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​ = 10 kNABCRA​ = ?2 m1 m2 m

The beam has a pin at A and a roller at B, 3 m from A, and overhangs B to the free end C. Find the vertical reaction RA, taking upward as positive.

AB = 3 mAC = 5 mP1 = 30 kN at 2 mP2 = 10 kN at 5 m
RA = kN
2.Beam support reactionsHard
w = 3 kN/mP = 40 kNABCRB​ = ?2.5 m1 m1 m1.5 m

The beam has a pin at A and a roller at B, 4.5 m from A, and overhangs B to the free end C. It carries a point load P at 2.5 m from A and a uniformly distributed load w from 3.5 m to the free end at 6 m. Find the vertical reaction RB, taking upward as positive.

AB = 4.5 mAC = 6 mP = 40 kN at 2.5 mw = 3 kN/m from 3.5 to 6 m
RB = kN
3.Truss: method of jointsMedium
ABCDEFGH40 kN25 kN40 kN30 kN4 × 4 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: 25 kN ↓D: 40 kN ↓F: 30 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 kN25 kN30 kN30 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: 40 kN ↓F: 25 kN ↓G: 30 kN ↓H: 30 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
12 kN/m30 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.

30 kN @ 1 m12 kN/m, 2–6 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
40 kN60 kN60 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.

40 kN @ 0 m60 kN @ 6 m60 kN @ 3 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)
7.Beam deflectionMedium
w = 12 kN/mδL = 5 m

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

w = 12 kN/mL = 5 mE = 200 GPa (steel)I = 36 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 2.5 kN/mABδ4 m

A simply supported timber beam of rectangular section, 125 mm wide, carries a uniformly distributed load w over its whole span. Its midspan deflection may not exceed span/300. Find the smallest depth hreq of the section.

w = 2.5 kN/mL = 4 mE = 11 GPa (timber)b = 125 mm
hreq = mm
9.Column bucklingMedium
PL = 3 md = 60 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 = 60 mm
Pcr = kN
10.Column bucklingHard
PL = 4 md = 80 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 = 4 mE = 70 GPa (aluminium)d = 80 mm
σcr = MPa
11.Centroid & second moment of areaMedium
xD = 260d = 248dimensions in mm

A circular tube has outside diameter D = 260 mm and inside diameter d = 248 mm. Find its radius of gyration r about the horizontal centroidal axis.

D = 260 mmd = 248 mm
r = mm
12.Centroid & second moment of areaHard
2305001814xM = 200 kN·mdimensions in mm

A symmetric I-section has flanges 230 mm wide and 18 mm thick, an overall depth of 500 mm and a web 14 mm thick. It carries a bending moment of 200 kN·m about the axis x. Find the size of the maximum bending stress σmax in the section.

B = 230 mmH = 500 mmtf = 18 mmtw = 14 mmM = 200 kN·m
σmax = MPa
13.Effective stress in soilMedium
sandγd​ = 16.5 kN/m³γsat​ = 19 kN/m³7 mwater tableXz = 4 m

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

z = 4 mzw = 1 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 19 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 16.5 kN/m³γsat​ = 18.5 kN/m³5 mclayγsat​ = 18 kN/m³6 mwater tableXz = 8 m

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

z = 8 mzw = 1 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 18.5 kN/m³clay: γsat = 18 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 250 kPasandclayCc​ = 0.25, Cr​ = 0.03e0​ = 0.6σ′0​ = 115 kPaσ′p​ = 215 kPa3 mwater table

A 3 m thick overconsolidated clay layer has Cc = 0.25, Cr = 0.03 and e₀ = 0.6. At its mid-depth the effective vertical stress is 115 kPa and the preconsolidation pressure is 215 kPa. A new building adds 250 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 3 mCc = 0.25Cr = 0.03e0 = 0.6σ′0 = 115 kPaσ′p = 215 kPaΔσ = 250 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 10 m10 msandwater table

In a laboratory oedometer test, a clay specimen 19 mm thick, drained at the top and bottom, reaches 50% consolidation in 5 min. In the field the same clay forms a layer 10 m thick. It lies between two sand layers, so water drains out at the top and the bottom. How many days t does the field layer take to reach 50% consolidation?

hlab = 19 mmtlab = 5 minH = 10 mfield: double drainage
t = days
17.Hydrostatic forceMedium
gated = 2 mH = 1.5 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 = 1.5 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 4 mH = 3 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of glycerin, with its top edge 4 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 4 mH = 3 mb = 1.5 mρ = 1260 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
V = 2.5 m/sD = 75 mmL = 1000 mf = 0.03

Water (ρ = 1000 kg/m³) flows at 2.5 m/s through a horizontal pipe, 1000 m long, with an inside diameter of 75 mm. Use the Darcy friction factor f = 0.03 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 2.5 m/sL = 1000 mD = 75 mmf = 0.03ρ = 1000 kg/m³
Δp = kPa
20.Pipe friction & head lossHard
K = 5Δz = ?L = 100 m, D = 250 mm, f = 0.0253× bend (K = 0.3)

Two open reservoirs are joined by a pipe 100 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.025. 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 120 L/s?

Q = 120 L/sL = 100 mD = 250 mmf = 0.025Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 5Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
b = 3 my = 1.5 m1.5 : 1n = 0.015, S = 0.005

A trapezoidal brickwork channel has a bottom width of 3 m and side slopes of 1.5:1 (horizontal:vertical). Water flows uniformly 1.5 m deep. Manning n = 0.015 and the bed slope is S = 0.005. Find the flow rate Q in m³/s.

b = 3 my = 1.5 mz = 1.5n = 0.015S = 0.005
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 2 my = 2 mn = 0.022, Q = 3.1 m³/s

A rectangular clean earth channel 2 m wide must carry 3.1 m³/s in uniform flow at a depth of 2 m. Manning n = 0.022. Find the required bed slope S (in m/m).

Q = 3.1 m³/sb = 2 my = 2 mn = 0.022
S = m/m
23.Pumps & pump powerMedium
PQ = 50 L/sH = 50 m

A pump delivers 50 L/s of water (ρ = 1000 kg/m³) against a head of 50 m. The pump efficiency is 70% and the electric motor driving it has an efficiency of 92%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 50 L/sH = 50 mηpump = 70%ηmotor = 92%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
PQ = 120 L/sΔz = 15 mL = 200 m, D = 250 mm, f = 0.025, ΣK = 6

A pump moves 120 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 15 m higher. The pipe is 200 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.025; the minor-loss coefficients add up to ΣK = 6 (entrance and exit included). Use g = 9.81 m/s². Find the head H the pump must add.

Q = 120 L/sΔz = 15 mL = 200 mD = 250 mmf = 0.025ΣK = 6
H = m
25.Time value of moneyMedium
years0123…9PV = ?€6 000+1%+1%…r = 7%

A property is expected to earn net rent of €6 000 next year. The rent is expected to grow by 1% per year forever. The required return is 7% per year. Find the value PV of the property today.

C1 = €6 000g = 1%r = 7%
PV = €
26.Time value of moneyHard
years01234567€2 000€2 000€2 000FV = ?

You deposit €2 000 at the start of every year for 7 years, the first deposit today. The account pays 6% per year. How much is in the account at the end of year 7? Find FV.

A = €2 000i = 6%n = 7
FV = €
27.NPV & IRRMedium
years0123456€40 000€1 500€1 500€1 500€1 500€1 500€1 500r = 6%, EAC = ?

A machine costs €40 000 today, lasts 6 years and costs €1 500 per year to run (paid at the end of each year). The cost of capital is 6%. Find its equivalent annual cost EAC.

C0 = €40 000M = €1 500n = 6r = 6%
EAC = €
28.NPV & IRRHard
years0123−40 00018 00013 00012 000

A project costs €40 000 and returns €18 000, €13 000, €12 000 at the end of years 1 to 3. Cash flows can be reinvested at the cost of capital of 6%. Find the modified internal rate of return MIRR in percent.

r = 6%CF0 = −40 000CF1 = 18 000CF2 = 13 000CF3 = 12 000
MIRR = %
29.Normal distributionMedium
−3−2−10123zshaded area to the right of z = 0.9406

Drag z so that the shaded area under the standard normal curve, to the right of z, is 0.9406. Find z to two decimals.

A = 0.9406
z =
30.Normal distributionHard
0.05 mm0D − d?

Hole diameters D are normal with mean 25.05 mm and standard deviation 0.02 mm. Shaft diameters d are independent and normal with mean 25 mm and standard deviation 0.02 mm. A randomly chosen shaft fits when D − d > 0. Find the probability P that it fits. Round z to two decimals.

hole: μ = 25.05 mm, σ = 0.02 mmshaft: μ = 25 mm, σ = 0.02 mm
P =

3Solutions

1.Beam support reactions

Answer: RA = 3.333 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·3 = 30·2 + 10·5
RB = 110/3 = 36.67 kN

Vertical equilibrium

RA = 30 + 10 − 36.67 = 3.333 kN

Answer

RA = 3.333 kN
2.Beam support reactions

Answer: RB = 30.14 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 = 3·2.5 = 7.5 kN, x̄ = (3.5 + 6)/2 = 4.75 m

Equilibrium

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

ΣMA = 0: RB·4.5 = 40·2.5 + 7.5·4.75
RB = 135.6/4.5 = 30.14 kN
RA = 47.5 − 30.14 = 17.36 kN

Answer

RB = 30.14 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: 100 kN (T), BC: 100 kN (T), CD: 80 kN (T), DE: 80 kN (T), FG: 106.7 kN (C), GH: 106.7 kN (C), AF: 125 kN (C), HE: 100 kN (C), BF: 40 kN (T), CG: 0, DH: 40 kN (T), FC: 8.333 kN (T), HC: 33.33 kN (T)

Answer

Zero-force member: CG
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: 25.31 kN (T), BC: 31.87 kN (T), CD: 31.87 kN (T), DE: 15.94 kN (T), FG: 55.31 kN (C), GH: 45.94 kN (C), AF: 92.19 kN (C), HE: 26.56 kN (C), BF: 48.75 kN (T), CG: 0, DH: 21.25 kN (T), BG: 10.94 kN (C), DG: 26.56 kN (C)

Answer

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

Answer: D (x = 3 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 = 41 kN, R2 = 37 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 = 41, MC = 52, MD = 57 kN·m, ME = 50, MF = 31, MG = 0

Answer

Mark D: MD = 57 kN·m
6.Shear force & bending moment

Answer: E (x = 4 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 = 33.33 kN, R2 = 126.7 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 = −40, MC = −46.67, MD = −53.33, ME = −120 kN·m, MF = −60, MG = 0

Answer

Mark E: ME = −120 kN·m
7.Beam deflection

Answer: δmax = 13.56 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 = 12 N/mm, L = 5000 mm
EI = 7.2 × 10¹² N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·12·5000⁴/(384·7.2 × 10¹²) = 13.56 mm

Answer

δmax = 13.56 mm
8.Beam deflection

Answer: hreq = 176 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 = 2.5 N/mm, L = 4000 mm, E = 11000 N/mm²

Deflection limit

δallow = L/300 = 4000/300 = 13.33 mm

Required second moment of area

Ireq = 5wL⁴/(384·E·δallow) = 5·2.5·4000⁴/(384·11000·13.33) = 5.682 × 10⁷ mm⁴

Required depth

bh³/12 = Ireq → h = (12·5.682 × 10⁷/125)1/3 = 176 mm

Answer

hreq = 176 mm

In practice, choose the next standard depth above this value.

9.Column buckling

Answer: Pcr = 48.83 kN

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

Smallest second moment of area

A round section has the same I about every axis.

I = πd⁴/64 = π·60⁴/64 = 636173 mm⁴

Effective length

KL = 1·3000 = 3000 mm

Critical load

Pcr = π²EI/(KL)² = π²·70000·636173/3000² = 48835 N = 48.83 kN

Answer

Pcr = 48.83 kN
10.Column buckling

Answer: σcr = 17.27 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·80⁴/64 = 2.011 × 10⁶ mm⁴

Radius of gyration and slenderness

A = 5027 mm²
r = √(I/A) = √(2.011 × 10⁶/5027) = 20 mm
KL = 1·4000 = 4000 mm
KL/r = 4000/20 = 200

Critical stress

σcr = π²E/(KL/r)² = π²·70000/200² = 17.27 MPa

Answer

σcr = 17.27 MPa
11.Centroid & second moment of area

Answer: r = 89.83 mm

Second moment of area: for a rectangle about its own centroidal axis I = bh³/12, and about its base bh³/3 (parallel-axis theorem I = Ic + A·d²). A hole is handled by subtracting its I, as long as both parts share the same axis. The elastic section modulus is S = I/c, where c is the distance to the extreme fibre. The radius of gyration r = √(I/A) is the distance at which the whole area would give the same I; it is used in column buckling.

Net area and second moment of area

A = π(D² − d²)/4 = 4788 mm²
I = π(D⁴ − d⁴)/64 = 3.863 × 10⁷ mm⁴

Radius of gyration

r = √(I/A) = √(3.863 × 10⁷/4788) = 89.83 mm

Answer

r = 89.83 mm
12.Centroid & second moment of area

Answer: σmax = 83.66 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 = 500 − 2·18 = 464 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (230·500³ − 216·464³)/12
Ix = 5.977 × 10⁸ mm⁴

Bending stress

y = 250 mm
σ = M·y/I = 2 × 10⁸·250/5.977 × 10⁸ = 83.66 MPa

Answer

σmax = 83.66 MPa
13.Effective stress in soil

Answer: σ′ = 44.07 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) = 16.5·1 + 19·3 = 73.5 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·3 = 29.43 kPa

Effective stress

σ′ = σ − u = 73.5 − 29.43 = 44.07 kPa

Answer

σ′ = 44.07 kPa
14.Effective stress in soil

Answer: σ′ = 75.83 kPa

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

Total stress

Add the weight of each soil band above X. Above the water table use the dry unit weight, below it the saturated one.

σ = γd·1 + γsat,sand·4 + γsat,clay·3
σ = 16.5·1 + 18.5·4 + 18·3 = 144.5 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·7 = 68.67 kPa

Effective stress

σ′ = σ − u = 144.5 − 68.67 = 75.83 kPa

Answer

σ′ = 75.83 kPa
15.Consolidation settlement

Answer: S = 123 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 = 115 + 250 = 365 kPa > 215 kPa

Settlement

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

S = 0.03·3/(1 + 0.6)·log₁₀(215/115) + 0.25·3/(1 + 0.6)·log₁₀(365/215)
S = 15.29 + 107.7 = 123 mm

Answer

S = 123 mm
16.Consolidation settlement

Answer: t = 961.8 days

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 paths

Hdr,lab = 19/2 = 9.5 mm = 0.0095 m
Hdr,field = 10/2 = 5 m

Scale the time

t = Tv·Hdr²/cv with the same T_v and cv in the lab and the field.

tfield = 5·(5/0.0095)² = 1.385 × 10⁶ min
tfield = 1.385 × 10⁶/1440 = 961.8 days

Answer

t = 961.8 days
17.Hydrostatic force

Answer: F = 40.47 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 = 1.5·1 = 1.5 m²
gated = 2 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2.75·1.5 = 40.47 kN

Answer

F = 40.47 kN
18.Hydrostatic force

Answer: F = 305.9 kN

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

Centroid depth and area

yc = d + H/2 = 4 + 3/2 = 5.5 m
A = H·b = 3·1.5 = 4.5 m²
gated = 4 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·5.5·4.5 = 305.9 kN

Answer

F = 305.9 kN
19.Pipe friction & head loss

Answer: Δp = 1250 kPa

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.

Head loss

hf = f·(L/D)·V²/(2g) = 0.03·(1000/0.075)·2.5²/(2·9.81) = 127.4 m

Pressure drop

The pipe is horizontal and the velocity does not change, so the energy equation reduces to Δp = ρ·g·hf.

Δp = ρ·g·hf = 1000·9.81·127.4 = 1.25 × 10⁶ Pa = 1250 kPa

Answer

Δp = 1250 kPa
20.Pipe friction & head loss

Answer: Δz = 5.3 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 = 0.12/0.04909 = 2.445 m/s
V²/(2g) = 0.3046 m

Loss coefficients

f·L/D = 0.025·100/0.25 = 10
ΣK = 0.5 + 3·0.3 + 5 + 1.0 = 7.4

Total head loss

hf = 10·0.3046 = 3.046 m
hm = 7.4·0.3046 = 2.254 m
Δz = hf + hm = 5.3 m

Answer

Δz = 5.3 m
21.Open-channel flow (Manning)

Answer: Q = 35.54 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 + 1.5·1.5)·1.5 = 7.875 m²
P = b + 2y·√(1 + z²) = 3 + 2·1.5·√(1 + 1.5²) = 8.408 m
R = A/P = 0.9366 m

Velocity

V = (1/0.015)·0.93662/3·0.0051/2 = 4.513 m/s

Flow rate

Q = A·V = 7.875·4.513 = 35.54 m³/s

Answer

Q = 35.54 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.0004992 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 = 2·2 = 4 m²
P = b + 2y = 2 + 2·2 = 6 m
R = A/P = 0.6667 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.022·3.1/(4·0.7631) = 0.02234
S = 0.02234² = 0.0004992

Answer

S = 0.0004992

That is a fall of 0.4992 m per kilometre.

23.Pumps & pump power

Answer: Pel = 38.08 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 = 1000·9.81·0.05·50 = 24.52 kW

Shaft power

Pshaft = 24.52/0.7 = 35.04 kW

Electrical power

Pel = 35.04/0.92 = 38.08 kW

Answer

Pel = 38.08 kW
24.Pumps & pump power

Answer: H = 22.92 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 = 0.12/0.04909 = 2.445 m/s
V²/(2g) = 0.3046 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (20 + 6)·0.3046 = 7.919 m

Pump head

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

H = Δz + hL = 15 + 7.919 = 22.92 m

Answer

H = 22.92 m
25.Time value of money

Answer: PV = 100000 €

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

Growing perpetuity

PV = C1/(r − g) = 6 000/(0.07 − 0.01) = 6 000/0.06 = €100 000.00

Answer

PV = €100 000.00
26.Time value of money

Answer: FV = 17795 €

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 + 0.06)7 − 1)/0.06 = 8.394

Annuity due

Each deposit is invested one year longer.

FV = 2 000·8.394·1.06 = €17 794.94

Answer

FV = €17 794.94
27.NPV & IRR

Answer: EAC = 9635 €

Equivalent annual cost: spread the present value of all costs over the life as an equal yearly amount (an annuity): EAC = PV·r/(1 − (1 + r)⁻ⁿ). It lets you compare machines with different lives.

Annuity factor

(1 − 1.06−6)/0.06 = 4.917

Annualised purchase price

40 000/4.917 = 8 134.51

EAC

EAC = 8 134.51 + 1 500 = €9 634.51

Answer

EAC = €9 634.51
28.NPV & IRR

Answer: MIRR = 4.773 %

Modified IRR: compound every inflow forward to the end of the project at the reinvestment rate (usually the cost of capital) to get the terminal value TV. MIRR is the rate that turns the initial investment into TV: MIRR = (TV/C₀)^(1/n) − 1.

Terminal value of the inflows

18 000·1.062 = 20 224.80
13 000·1.061 = 13 780.00
12 000·1.060 = 12 000.00
TV = 46 004.80

MIRR

MIRR = (46 004.80/40 000)1/3 − 1 = 4.773%

Answer

MIRR = 4.773%
29.Normal distribution

Answer: z = −1.56

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 − 0.9406 = 0.0594

Read the z-table backwards

Find 0.0594 inside the table and read off z.

z = −1.56

Answer

z = −1.56
30.Normal distribution

Answer: P = 0.9616

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 = 25.05 − 25 = 0.05 mm, σ = 0.02828 mm

Standardise

z = (0 − 0.05)/0.02828 = −1.77

Probability

P = 1 − Φ(−1.77) = 0.9616

Answer

P = 0.9616

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