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
w0​ = 4 kN/mABRB​ = ?10 m

The simply supported beam (pin at A, roller at B) carries a linearly varying load that rises from zero at A to 4 kN/m at B. Find the vertical support reaction RB.

L = 10 mw0 = 4 kN/m
RB = kN
2.Beam support reactionsHard
w = 4 kN/mP = 80 kNABCRB​ = ?2 m1 m0.5 m1.5 m

The beam has a pin at A and a roller at B, 3.5 m from A, and overhangs B to the free end C. It carries a point load P at 2 m from A and a uniformly distributed load w from 3 m to the free end at 5 m. Find the vertical reaction RB, taking upward as positive.

AB = 3.5 mAC = 5 mP = 80 kN at 2 mw = 4 kN/m from 3 to 5 m
RB = kN
3.Truss: method of jointsMedium
ABCDEFGH30 kN25 kN20 kN35 kN20 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.

C: 30 kN ↓D: 25 kN ↓F: 20 kN ↓G: 35 kN ↓H: 20 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
ABBCACACB35 kN10 kN6 m2 m4 m

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

span = 6 mheight = 4 mB is 2 m from Avertical load = 35 kNhorizontal load = 10 kN →
FAC = kN
5.Shear force & bending momentMedium
P1​ = 70 kNP2​ = 80 kNAB4 m1 m1 m

The simply supported beam carries two point loads. Find the maximum bending moment Mmax in the beam.

L = 6 mP1 = 70 kN at 4 mP2 = 80 kN at 5 m
Mmax = kN·m
6.Shear force & bending momentHard
w = 10 kN/mP = 10 kNABsection2.5 m2.5 m

Find the bending moment Mx at the section x = 2.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 5 mP = 10 kN at 2.5 mw = 10 kN/m from 0 to 5 mx = 2.5 m
Mx = kN·m
7.Beam deflectionMedium
w = 5 kN/mδL = 2 m

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

w = 5 kN/mL = 2 mE = 200 GPa (steel)I = 12 × 10⁶ mm⁴
δ = mm
8.Beam deflectionHard
w = 1.5 kN/mABδ6 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 = 1.5 kN/mL = 6 mE = 11 GPa (timber)b = 125 mm
hreq = mm
9.Column bucklingMedium
PL = 5 md = 30 mmcross-section

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

L = 5 mE = 200 GPa (steel)d = 30 mm
Pcr = kN
10.Column bucklingHard
PL = 6 md = 80 mmcross-section

A column of length L made of aluminium is fixed at the base and free at the top. Find its slenderness and the critical buckling stress σcr from Euler’s formula.

L = 6 mE = 70 GPa (aluminium)d = 80 mm
σcr = MPa
11.Centroid & second moment of areaMedium
2801522020xdimensions in mm

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

bf = 280 mmtf = 15 mmtw = 20 mmhw = 220 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
1603028020xM = 10 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 10 kN·m. Find the bending stress σbottom at the bottom edge.

bf = 160 mmtf = 30 mmtw = 20 mmhw = 280 mmM = 10 kN·m
σbottom = MPa
13.Effective stress in soilMedium
sandγd​ = 15 kN/m³γsat​ = 20.5 kN/m³9 mwater tableXz = 3 m

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

z = 3 mzw = 2 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 20.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 17 kN/m³γsat​ = 19 kN/m³6 mclayγsat​ = 19 kN/m³8 mwater tableXz = 10 m

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

z = 10 mzw = 5 mγw = 9.81 kN/m³sand: γd = 17 kN/m³sand: γsat = 19 kN/m³clay: γsat = 19 kN/m³
σ = kPa
15.Consolidation settlementMedium
Δσ = 80 kPasandclayCc​ = 0.25, Cr​ = 0.05e0​ = 0.7σ′0​ = 115 kPaσ′p​ = 145 kPa6.5 mwater table

A 6.5 m thick overconsolidated clay layer has Cc = 0.25, Cr = 0.05 and e₀ = 0.7. At its mid-depth the effective vertical stress is 115 kPa and the preconsolidation pressure is 145 kPa. A new building adds 80 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 6.5 mCc = 0.25Cr = 0.05e0 = 0.7σ′0 = 115 kPaσ′p = 145 kPaΔσ = 80 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 5 mcv​ = 5 m²/year5 mimpervious rockwater table

A clay layer 5 m thick has a coefficient of consolidation cv = 5 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 = 5 mcv = 5 m²/yearU = 70%Tv = 0.403single drainage
t = years
17.Hydrostatic forceMedium
gated = 2 mH = 3 m

A vertical rectangular gate 3 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 = 3 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 1 mH = 3 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of water, with its top edge 1 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 1 mH = 3 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
Q = 3 L/sD = 75 mmL = 150 mf = 0.025

Water flows at 3 L/s through a pipe 150 m long with an inside diameter of 75 mm. Use the Darcy friction factor f = 0.025 and g = 9.81 m/s². Find the friction head loss hf.

Q = 3 L/sL = 150 mD = 75 mmf = 0.025g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 5free outletH = ?L = 300 m, D = 150 mm, f = 0.0153× bend (K = 0.3)

A pipe 300 m long with an inside diameter of 150 mm (Darcy friction factor f = 0.015) runs from an open reservoir and discharges as a free jet into the air. The minor losses are a square-edged entrance (K = 0.5), 3 bends (K = 0.3 each) and a valve (K = 5). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 40 L/s?

Q = 40 L/sL = 300 mD = 150 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 5
H = m
21.Open-channel flow (Manning)Medium
D = 450 mmn = 0.013, S = 0.002

A concrete storm sewer with an inside diameter of 450 mm flows just full (as an open channel, not under pressure). Manning n = 0.013 and the slope is S = 0.002. Find the flow rate Q in m³/s.

D = 450 mmn = 0.013S = 0.002
Q = m³/s
22.Open-channel flow (Manning)Hard
D = 250 mmn = 0.013, V = 0.75 m/s

A concrete sewer with an inside diameter of 250 mm (Manning n = 0.013) must reach a self-cleansing velocity of 0.75 m/s when flowing just full. Find the minimum slope S (in m/m).

D = 250 mmn = 0.013V = 0.75 m/s
S = m/m
23.Pumps & pump powerMedium
PQ = 20 L/sH = 58 m

A pump with an efficiency of 82% delivers 20 L/s of water (ρ = 1000 kg/m³) against a head of 58 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 20 L/sH = 58 mη = 82%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 100 L/sΔz = 24 mL = 500 m, D = 250 mm, f = 0.018, ΣK = 8

A pump moves 100 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 24 m higher. The pipe is 500 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.018; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 70%. Find the shaft power Pshaft in kW.

Q = 100 L/sΔz = 24 mL = 500 mD = 250 mmf = 0.018ΣK = 8η = 70%
Pshaft = kW
25.Time value of moneyMedium
years0123456€20 000FV = ?

You invest €20 000 at a nominal rate of 2% per year, compounded monthly. Find the value FV of the investment after 6 years.

PV = €20 0002% / 12n = 6
FV = €
26.Time value of moneyHard
months0123…84€10 000AAAA4.8% / 12, I = ?

A loan of €10 000 is repaid with equal monthly payments over 7 years at 4.8% per year, compounded monthly. How much interest I is paid in total over the life of the loan?

P = €10 0004.8% / 12N = 84
I = €
27.NPV & IRRMedium
years0123…10€60 000€5 000€5 000€5 000€5 000r = 12%, EAC = ?

A machine costs €60 000 today, lasts 10 years and costs €5 000 per year to run (paid at the end of each year). The cost of capital is 12%. Find its equivalent annual cost EAC.

C0 = €60 000M = €5 000n = 10r = 12%
EAC = €
28.NPV & IRRHard
years0123−40 00017 50027 00022 500

A project costs €40 000 and returns €17 500, €27 000, €22 500 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −40 000CF1 = 17 500CF2 = 27 000CF3 = 22 500
IRR = %
29.Normal distributionMedium
750 g769.7 gX + Y?

X is normal with mean 250 g and standard deviation 4 g; Y is independent and normal with mean 500 g and standard deviation 9 g. Find the probability P that X + Y is more than 769.7 g. Round z to two decimals.

μX = 250, σX = 4μY = 500, σY = 9X + Y > 769.7 g
P =
30.Normal distributionHard
10 g0X − Y?

The mass X of a product from line 1 and Y from line 2 are independent and normal: X has mean 500 g and standard deviation 8 g, Y has mean 490 g and standard deviation 6 g. Find the probability P that X is greater than Y. Round z to two decimals.

μX = 500 g, σX = 8 gμY = 490 g, σY = 6 g
P =

3Solutions

1.Beam support reactions

Answer: RB = 13.33 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 triangular load

W = ½·4·10 = 20 kN
x̄ = 2L/3 = 6.667 m

Equilibrium

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

ΣMA = 0: RB·10 = 20·6.667
RB = 13.33 kN
RA = 20 − 13.33 = 6.667 kN

Answer

RB = 13.33 kN
2.Beam support reactions

Answer: RB = 54.86 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 = 4·2 = 8 kN, x̄ = (3 + 5)/2 = 4 m

Equilibrium

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

ΣMA = 0: RB·3.5 = 80·2 + 8·4
RB = 192/3.5 = 54.86 kN
RA = 88 − 54.86 = 33.14 kN

Answer

RB = 54.86 kN
3.Truss: method of joints

Answer: member BF

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 B

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

ΣF⊥ = 0 → FBF = 0

Check with the method of joints

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

AB: 58.75 kN (T), BC: 58.75 kN (T), CD: 71.25 kN (T), DE: 71.25 kN (T), FG: 97.5 kN (C), GH: 97.5 kN (C), AF: 83.09 kN (C), HE: 100.8 kN (C), BF: 0, CG: 35 kN (C), DH: 25 kN (T), FC: 54.8 kN (T), HC: 37.12 kN (T)

Answer

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

Answer: FAC = 18.33 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 kN10 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·6 = 35·2 + 10·4 → Cy = 18.33 kN
ΣFy = 0: Ay = 35 − 18.33 = 16.67 kN
ΣFx = 0: Ax = −10 kN

Joint C

The roller gives only a vertical reaction, so joint C has just two unknown member forces. Assume both in tension.

sin γ = 4/5.657 = 0.7071, cos γ = 4/5.657 = 0.7071
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −18.33/0.7071 = −25.93 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−25.93)·0.7071 = 18.33 kN

Answer

FAC = 18.33 kN (tension)
5.Shear force & bending moment

Answer: Mmax = 146.7 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.

ΣMA = 0: RB·6 = 70·4 + 80·5
RB = 680/6 = 113.3 kN
ΣFy = 0: RA = 150 − 113.3 = 36.67 kN

Moment under each load

Keep the part left of each load.

under P1: M = RA·4 = 36.67·4 = 146.7 kN·m
under P2: M = RB·1 = 113.3·1 = 113.3 kN·m

Largest value

Mmax = 146.7 kN·m (under P1)

Answer

Mmax = 146.7 kN·m
6.Shear force & bending moment

Answer: Mx = 43.75 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 = 10·5 = 50 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 10·2.5 + 10·5·2.5
RB = 150/5 = 30 kN
ΣFy = 0: RA = 60 − 30 = 30 kN
w = 10 kN/mP = 10 kNABRA​ = 30RB​ = 30section2.5 m2.5 m

Cut at x = 2.5 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 = 30·2.5 − 10·2.5·1.25 = 43.75 kN·m

Answer

Mx = 43.75 kN·m
7.Beam deflection

Answer: δ = 4.167 mm

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

Consistent units

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

w = 5 N/mm, L = 2000 mm
EI = 2.4 × 10¹² N·mm²

Deflection

δ = wL⁴/(8EI) = 5·2000⁴/(8·2.4 × 10¹²) = 4.167 mm

Answer

δ = 4.167 mm
8.Beam deflection

Answer: hreq = 222.7 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 = 1.5 N/mm, L = 6000 mm, E = 11000 N/mm²

Deflection limit

δallow = L/300 = 6000/300 = 20 mm

Required second moment of area

Ireq = 5wL⁴/(384·E·δallow) = 5·1.5·6000⁴/(384·11000·20) = 1.151 × 10⁸ mm⁴

Required depth

bh³/12 = Ireq → h = (12·1.151 × 10⁸/125)1/3 = 222.7 mm

Answer

hreq = 222.7 mm

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

9.Column buckling

Answer: Pcr = 3.139 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·30⁴/64 = 39761 mm⁴

Effective length

KL = 1·5000 = 5000 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·39761/5000² = 3139 N = 3.139 kN

Answer

Pcr = 3.139 kN
10.Column buckling

Answer: σcr = 1.919 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 = 2·6000 = 12000 mm
KL/r = 12000/20 = 600

Critical stress

σcr = π²E/(KL/r)² = π²·70000/600² = 1.919 MPa

Answer

σcr = 1.919 MPa
11.Centroid & second moment of area

Answer: Ix = 47.49 × 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 = 280·15 = 4200 mm², yf = 220 + 15/2 = 227.5 mm
web: Aw = 20·220 = 4400 mm², yw = 220/2 = 110 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (4200·227.5 + 4400·110)/8600 = 167.4 mm

Parallel-axis theorem

flange: 280·15³/12 + 4200·(227.5 − 167.4)² = 1.526 × 10⁷ mm⁴
web: 20·220³/12 + 4400·(110 − 167.4)² = 3.224 × 10⁷ mm⁴
Ix = 1.526 × 10⁷ + 3.224 × 10⁷ = 4.749 × 10⁷ mm⁴ = 47.49 × 10⁶ mm⁴

Answer

Ix = 47.49 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σbottom = 21.36 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.

Split into two rectangles

Measure every y from the bottom edge.

flange: Af = 160·30 = 4800 mm², yf = 280 + 30/2 = 295 mm
web: Aw = 20·280 = 5600 mm², yw = 280/2 = 140 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (4800·295 + 5600·140)/10400 = 211.5 mm

Parallel-axis theorem

flange: 160·30³/12 + 4800·(295 − 211.5)² = 3.38 × 10⁷ mm⁴
web: 20·280³/12 + 5600·(140 − 211.5)² = 6.525 × 10⁷ mm⁴
Ix = 3.38 × 10⁷ + 6.525 × 10⁷ = 9.904 × 10⁷ mm⁴

Bending stress

The bottom edge is ȳ from the axis.

y = 211.5 mm
σ = M·y/I = 1 × 10⁷·211.5/9.904 × 10⁷ = 21.36 MPa

Answer

σbottom = 21.36 MPa
13.Effective stress in soil

Answer: σ′ = 40.69 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) = 15·2 + 20.5·1 = 50.5 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·1 = 9.81 kPa

Effective stress

σ′ = σ − u = 50.5 − 9.81 = 40.69 kPa

Answer

σ′ = 40.69 kPa
14.Effective stress in soil

Answer: σ = 180 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·5 + γsat,sand·1 + γsat,clay·4
σ = 17·5 + 19·1 + 19·4 = 180 kPa

Answer

σ = 180 kPa
15.Consolidation settlement

Answer: S = 142.2 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 + 80 = 195 kPa > 145 kPa

Settlement

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

S = 0.05·6.5/(1 + 0.7)·log₁₀(145/115) + 0.25·6.5/(1 + 0.7)·log₁₀(195/145)
S = 19.25 + 123 = 142.2 mm

Answer

S = 142.2 mm
16.Consolidation settlement

Answer: t = 2.015 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 = 5 m

Time

t = Tv·Hdr²/cv = 0.403·5²/5 = 2.015 years

Answer

t = 2.015 years
17.Hydrostatic force

Answer: F = 309 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 + 3/2 = 3.5 m
A = H·b = 3·3 = 9 m²
gated = 2 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3.5·9 = 309 kN

Answer

F = 309 kN
18.Hydrostatic force

Answer: F = 220.7 kN

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

Centroid depth and area

yc = d + H/2 = 1 + 3/2 = 2.5 m
A = H·b = 3·3 = 9 m²
gated = 1 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2.5·9 = 220.7 kN

Answer

F = 220.7 kN
19.Pipe friction & head loss

Answer: hf = 1.175 m

Pipe flow: the Reynolds number Re = V·D/ν = ρ·V·D/μ tells laminar flow (Re below about 2000) from turbulent flow (above about 4000). Friction along a pipe costs the Darcy–Weisbach head loss hf = f·(L/D)·V²/(2g). Fittings, valves, the entrance and the exit add minor losses hm = ΣK·V²/(2g). Between two open reservoir surfaces the energy equation gives Δz = hf + hm, with the exit loss K = 1 included.

Mean velocity

A = π·0.075²/4 = 0.004418 m²
V = Q/A = 0.003/0.004418 = 0.6791 m/s

Velocity head

V²/(2g) = 0.6791²/(2·9.81) = 0.0235 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.025·(150/0.075)·0.6791²/(2·9.81) = 1.175 m

Answer

hf = 1.175 m
20.Pipe friction & head loss

Answer: H = 9.767 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 = 0.04/0.01767 = 2.264 m/s
V²/(2g) = 0.2611 m

Loss coefficients

f·L/D = 0.015·300/0.15 = 30
ΣK = 0.5 + 3·0.3 + 5 = 6.4

Energy equation

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

H = (1 + 30 + 6.4)·0.2611 = 9.767 m

Answer

H = 9.767 m
21.Open-channel flow (Manning)

Answer: Q = 0.1275 m³/s

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

Geometry

A = 0.159 m², R = D/4 = 0.1125 m

Velocity

V = (1/0.013)·0.11252/3·0.0021/2 = 0.8017 m/s

Flow rate

Q = A·V = 0.159·0.8017 = 0.1275 m³/s

Answer

Q = 0.1275 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.003833 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 = 0.25/4 = 0.0625 m

Solve Manning for S

S = (n·V/R2/3)² = (0.013·0.75/0.1575)² = 0.003833

Answer

S = 0.003833

That is a fall of 3.833 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 13.88 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 = 1000·9.81·0.02·58 = 11.38 kW

Shaft power

Pshaft = Ph/η = 11.38/0.82 = 13.88 kW

Answer

Pshaft = 13.88 kW
24.Pumps & pump power

Answer: Pshaft = 46.68 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 = 0.1/0.04909 = 2.037 m/s
V²/(2g) = 0.2115 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (36 + 8)·0.2115 = 9.307 m

Pump head

H = Δz + hL = 24 + 9.307 = 33.31 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.1·33.31/0.7 = 46.68 kW

Answer

Pshaft = 46.68 kW
25.Time value of money

Answer: FV = 22548 €

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

Rate and number of periods

i = r/m = 0.02/12 = 0.001667
N = m·n = 12·6 = 72

Future value

FV = 20 000·(1 + 0.001667)72 = 20 000·1.127 = €22 547.68

Answer

FV = €22 547.68
26.Time value of money

Answer: I = 1794 €

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 payment

i = 0.004, N = 84
A = 10 000·0.004/(1 − (1 + 0.004)−84) = €140.40

Total interest

I = N·A − P = 84·140.4 − 10 000 = €1 793.70

Answer

I = €1 793.70
27.NPV & IRR

Answer: EAC = 15619 €

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 − 1.12−10)/0.12 = 5.65

Annualised purchase price

60 000/5.65 = 10 619.05

EAC

EAC = 10 619.05 + 5 000 = €15 619.05

Answer

EAC = €15 619.05
28.NPV & IRR

Answer: IRR = 29.46 %

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%) = 2 800.00
NPV(30%) = −320.89

Narrow down

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

IRR ≈ 25 + 5·2 800.00/(2 800.00 − (−320.89)) = 29.49%
exact: NPV(29.46%) = 0 → IRR = 29.46%

Answer

IRR = 29.46%
29.Normal distribution

Answer: P = 0.02275

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 sum

μ = 750 g, σ = √(4² + 9²) = 9.849 g

Standardise

z = (769.7 − 750)/9.849 = 2

Upper tail

P = 1 − Φ(2) = 1 − 0.9772 = 0.02275

Answer

P = 0.02275
30.Normal distribution

Answer: P = 0.8413

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 = 500 − 490 = 10 g, σ = 10 g

Standardise

z = (0 − 10)/10 = −1

Probability

P = 1 − Φ(−1) = 0.8413

Answer

P = 0.8413

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