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​ = 30 kNP2​ = 20 kNABCRA​ = ?1 m1.5 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. Find the vertical reaction RA, taking upward as positive.

AB = 2.5 mAC = 4 mP1 = 30 kN at 1 mP2 = 20 kN at 4 m
RA = kN
2.Beam support reactionsHard
w = 5 kN/mP = 25 kNABRA​RB​ = ?2 m0.5 m0.5 m2 m

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

L = 5 mP = 25 kN at 2.5 mw = 5 kN/m from 2 to 3 m
RB = kN
3.Truss: method of jointsMedium
ABBCACACB35 kN4 m1 m4 m

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

span = 4 mheight = 4 mB is 1 m from Avertical load = 35 kN
FBC = kN
4.Truss: method of jointsHard
ABCDEFGH35 kN30 kN25 kN4 × 4 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: 35 kN ↓F: 30 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 BG
  13. 13member DG
5.Shear force & bending momentMedium
5 kN/m50 kNABCDEFG1 m1 m1 m1 m1 m1 m

The marks A to G split the beam into six equal parts. At which mark is the bending moment largest in size, sagging or hogging? Click it in the diagram.

50 kN @ 2 m5 kN/m, 1–6 m
  1. 1A (x = 0 m)
  2. 2B (x = 1 m)
  3. 3C (x = 2 m)
  4. 4D (x = 3 m)
  5. 5E (x = 4 m)
  6. 6F (x = 5 m)
  7. 7G (x = 6 m)
6.Shear force & bending momentHard
w = 10 kN/mP = 50 kNAB2.5 m3.5 m

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

L = 6 mP = 50 kN at 2.5 mw = 10 kN/m from 0 to 6 m
Mmax = kN·m
7.Beam deflectionMedium
w = 20 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 = 20 kN/mL = 2.5 mE = 70 GPa (aluminium)I = 84 × 10⁶ mm⁴
δ = mm
8.Beam deflectionHard
w = 15 kN/mP = 6 kNδL = 2.5 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 = 6 kNw = 15 kN/mL = 2.5 mE = 200 GPa (steel)I = 12 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 3 md = 80 mmcross-section

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

L = 3 mE = 70 GPa (aluminium)d = 80 mm
Pcr = kN
10.Column bucklingHard
P = 40 kNL = 1.5 md = ?cross-section

A solid round column of length L made of steel is fixed at the base and free at the top. It must carry 40 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.

P = 40 kNn = 3L = 1.5 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
2403001214xdimensions in mm

A symmetric I-section has flanges 240 mm wide and 12 mm thick, an overall depth of 300 mm and a web 14 mm thick. Find its elastic section modulus Sx for bending about the horizontal centroidal axis x.

B = 240 mmH = 300 mmtf = 12 mmtw = 14 mm
Sx = × 10³ mm³
12.Centroid & second moment of areaHard
1304802214xM = 40 kN·mdimensions in mm

A symmetric I-section has flanges 130 mm wide and 22 mm thick, an overall depth of 480 mm and a web 14 mm thick. It carries a bending moment of 40 kN·m about the axis x. Find the size of the maximum bending stress σmax in the section.

B = 130 mmH = 480 mmtf = 22 mmtw = 14 mmM = 40 kN·m
σmax = MPa
13.Effective stress in soilMedium
sandγd​ = 16 kN/m³γsat​ = 19.5 kN/m³14 mwater tableXz = 12 m

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

z = 12 mzw = 3 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 19.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 15 kN/m³γsat​ = 20.5 kN/m³5 mclayγsat​ = 18 kN/m³7 mwater tableXz = 8.5 m

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

z = 8.5 mzw = 3 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 20.5 kN/m³clay: γsat = 18 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 30 kPasandclayCc​ = 0.4, Cr​ = 0.04e0​ = 0.7σ′0​ = 95 kPaσ′p​ = 195 kPa2.5 mwater table

A 2.5 m thick overconsolidated clay layer has Cc = 0.4, Cr = 0.04 and e₀ = 0.7. At its mid-depth the effective vertical stress is 95 kPa and the preconsolidation pressure is 195 kPa. A new building adds 30 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 2.5 mCc = 0.4Cr = 0.04e0 = 0.7σ′0 = 95 kPaσ′p = 195 kPaΔσ = 30 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 3.5 mcv​ = 3 m²/year3.5 mimpervious rockwater table

A clay layer 3.5 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 = 3.5 mcv = 3 m²/yearU = 70%Tv = 0.403single drainage
t = years
17.Hydrostatic forceMedium
gated = 2 mH = 2.5 m

A vertical rectangular gate 1 m wide sits in the wall of a tank of water, with its top edge 2 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 2 mH = 2.5 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 0.5 mH = 1 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 = 1 mb = 2 mρ = 1260 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
V = 0.8 m/sD = 150 mmL = 50 mf = 0.015

Water flows at a mean velocity of 0.8 m/s through a pipe 50 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.

V = 0.8 m/sL = 50 mD = 150 mmf = 0.015g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 5Δz = ?L = 100 m, D = 150 mm, f = 0.0223× bend (K = 0.3)

Two open reservoirs are joined by a pipe 100 m long with an inside diameter of 150 mm and a Darcy friction factor f = 0.022. The minor losses are a square-edged entrance (K = 0.5), 3 bends (K = 0.3 each), a valve (K = 5) and the exit into the lower reservoir (K = 1.0). Use g = 9.81 m/s². What difference in water level Δz between the reservoirs gives a flow rate of 20 L/s?

Q = 20 L/sL = 100 mD = 150 mmf = 0.022Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 5Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
b = 3 my = 0.7 m1 : 1n = 0.025, S = 0.001

A trapezoidal gravel channel has a bottom width of 3 m and side slopes of 1:1 (horizontal:vertical). Water flows uniformly 0.7 m deep. Manning n = 0.025 and the bed slope is S = 0.001. Find the flow rate Q in m³/s.

b = 3 my = 0.7 mz = 1n = 0.025S = 0.001
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 3.5 my = 1.6 mn = 0.025, Q = 11 m³/s

A rectangular gravel channel 3.5 m wide must carry 11 m³/s in uniform flow at a depth of 1.6 m. Manning n = 0.025. Find the required bed slope S (in m/m).

Q = 11 m³/sb = 3.5 my = 1.6 mn = 0.025
S = m/m
23.Pumps & pump powerMedium
PQ = 15 L/sH = 62 m

A pump delivers 15 L/s of water (ρ = 1000 kg/m³) against a head of 62 m. The pump efficiency is 65% and the electric motor driving it has an efficiency of 88%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 15 L/sH = 62 mηpump = 65%ηmotor = 88%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
PQ = 50 L/sΔz = 8 mL = 300 m, D = 200 mm, f = 0.022, 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 8 m higher. The pipe is 300 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.022; the minor-loss coefficients add up to ΣK = 6 (entrance and exit included). Use g = 9.81 m/s². Find the head H the pump must add.

Q = 50 L/sΔz = 8 mL = 300 mD = 200 mmf = 0.022ΣK = 6
H = m
25.Time value of moneyMedium
years0123…8€20 000FV = ?

You invest €20 000 at a nominal rate of 3.6% per year, compounded quarterly. Find the value FV of the investment after 8 years.

PV = €20 0003.6% / 4n = 8
FV = €
26.Time value of moneyHard
years0123…17€2 500€2 500€2 500FV = ?

You deposit €2 500 at the start of every year for 17 years, the first deposit today. The account pays 8% per year. How much is in the account at the end of year 17? Find FV.

A = €2 500i = 8%n = 17
FV = €
27.NPV & IRRMedium
years01234−30 0009 00012 00014 00011 000

An investment of €30 000 gives these cash flows at the end of years 1 to 4: €9 000, €12 000, €14 000, €11 000. The cost of capital is 7.000000000000001%. Find the net present value NPV.

r = 7.000000000000001%CF0 = −30 000CF1 = 9 000CF2 = 12 000CF3 = 14 000CF4 = 11 000
NPV = €
28.NPV & IRRHard
years0123−10 0005 0004 5007 000

A project costs €10 000 and returns €5 000, €4 500, €7 000 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −10 000CF1 = 5 000CF2 = 4 500CF3 = 7 000
IRR = %
29.Normal distributionMedium
468540P = ?

The battery lifetimes are normally distributed with mean 500 h and standard deviation 40 h. What fraction lies between 468 and 540 h? Give P as a decimal.

μ = 500σ = 40x1 = 468x2 = 540
P =
30.Normal distributionHard
μ = 500x = ?5%

The battery lifetimes are normally distributed with mean 500 h and standard deviation 40 h. Find the value x below which 5% of them lie (the 5th percentile).

μ = 500σ = 40P = 5%
x = h

3Solutions

1.Beam support reactions

Answer: RA = 6 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.

Moments about A

Counter-clockwise positive.

ΣMA = 0: RB·2.5 = 30·1 + 20·4
RB = 110/2.5 = 44 kN

Vertical equilibrium

RA = 30 + 20 − 44 = 6 kN

Answer

RA = 6 kN
2.Beam support reactions

Answer: RB = 15 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 = 5 kN/mP = 25 kNABRA​RB​2 m0.5 m0.5 m2 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 = 5·1 = 5 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 25·2.5 + 5·1·2.5
RB = 75/5 = 15 kN
ΣFy = 0: RA = 30 − 15 = 15 kN

Answer

RB = 15 kN
3.Truss: method of joints

Answer: FBC = −10.94 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.

ABBCACACB35 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·4 = 35·1 → Cy = 8.75 kN
ΣFy = 0: Ay = 35 − 8.75 = 26.25 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 = 4/5 = 0.8, cos γ = 3/5 = 0.6
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −8.75/0.8 = −10.94 kN

Answer

FBC = −10.94 kN (compression)
4.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: 30 kN (T), BC: 20 kN (T), CD: 20 kN (T), DE: 10 kN (T), FG: 55 kN (C), GH: 35 kN (C), AF: 77.78 kN (C), HE: 14.14 kN (C), BF: 25 kN (T), CG: 0, DH: 10 kN (T), BG: 14.14 kN (T), DG: 14.14 kN (C)

Answer

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

Answer: C (x = 2 m)

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

Support reactions

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

R1 = 43.75 kN, R2 = 31.25 kN

Bending moment at every mark

Sum the moments of all forces on one side of the cut. Sagging is positive, hogging negative.

MA = 0, MB = 43.75, MC = 85 kN·m, MD = 71.25, ME = 52.5, MF = 28.75, MG = 0

Answer

Mark C: MC = 85 kN·m
6.Shear force & bending moment

Answer: Mmax = 116.7 kN·m

Method of sections: cut the beam where you want the internal forces and keep one side. The shear force V balances the vertical forces on that side, and the bending moment M balances their moments about the cut. Maximum moment: since dM/dx = V, the bending moment has its peak where the shear force passes through zero, either at a point load or inside a distributed load.

Support reactions

Equilibrium of the whole beam.

UDL resultant: W = w·ℓ = 10·6 = 60 kN, acting at x̄ = 3 m
ΣMA = 0: RB·6 = 50·2.5 + 10·6·3
RB = 305/6 = 50.83 kN
ΣFy = 0: RA = 110 − 50.83 = 59.17 kN

Where is V = 0?

V(2.5⁻) = RA − w·2.5 = 34.17 kN
V(2.5⁺) = 34.17 − 50 = −15.83 kN
The shear changes sign at the load, so the maximum is under the load.

Maximum moment

Mmax = RA·2.5 − w·2.5²/2 = 59.17·2.5 − 10·2.5²/2 = 116.7 kN·m

Answer

Mmax = 116.7 kN·m

It occurs at x = 2.5 m from A.

7.Beam deflection

Answer: δ = 16.61 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 = 20 N/mm, L = 2500 mm
EI = 5.88 × 10¹² N·mm²

Deflection

δ = wL⁴/(8EI) = 20·2500⁴/(8·5.88 × 10¹²) = 16.61 mm

Answer

δ = 16.61 mm
8.Beam deflection

Answer: δmax = 3.993 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 = 6000 N, w = 15 N/mm, L = 2500 mm, EI = 2.4 × 10¹² N·mm²

Each load on its own

δP = PL³/(48EI) = 6000·2500³/(48·2.4 × 10¹²) = 0.8138 mm
δw = 5wL⁴/(384EI) = 5·15·2500⁴/(384·2.4 × 10¹²) = 3.179 mm

Add them

δmax = 0.8138 + 3.179 = 3.993 mm

Answer

δmax = 3.993 mm
9.Column buckling

Answer: Pcr = 154.3 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 = 1·3000 = 3000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·2.011 × 10⁶/3000² = 154342 N = 154.3 kN

Answer

Pcr = 154.3 kN
10.Column buckling

Answer: d = 57.78 mm

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

Required critical load

Pcr = n·P = 3·40000 = 120000 N
KL = 2·1500 = 3000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·120000·3000²/(π³·200000))^(1/4) = 57.78 mm

Answer

d = 57.78 mm

Check: the slenderness KL/r is 207.7, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: Sx = 960.2 × 10³ mm³

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

Outer rectangle minus the two side cut-outs

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

hw = 300 − 2·12 = 276 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (240·300³ − 226·276³)/12
Ix = 1.44 × 10⁸ mm⁴

Section modulus

c = H/2 = 150 mm
Sx = I/c = 1.44 × 10⁸/150
Sx = 960248 mm³ = 960.2 × 10³ mm³

Answer

Sx = 960.2 × 10³ mm³
12.Centroid & second moment of area

Answer: σmax = 24.19 MPa

Composite areas: split the section into rectangles. The centroid is the area-weighted average ȳ = ΣAᵢyᵢ/ΣAᵢ. The second moment of area about the centroidal axis adds each part’s own bh³/12 and its parallel-axis term A·d², where d is the distance from the part’s centroid to the overall centroid. Bending stress is σ = M·y/I.

Outer rectangle minus the two side cut-outs

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

hw = 480 − 2·22 = 436 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (130·480³ − 116·436³)/12
Ix = 3.969 × 10⁸ mm⁴

Bending stress

y = 240 mm
σ = M·y/I = 4 × 10⁷·240/3.969 × 10⁸ = 24.19 MPa

Answer

σmax = 24.19 MPa
13.Effective stress in soil

Answer: σ′ = 135.2 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 + 19.5·9 = 223.5 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·9 = 88.29 kPa

Effective stress

σ′ = σ − u = 223.5 − 88.29 = 135.2 kPa

Answer

σ′ = 135.2 kPa
14.Effective stress in soil

Answer: σ′ = 95.04 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·3 + γsat,sand·2 + γsat,clay·3.5
σ = 15·3 + 20.5·2 + 18·3.5 = 149 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·5.5 = 53.96 kPa

Effective stress

σ′ = σ − u = 149 − 53.96 = 95.04 kPa

Answer

σ′ = 95.04 kPa
15.Consolidation settlement

Answer: S = 7.011 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 = 95 + 30 = 125 kPa ≤ 195 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.04·2.5/(1 + 0.7)·log₁₀(125/95) = 7.011 mm

Answer

S = 7.011 mm
16.Consolidation settlement

Answer: t = 1.646 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 = 3.5 m

Time

t = Tv·Hdr²/cv = 0.403·3.5²/3 = 1.646 years

Answer

t = 1.646 years
17.Hydrostatic force

Answer: F = 79.71 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 = 2 + 2.5/2 = 3.25 m
A = H·b = 2.5·1 = 2.5 m²
gated = 2 mH = 2.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3.25·2.5 = 79.71 kN

Answer

F = 79.71 kN
18.Hydrostatic force

Answer: F = 24.72 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 + 1/2 = 1 m
A = H·b = 1·2 = 2 m²
gated = 0.5 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·1·2 = 24.72 kN

Answer

F = 24.72 kN
19.Pipe friction & head loss

Answer: hf = 0.1631 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) = 0.8²/(2·9.81) = 0.03262 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.015·(50/0.15)·0.8²/(2·9.81) = 0.1631 m

Answer

hf = 0.1631 m
20.Pipe friction & head loss

Answer: Δz = 1.441 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 = 0.02/0.01767 = 1.132 m/s
V²/(2g) = 0.06529 m

Loss coefficients

f·L/D = 0.022·100/0.15 = 14.67
ΣK = 0.5 + 3·0.3 + 5 + 1.0 = 7.4

Total head loss

hf = 14.67·0.06529 = 0.9575 m
hm = 7.4·0.06529 = 0.4831 m
Δz = hf + hm = 1.441 m

Answer

Δz = 1.441 m
21.Open-channel flow (Manning)

Answer: Q = 2.119 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 + 1·0.7)·0.7 = 2.59 m²
P = b + 2y·√(1 + z²) = 3 + 2·0.7·√(1 + 1²) = 4.98 m
R = A/P = 0.5201 m

Velocity

V = (1/0.025)·0.52012/3·0.0011/2 = 0.818 m/s

Flow rate

Q = A·V = 2.59·0.818 = 2.119 m³/s

Answer

Q = 2.119 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.003063 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 = 3.5·1.6 = 5.6 m²
P = b + 2y = 3.5 + 2·1.6 = 6.7 m
R = A/P = 0.8358 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.025·11/(5.6·0.8873) = 0.05534
S = 0.05534² = 0.003063

Answer

S = 0.003063

That is a fall of 3.063 m per kilometre.

23.Pumps & pump power

Answer: Pel = 15.95 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 = 1000·9.81·0.015·62 = 9.123 kW

Shaft power

Pshaft = 9.123/0.65 = 14.04 kW

Electrical power

Pel = 14.04/0.88 = 15.95 kW

Answer

Pel = 15.95 kW
24.Pumps & pump power

Answer: H = 13.04 m

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

Velocity

V = Q/A = 0.05/0.03142 = 1.592 m/s
V²/(2g) = 0.1291 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (33 + 6)·0.1291 = 5.035 m

Pump head

Both surfaces are open and practically at rest, so pressure and velocity terms drop out.

H = Δz + hL = 8 + 5.035 = 13.04 m

Answer

H = 13.04 m
25.Time value of money

Answer: FV = 26641 €

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

Future value

FV = 20 000·(1 + 0.009)32 = 20 000·1.332 = €26 640.80

Answer

FV = €26 640.80
26.Time value of money

Answer: FV = 91126 €

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.

Ordinary annuity factor

((1 + 0.08)17 − 1)/0.08 = 33.75

Annuity due

Each deposit is invested one year longer.

FV = 2 500·33.75·1.08 = €91 125.61

Answer

FV = €91 125.61
27.NPV & IRR

Answer: NPV = 8712 €

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 = −30 000
CF1/(1 + 0.07)1 = 9 000/1.07 = 8 411.21
CF2/(1 + 0.07)2 = 12 000/1.145 = 10 481.26
CF3/(1 + 0.07)3 = 14 000/1.225 = 11 428.17
CF4/(1 + 0.07)4 = 11 000/1.311 = 8 391.85

Add them up

NPV = €8 712.50

Answer

NPV = €8 712.50

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

28.NPV & IRR

Answer: IRR = 27.94 %

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(25%) = 464.00
NPV(30%) = −304.96

Narrow down

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

IRR ≈ 25 + 5·464.00/(464.00 − (−304.96)) = 28.02%
exact: NPV(27.94%) = 0 → IRR = 27.94%

Answer

IRR = 27.94%
29.Normal distribution

Answer: P = 0.6295

Normal distribution: convert a value x to a z-score, z = (x − μ)/σ, which counts standard deviations from the mean. A z-table (or Φ(z)) gives the area to the left of z, which is P(X < x). The area to the right is 1 − Φ(z), and the area between two values is the difference of their two areas.

z-scores

z₁ = (468 − 500)/40 = −0.8
z₂ = (540 − 500)/40 = 1

Area between

P = Φ(1) − Φ(−0.8) = 0.8413 − 0.2119 = 0.6295

Answer

P = 0.6295
30.Normal distribution

Answer: x = 434.2 h

Normal distribution: convert a value x to a z-score, z = (x − μ)/σ, which counts standard deviations from the mean. A z-table (or Φ(z)) gives the area to the left of z, which is P(X < x). The area to the right is 1 − Φ(z), and the area between two values is the difference of their two areas.

z for the percentile

Φ(z) = 0.05 → z = −1.645

Back to x

x = 500 + −1.645·40 = 434.2 h

Answer

x = 434.2 h

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