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​ = 40 kNABRA​RB​ = ?2.5 m0.5 m1 m

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

L = 4 mP1 = 45 kN at 2.5 mP2 = 40 kN at 3 m
RB = kN
2.Beam support reactionsHard
w = 5 kN/mP = 40 kNABCRB​ = ?0.5 m1.5 m0.5 m1.5 m

The beam has a pin at A and a roller at B, 2.5 m from A, and overhangs B to the free end C. It carries a point load P at 0.5 m from A and a uniformly distributed load w from 2 m to the free end at 4 m. Find the vertical reaction RB, taking upward as positive.

AB = 2.5 mAC = 4 mP = 40 kN at 0.5 mw = 5 kN/m from 2 to 4 m
RB = kN
3.Truss: method of jointsMedium
ABCDEFGH30 kN25 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.

B: 30 kN ↓D: 25 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 FC
  13. 13member HC
4.Truss: method of jointsHard
ABCDEFGH40 kN30 kN30 kN25 kN25 kN4 × 3 m3 m

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

B: 40 kN ↓C: 30 kN ↓G: 30 kN ↓H: 25 kN ↓H: 25 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 FC
  13. 13member HC
5.Shear force & bending momentMedium
w = 4 kN/mP = 35 kNAB1.5 m1.5 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 MA at the fixed support A. Use sagging moments positive and upward shear on the left face positive.

L = 3 mP = 35 kN at 1.5 mw = 4 kN/m from 0 to 3 m
MA = kN·m
6.Shear force & bending momentHard
w = 10 kN/mP = 55 kNABsection0.5 m2 m3.5 m

Find the bending moment Mx at the section x = 0.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 6 mP = 55 kN at 2.5 mw = 10 kN/m from 0 to 6 mx = 0.5 m
Mx = kN·m
7.Beam deflectionMedium
P = 15 kNABδ1.5 m0.5 m

A cantilever of length L is fixed at A and carries a point load P at a distance a = 1.5 m from A. Find the deflection δB at the free end B.

P = 15 kNa = 1.5 mL = 2 mE = 70 GPa (aluminium)I = 120 × 10⁶ mm⁴
δB = mm
8.Beam deflectionHard
w = 2 kN/mP = 4 kNδL = 6 m

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

P = 4 kNw = 2 kN/mL = 6 mE = 11 GPa (timber)I = 120 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 3 md = 40 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 = 40 mm
Pcr = kN
10.Column bucklingHard
P = 10 kNL = 1.5 md = ?cross-section

A solid round column of length L made of aluminium is fixed at the base and pinned at the top. It must carry 10 kN with a factor of safety of 2 against buckling. Find the smallest diameter d.

P = 10 kNn = 2L = 1.5 mE = 70 GPa (aluminium)
d = mm
11.Centroid & second moment of areaMedium
3001018010xdimensions in mm

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

bf = 300 mmtf = 10 mmtw = 10 mmhw = 180 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
100 mm150 mm97.5 mm60 × 40xIx​ = ?

A 100 mm × 150 mm plate has a rectangular cut-out 60 mm wide and 40 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 = 100 mmh = 150 mmcut-out: 60 × 40 mmhole centre: y = 97.5 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
sandγd​ = 15.5 kN/m³γsat​ = 19 kN/m³14 mwater tableXz = 14 m

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

z = 14 mzw = 1 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 19 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 15.5 kN/m³γsat​ = 20 kN/m³4 mclayγsat​ = 18.5 kN/m³7 mwater tableXz = 7.5 m

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

z = 7.5 mzw = 1 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 20 kN/m³clay: γsat = 18.5 kN/m³
u = kPa
15.Consolidation settlementMedium
Δσ = 60 kPasandclayCc​ = 0.3, Cr​ = 0.05e0​ = 0.85σ′0​ = 120 kPaσ′p​ = 200 kPa8 mwater table

An 8 m thick overconsolidated clay layer has Cc = 0.3, Cr = 0.05 and e₀ = 0.85. At its mid-depth the effective vertical stress is 120 kPa and the preconsolidation pressure is 200 kPa. A new building adds 60 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 8 mCc = 0.3Cr = 0.05e0 = 0.85σ′0 = 120 kPaσ′p = 200 kPaΔσ = 60 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 10 mcv​ = 4 m²/year10 mimpervious rockwater table

A clay layer 10 m thick has a coefficient of consolidation cv = 4 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 = 10 mcv = 4 m²/yearU = 50%Tv = 0.197single drainage
t = years
17.Hydrostatic forceMedium
gated = 2 mH = 1.5 m

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

d = 2 mH = 1.5 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 2 m wide sits in the wall of a tank of seawater, 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 = 2 mρ = 1025 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
V = 1.8 m/sD = 50 mmL = 50 mf = 0.028

Water flows at a mean velocity of 1.8 m/s through a pipe 50 m long with an inside diameter of 50 mm. Use the Darcy friction factor f = 0.028 and g = 9.81 m/s². Find the friction head loss hf.

V = 1.8 m/sL = 50 mD = 50 mmf = 0.028g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 10free outletH = ?L = 300 m, D = 250 mm, f = 0.0224× bend (K = 0.3)

A pipe 300 m long with an inside diameter of 250 mm (Darcy friction factor f = 0.022) 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 150 L/s?

Q = 150 L/sL = 300 mD = 250 mmf = 0.022Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 10
H = m
21.Open-channel flow (Manning)Medium
D = 1200 mmn = 0.013, S = 0.004

A concrete storm sewer with an inside diameter of 1200 mm flows just full (as an open channel, not under pressure). Manning n = 0.013 and the slope is S = 0.004. Find the flow rate Q in m³/s.

D = 1200 mmn = 0.013S = 0.004
Q = m³/s
22.Open-channel flow (Manning)Hard
D = 300 mmn = 0.013, V = 1.2 m/s

A concrete sewer with an inside diameter of 300 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 = 300 mmn = 0.013V = 1.2 m/s
S = m/m
23.Pumps & pump powerMedium
PQ = 10 L/sH = 52 m

A pump with an efficiency of 82% delivers 10 L/s of water (ρ = 1000 kg/m³) against a head of 52 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 10 L/sH = 52 mη = 82%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 50 L/sΔz = 6 mL = 150 m, D = 200 mm, f = 0.025, ΣK = 6

A pump moves 50 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 6 m higher. The pipe is 150 m long with an inside diameter of 200 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 65%. Find the shaft power Pshaft in kW.

Q = 50 L/sΔz = 6 mL = 150 mD = 200 mmf = 0.025ΣK = 6η = 65%
Pshaft = kW
25.Time value of moneyMedium
years0123…8PV = ?€40 000

You need €40 000 in 8 years. An account pays 3.6% per year, compounded quarterly. How much must you deposit today? Find the present value PV.

FV = €40 0003.6% / 4n = 8
PV = €
26.Time value of moneyHard
months0123…324€50€50€50FV = ?

You save €50 at the end of every month for 27 years. The account pays 7.2% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €507.2% / 12N = 324
FV = €
27.NPV & IRRMedium
years0123−20 00010 0006 0005 000

An investment of €20 000 gives these cash flows at the end of years 1 to 3: €10 000, €6 000, €5 000. The cost of capital is 12%. Find the net present value NPV.

r = 12%CF0 = −20 000CF1 = 10 000CF2 = 6 000CF3 = 5 000
NPV = €
28.NPV & IRRHard
years0123−20 00014 00014 00011 000

A project costs €20 000 and returns €14 000, €14 000, €11 000 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −20 000CF1 = 14 000CF2 = 14 000CF3 = 11 000
IRR = %
29.Normal distributionMedium
−3−2−10123zshaded area between −z and z = 0.6729

Drag z so that the shaded area between −z and z under the standard normal curve is 0.6729. Find z to two decimals.

A = 0.6729
z =
30.Normal distributionHard
10 cm0X − Y?

The heights X of men and Y of women in a group are independent and normal: X has mean 180 cm and standard deviation 10 cm, Y has mean 170 cm and standard deviation 12 cm. Find the probability P that X is greater than Y. Round z to two decimals.

μX = 180 cm, σX = 10 cmμY = 170 cm, σY = 12 cm
P =

3Solutions

1.Beam support reactions

Answer: RB = 58.13 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​ = 40 kNABRA​RB​2.5 m0.5 m1 m

Free-body diagram

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

Equilibrium

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

ΣMA = 0: RB·4 = 45·2.5 + 40·3
RB = 232.5/4 = 58.13 kN
ΣFy = 0: RA = 85 − 58.13 = 26.88 kN

Answer

RB = 58.13 kN
2.Beam support reactions

Answer: RB = 20 kN

Static equilibrium: a body at rest has ΣFx = 0, ΣFy = 0 and ΣM = 0 about any point. Replace each distributed load by its resultant (its area) acting at the centroid of the load diagram, and take moments about a support to remove that support’s reaction from the equation.

Resultant of the distributed load

W = 5·2 = 10 kN, x̄ = (2 + 4)/2 = 3 m

Equilibrium

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

ΣMA = 0: RB·2.5 = 40·0.5 + 10·3
RB = 50/2.5 = 20 kN
RA = 50 − 20 = 30 kN

Answer

RB = 20 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 G

FG and GH 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: 21.56 kN (T), BC: 21.56 kN (T), CD: 19.69 kN (T), DE: 19.69 kN (T), FG: 20.63 kN (C), GH: 20.63 kN (C), AF: 35.94 kN (C), HE: 32.81 kN (C), BF: 30 kN (T), CG: 0, DH: 25 kN (T), FC: 1.563 kN (C), HC: 1.563 kN (T)

Answer

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

Answer: member DH

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 D

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

ΣF⊥ = 0 → FDH = 0

Check with the method of joints

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

AB: 47.5 kN (T), BC: 47.5 kN (T), CD: 52.5 kN (T), DE: 52.5 kN (T), FG: 105 kN (C), GH: 105 kN (C), AF: 102.5 kN (C), HE: 74.25 kN (C), BF: 40 kN (T), CG: 30 kN (C), DH: 0, FC: 45.96 kN (T), HC: 38.89 kN (T)

Answer

Zero-force member: DH
5.Shear force & bending moment

Answer: MA = −70.5 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: −35·1.5 = −52.5 kN·m
w: −4·3²/2 = −18 kN·m
MA = −52.5 − 18 = −70.5 kN·m

Answer

MA = −70.5 kN·m

Negative means hogging: tension on the top face.

6.Shear force & bending moment

Answer: Mx = 29.79 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 = 10·6 = 60 kN, acting at x̄ = 3 m
ΣMA = 0: RB·6 = 55·2.5 + 10·6·3
RB = 317.5/6 = 52.92 kN
ΣFy = 0: RA = 115 − 52.92 = 62.08 kN
w = 10 kN/mP = 55 kNABRA​ = 62.08RB​ = 52.92section0.5 m2 m3.5 m

Cut at x = 0.5 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 = 62.08·0.5 − 10·0.5·0.25 = 29.79 kN·m

Answer

Mx = 29.79 kN·m
7.Beam deflection

Answer: δB = 3.013 mm

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

Consistent units

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

P = 15000 N, a = 1500 mm, L = 2000 mm
EI = 8.4 × 10¹² N·mm²

Deflection at the free end

Deflection at the load plus the slope at the load times the remaining length.

δP = Pa³/(3EI) = 2.009 mm
θP = Pa²/(2EI) = 0.002009 rad
δB = δP + θP·(L − a) = Pa²(3L − a)/(6EI) = 3.013 mm

Answer

δB = 3.013 mm
8.Beam deflection

Answer: δmax = 39.2 mm

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

Consistent units

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

P = 4000 N, w = 2 N/mm, L = 6000 mm, EI = 1.32 × 10¹² N·mm²

Each load on its own

δP = PL³/(48EI) = 4000·6000³/(48·1.32 × 10¹²) = 13.64 mm
δw = 5wL⁴/(384EI) = 5·2·6000⁴/(384·1.32 × 10¹²) = 25.57 mm

Add them

δmax = 13.64 + 25.57 = 39.2 mm

Answer

δmax = 39.2 mm
9.Column buckling

Answer: Pcr = 56.25 kN

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

Smallest second moment of area

A round section has the same I about every axis.

I = πd⁴/64 = π·40⁴/64 = 125664 mm⁴

Effective length

KL = 0.7·3000 = 2100 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·125664/2100² = 56247 N = 56.25 kN

Answer

Pcr = 56.25 kN
10.Column buckling

Answer: d = 28.4 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 = 2·10000 = 20000 N
KL = 0.7·1500 = 1050 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·20000·1050²/(π³·70000))^(1/4) = 28.4 mm

Answer

d = 28.4 mm

Check: the slenderness KL/r is 147.9, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: Ix = 15.04 × 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 = 300·10 = 3000 mm², yf = 180 + 10/2 = 185 mm
web: Aw = 10·180 = 1800 mm², yw = 180/2 = 90 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (3000·185 + 1800·90)/4800 = 149.4 mm

Parallel-axis theorem

flange: 300·10³/12 + 3000·(185 − 149.4)² = 3.832 × 10⁶ mm⁴
web: 10·180³/12 + 1800·(90 − 149.4)² = 1.121 × 10⁷ mm⁴
Ix = 3.832 × 10⁶ + 1.121 × 10⁷ = 1.504 × 10⁷ mm⁴ = 15.04 × 10⁶ mm⁴

Answer

Ix = 15.04 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 26.36 × 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 = (15000·75 − 2400·97.5)/(15000 − 2400) = 70.71 mm

Full plate about ȳ

100·150³/12 + 15000·4.286² = 28.4 × 10⁶ mm⁴

Hole about ȳ

60·40³/12 + 2400·26.79² = 2.042 × 10⁶ mm⁴

Subtract

Ix = 26.36 × 10⁶ mm⁴

Answer

Ix = 26.36 × 10⁶ mm⁴
13.Effective stress in soil

Answer: σ′ = 135 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 + 19·13 = 262.5 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·13 = 127.5 kPa

Effective stress

σ′ = σ − u = 262.5 − 127.5 = 135 kPa

Answer

σ′ = 135 kPa
14.Effective stress in soil

Answer: u = 63.77 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) = 9.81·6.5 = 63.77 kPa

Answer

u = 63.77 kPa
15.Consolidation settlement

Answer: S = 38.07 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 = 120 + 60 = 180 kPa ≤ 200 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.05·8/(1 + 0.85)·log₁₀(180/120) = 38.07 mm

Answer

S = 38.07 mm
16.Consolidation settlement

Answer: t = 4.925 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 = 0.197·10²/4 = 4.925 years

Answer

t = 4.925 years
17.Hydrostatic force

Answer: F = 80.93 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 = 1.5·2 = 3 m²
gated = 2 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2.75·3 = 80.93 kN

Answer

F = 80.93 kN
18.Hydrostatic force

Answer: F = 140.8 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 = 2·2 = 4 m²
gated = 2.5 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1025·9.81·3.5·4 = 140.8 kN

Answer

F = 140.8 kN
19.Pipe friction & head loss

Answer: hf = 4.624 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) = 1.8²/(2·9.81) = 0.1651 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.028·(50/0.05)·1.8²/(2·9.81) = 4.624 m

Answer

hf = 4.624 m
20.Pipe friction & head loss

Answer: H = 18.61 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 = 0.15/0.04909 = 3.056 m/s
V²/(2g) = 0.4759 m

Loss coefficients

f·L/D = 0.022·300/0.25 = 26.4
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 + 26.4 + 11.7)·0.4759 = 18.61 m

Answer

H = 18.61 m
21.Open-channel flow (Manning)

Answer: Q = 2.466 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 = 1.131 m², R = D/4 = 0.3 m

Velocity

V = (1/0.013)·0.32/3·0.0041/2 = 2.18 m/s

Flow rate

Q = A·V = 1.131·2.18 = 2.466 m³/s

Answer

Q = 2.466 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.007694 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 = 0.3/4 = 0.075 m

Solve Manning for S

S = (n·V/R2/3)² = (0.013·1.2/0.1778)² = 0.007694

Answer

S = 0.007694

That is a fall of 7.694 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 6.221 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 = 1000·9.81·0.01·52 = 5.101 kW

Shaft power

Pshaft = Ph/η = 5.101/0.82 = 6.221 kW

Answer

Pshaft = 6.221 kW
24.Pumps & pump power

Answer: Pshaft = 6.939 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 = 0.05/0.03142 = 1.592 m/s
V²/(2g) = 0.1291 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (18.75 + 6)·0.1291 = 3.195 m

Pump head

H = Δz + hL = 6 + 3.195 = 9.195 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.05·9.195/0.65 = 6.939 kW

Answer

Pshaft = 6.939 kW
25.Time value of money

Answer: PV = 30029 €

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 = 0.036000000000000004/4 = 0.009
N = 4·8 = 32

Present value

PV = FV/(1 + i)N = 40 000/1.332 = €30 029.12

Answer

PV = €30 029.12
26.Time value of money

Answer: FV = 49551 €

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 = 0.07200000000000001/12 = 0.006
N = 12·27 = 324

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 50·(6.946 − 1)/0.006 = €49 551.46

Answer

FV = €49 551.46

You paid in €16 200 yourself; the rest is interest.

27.NPV & IRR

Answer: NPV = −2729 €

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 = −20 000
CF1/(1 + 0.12)1 = 10 000/1.12 = 8 928.57
CF2/(1 + 0.12)2 = 6 000/1.254 = 4 783.16
CF3/(1 + 0.12)3 = 5 000/1.405 = 3 558.90

Add them up

NPV = €−2 729.36

Answer

NPV = €−2 729.36

NPV is negative, so the project earns less than the required return.

28.NPV & IRR

Answer: IRR = 44.67 %

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(40%) = 1 151.60
NPV(45%) = −77.90

Narrow down

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

IRR ≈ 40 + 5·1 151.60/(1 151.60 − (−77.90)) = 44.68%
exact: NPV(44.67%) = 0 → IRR = 44.67%

Answer

IRR = 44.67%
29.Normal distribution

Answer: z = 0.98

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 + 0.6729)/2 = 0.8365

Read the z-table backwards

Find 0.8365 inside the table and read off z.

z = 0.98

Answer

z = 0.98
30.Normal distribution

Answer: P = 0.7389

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 difference

μ = 180 − 170 = 10 cm, σ = 15.62 cm

Standardise

z = (0 − 10)/15.62 = −0.64

Probability

P = 1 − Φ(−0.64) = 0.7389

Answer

P = 0.7389

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