013) must reach a self-cleansing velocity of 1.2 m/s when flowing just full. Find the minimum slope S (in m/m).

D = 200 mmn = 0.013V = 1.2 m/s
S = m/m
23.Pumps & pump powerMedium
PQ = 50 L/sH = 72 m

A pump with an efficiency of 70% delivers 50 L/s of water (ρ = 1000 kg/m³) against a head of 72 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 50 L/sH = 72 mη = 70%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 12 L/sΔz = 7 mL = 100 m, D = 100 mm, f = 0.018, ΣK = 8

A pump moves 12 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 7 m higher. The pipe is 100 m long with an inside diameter of 100 mm and a Darcy friction factor f = 0.018; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 70%. Find the shaft power Pshaft in kW.

Q = 12 L/sΔz = 7 mL = 100 mD = 100 mmf = 0.018ΣK = 8η = 70%
Pshaft = kW
25.Time value of moneyMedium
years0123…9€8 000FV = ?

You invest €8 000 at a nominal rate of 2% per year, compounded quarterly. Find the value FV of the investment after 9 years.

PV = €8 0002% / 4n = 9
FV = €
26.Time value of moneyHard
months0123…36€20 000A?AAA

A loan of €20 000 is repaid with equal monthly payments over 3 years. The interest rate is 7.2% per year, compounded monthly. Find the monthly payment A.

P = €20 0007.2% / 12N = 36
A = €
27.NPV & IRRMedium
years01234−60 00027 00013 00019 00017 000

An investment of €60 000 gives these cash flows at the end of years 1 to 4: €27 000, €13 000, €19 000, €17 000. The cost of capital is 9%. Find the net present value NPV.

r = 9%CF0 = −60 000CF1 = 27 000CF2 = 13 000CF3 = 19 000CF4 = 17 000
NPV = €
28.NPV & IRRHard
years01234−50 00015 50015 50015 50015 500

An investment of €50 000 returns €15 500 at the end of each year for 4 years. Find its internal rate of return IRR in percent.

C0 = €50 000CF = €15 500n = 4
IRR = %
29.Normal distributionMedium
60 kg58.2 kgT = X₁ + … + X₅?

The masses of boxes are independent and normal with mean 12 kg and standard deviation 0.8 kg. Find the probability P that the total mass of 5 of them exceeds 58.2 kg. Round z to two decimals.

μ = 12 kgσ = 0.8 kgn = 5> 58.2 kg
P =
30.Normal distributionHard
157164171178185192199cmbottom 85%

The heights of adult men are normally distributed with mean 178 cm and standard deviation 7 cm. Drag the cut-off so the shaded bottom 85% is to the left of it. Find the cut-off x.

μ = 178 cmσ = 7 cm85%
x = cm

3Solutions

1.Beam support reactions

Answer: RA = 56.25 kN

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

P1​ = 45 kNP2​ = 60 kNABRA​RB​2 m3 m3 m

Free-body diagram

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

Equilibrium

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

ΣMA = 0: RB·8 = 45·2 + 60·5
RB = 390/8 = 48.75 kN
ΣFy = 0: RA = 105 − 48.75 = 56.25 kN

Answer

RA = 56.25 kN
2.Beam support reactions

Answer: RA = 3.5 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.

w = 2 kN/mP = 10 kNABRA​RB​2 m1 m1 m

Free-body diagram

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

Equilibrium

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

UDL resultant: W = w·ℓ = 2·2 = 4 kN, acting at x̄ = 3 m
ΣMA = 0: RB·4 = 10·3 + 2·2·3
RB = 42/4 = 10.5 kN
ΣFy = 0: RA = 14 − 10.5 = 3.5 kN

Answer

RA = 3.5 kN
3.Truss: method of joints

Answer: member CG

Zero-force members: at a joint, the forces must balance in every direction. If a joint has no load and no support, and two of its three members are in line, then the balance across that line involves only the third member, so its force is zero. If only two members meet at an unloaded joint and they are not in line, both are zero.

Joint C

BC and CD lie on one straight line and the joint carries no load. Balancing forces across that line leaves only CG.

ΣF⊥ = 0 → FCG = 0

Check with the method of joints

Solving all joints gives these member forces (T = tension, C = compression).

AB: 32.81 kN (T), BC: 35.62 kN (T), CD: 35.62 kN (T), DE: 38.44 kN (T), FG: 32.81 kN (C), GH: 38.44 kN (C), AF: 54.69 kN (C), HE: 64.06 kN (C), BF: 3.75 kN (T), CG: 0, DH: 16.25 kN (T), BG: 4.688 kN (C), DG: 4.688 kN (T)

Answer

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

Answer: FBC = −16.49 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.

ABBCACACB10 kN10 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·5 = 10·4 + 10·4 → Cy = 16 kN
ΣFy = 0: Ay = 10 − 16 = −6 kN
ΣFx = 0: Ax = −10 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 = −16/0.9701 = −16.49 kN

Answer

FBC = −16.49 kN (compression)
5.Shear force & bending moment

Answer: Vx = −3 kN

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 = 3·5 = 15 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 3·5·2.5
RB = 37.5/5 = 7.5 kN
ΣFy = 0: RA = 15 − 7.5 = 7.5 kN
w = 3 kN/mABRA​ = 7.5RB​ = 7.5section3.5 m1.5 m

Cut at x = 3.5 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.

V = RA − (all downward loads left of the cut)
Vx = 7.5 − 3·3.5 = −3 kN

Answer

Vx = −3 kN
6.Shear force & bending moment

Answer: Mx = 49 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 = 4·8 = 32 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 40·7 + 4·8·4
RB = 408/8 = 51 kN
ΣFy = 0: RA = 72 − 51 = 21 kN
w = 4 kN/mP = 40 kNABRA​ = 21RB​ = 51section7 m1 m

Cut at x = 7 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 = 21·7 − 4·7·3.5 = 49 kN·m

Answer

Mx = 49 kN·m
7.Beam deflection

Answer: θA = 0.02116 rad

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). The slope θ = dv/dx is the first integral of M/(EI); in consistent units it comes out in radians.

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 = 20 N/mm, L = 4000 mm
EI = 2.52 × 10¹² N·mm²

End slope

θA = wL³/(24EI) = 20·4000³/(24·2.52 × 10¹²) = 0.02116 rad

Answer

θA = 0.02116 rad

That is 1.213°.

8.Beam deflection

Answer: MA = 46.88 kN·m

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). For a statically indeterminate beam, remove a redundant support and require the deflection there to be zero (compatibility).

Remove the prop

Without the prop the beam is a cantilever. Its free end would deflect under the load.

δload = wL⁴/(8EI)

Compatibility at the prop

The prop force RB alone lifts the free end by RBL³/(3EI). The prop holds B at zero deflection, so the two must cancel. EI cancels out.

RB·L³/(3EI) = wL⁴/(8EI) → RB = 3wL/8 = 3·15·5/8 = 28.13 kN

Moment at the fixed end

Moments about A of the loads and the prop force.

MA = wL²/2 − RB·L = 187.5 − 140.6 = 46.88 kN·m

Answer

MA = 46.88 kN·m
9.Column buckling

Answer: Pcr = 900 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 = 0.7·3000 = 2100 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·2.011 × 10⁶/2100² = 899955 N = 900 kN

Answer

Pcr = 900 kN
10.Column buckling

Answer: σcr = 7.676 MPa

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

Smallest second moment of area

A round section has the same I about every axis.

I = πd⁴/64 = π·40⁴/64 = 125664 mm⁴

Radius of gyration and slenderness

A = 1257 mm²
r = √(I/A) = √(125664/1257) = 10 mm
KL = 1·3000 = 3000 mm
KL/r = 3000/10 = 300

Critical stress

σcr = π²E/(KL/r)² = π²·70000/300² = 7.676 MPa

Answer

σcr = 7.676 MPa
11.Centroid & second moment of area

Answer: Ix = 11.3 × 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 two rectangles

Measure every y from the bottom edge.

flange: Af = 180·25 = 4500 mm², yf = 140 + 25/2 = 152.5 mm
web: Aw = 12·140 = 1680 mm², yw = 140/2 = 70 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (4500·152.5 + 1680·70)/6180 = 130.1 mm

Parallel-axis theorem

flange: 180·25³/12 + 4500·(152.5 − 130.1)² = 2.498 × 10⁶ mm⁴
web: 12·140³/12 + 1680·(70 − 130.1)² = 8.807 × 10⁶ mm⁴
Ix = 2.498 × 10⁶ + 8.807 × 10⁶ = 1.13 × 10⁷ mm⁴ = 11.3 × 10⁶ mm⁴

Answer

Ix = 11.3 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 40.65 × 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 = (22500·75 − 2400·97.5)/(22500 − 2400) = 72.31 mm

Full plate about ȳ

150·150³/12 + 22500·2.687² = 42.35 × 10⁶ mm⁴

Hole about ȳ

80·30³/12 + 2400·25.19² = 1.702 × 10⁶ mm⁴

Subtract

Ix = 40.65 × 10⁶ mm⁴

Answer

Ix = 40.65 × 10⁶ mm⁴
13.Effective stress in soil

Answer: u = 88.29 kPa

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

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·9 = 88.29 kPa

Answer

u = 88.29 kPa
14.Effective stress in soil

Answer: u = 73.58 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) = 9.81·7.5 = 73.58 kPa

Answer

u = 73.58 kPa
15.Consolidation settlement

Answer: S = 95.33 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 + 80 = 180 kPa > 150 kPa

Settlement

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

S = 0.05·5.5/(1 + 0.65)·log₁₀(150/100) + 0.25·5.5/(1 + 0.65)·log₁₀(180/150)
S = 29.35 + 65.98 = 95.33 mm

Answer

S = 95.33 mm
16.Consolidation settlement

Answer: t = 28.47 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 = 8.5 m

Time

t = Tv·Hdr²/cv = 0.197·8.5²/0.5 = 28.47 years

Answer

t = 28.47 years
17.Hydrostatic force

Answer: F = 14.71 kN

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

Centroid depth and area

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

Resultant force

F = ρ·g·yc·A = 1000·9.81·1.5·1 = 14.71 kN

Answer

F = 14.71 kN
18.Hydrostatic force

Answer: F = 148.3 kN

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

Centroid depth and area

yc = d + H/2 = 0.5 + 3/2 = 2 m
A = H·b = 3·2 = 6 m²
gated = 0.5 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·2·6 = 148.3 kN

Answer

F = 148.3 kN
19.Pipe friction & head loss

Answer: hf = 43.57 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·0.2²/4 = 0.03142 m²
V = Q/A = 0.075/0.03142 = 2.387 m/s

Velocity head

V²/(2g) = 2.387²/(2·9.81) = 0.2905 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.03·(1000/0.2)·2.387²/(2·9.81) = 43.57 m

Answer

hf = 43.57 m
20.Pipe friction & head loss

Answer: H = 1.645 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 = 0.05/0.04909 = 1.019 m/s
V²/(2g) = 0.05288 m

Loss coefficients

f·L/D = 0.015·400/0.25 = 24
ΣK = 0.5 + 2·0.3 + 5 = 6.1

Energy equation

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

H = (1 + 24 + 6.1)·0.05288 = 1.645 m

Answer

H = 1.645 m
21.Open-channel flow (Manning)

Answer: Q = 0.1574 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 = 0.2209 m², R = D/4 = 0.1875 m

Velocity

V = (1/0.013)·0.18752/3·0.00081/2 = 0.7127 m/s

Flow rate

Q = A·V = 0.2209·0.7127 = 0.1574 m³/s

Answer

Q = 0.1574 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.01321 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.

Hydraulic radius

R = D/4 = 0.2/4 = 0.05 m

Solve Manning for S

S = (n·V/R2/3)² = (0.013·1.2/0.1357)² = 0.01321

Answer

S = 0.01321

That is a fall of 13.21 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 50.45 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 = 1000·9.81·0.05·72 = 35.32 kW

Shaft power

Pshaft = Ph/η = 35.32/0.7 = 50.45 kW

Answer

Pshaft = 50.45 kW
24.Pumps & pump power

Answer: Pshaft = 1.697 kW

Pump power: the power given to the water is the hydraulic power Ph = ρ·g·Q·H = Q·Δp. The shaft must deliver more because the pump loses some: Pshaft = Ph/ηpump, and the motor draws Pel = Pshaft/ηmotor. The pump head H follows from the energy equation: static lift + pressure head + all friction and minor losses.

Velocity

V = Q/A = 0.012/0.007854 = 1.528 m/s
V²/(2g) = 0.119 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (18 + 8)·0.119 = 3.094 m

Pump head

H = Δz + hL = 7 + 3.094 = 10.09 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.012·10.09/0.7 = 1.697 kW

Answer

Pshaft = 1.697 kW
25.Time value of money

Answer: FV = 9573 €

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

Rate and number of periods

i = r/m = 0.02/4 = 0.005
N = m·n = 4·9 = 36

Future value

FV = 8 000·(1 + 0.005)36 = 8 000·1.197 = €9 573.44

Answer

FV = €9 573.44
26.Time value of money

Answer: A = 619.4 €

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 = 0.07200000000000001/12 = 0.006
N = 12·3 = 36

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 = 0.8063
A = 20 000·0.006/(1 − 0.8063) = €619.37

Answer

A = €619.37
27.NPV & IRR

Answer: NPV = 2427 €

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 = 27 000/1.09 = 24 770.64
CF2/(1 + 0.09)2 = 13 000/1.188 = 10 941.84
CF3/(1 + 0.09)3 = 19 000/1.295 = 14 671.49
CF4/(1 + 0.09)4 = 17 000/1.412 = 12 043.23

Add them up

NPV = €2 427.20

Answer

NPV = €2 427.20

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

28.NPV & IRR

Answer: IRR = 9.196 %

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)−4)/i = 50 000/15 500 = 3.226

Solve for the rate

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

i = 9%: 3.24
i = 10%: 3.17
IRR = 9.196%

Answer

IRR = 9.196%
29.Normal distribution

Answer: P = 0.8438

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 total

μT = 60 kg, σT = 0.8·√5 = 1.789 kg

Standardise

z = (58.2 − 60)/1.789 = −1.01

Probability

P = 1 − Φ(−1.01) = 0.8438

Answer

P = 0.8438
30.Normal distribution

Answer: x = 185.3 cm

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) = 0.85

z from the table

z ≈ 1.04

Back to the original units

x = 178 + 1.04·7 = 185.3 cm

Answer

x = 185.3 cm

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