FE Civil exam practice: cram pack

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

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1Formulas and methods

Beam support reactions

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

Method

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

Truss: method of joints

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

Method

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

Shear force & bending moment

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

Method

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

Beam deflection

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

Column buckling

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

Centroid & second moment of area

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

Effective stress in soil

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

Consolidation settlement

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

Hydrostatic force

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

Pipe friction & head loss

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

Open-channel flow (Manning)

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

Pumps & pump power

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

Time value of money

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

Method

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

NPV & IRR

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

Method

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

Normal distribution

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

Method

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

2Practice problems

1.Beam support reactionsMedium
P1​ = 45 kNP2​ = 15 kNABCRA​ = ?1.5 m1 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 = 45 kN at 1.5 mP2 = 15 kN at 4 m
RA = kN
2.Beam support reactionsHard
w = 2 kN/mP = 25 kNABRA​ = ?RB​4 m2 m3 m1 m

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

L = 10 mP = 25 kN at 6 mw = 2 kN/m from 4 to 9 m
RA = kN
3.Truss: method of jointsMedium
ABBCACACB25 kN5 m1 m2 m

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

span = 5 mheight = 2 mB is 1 m from Avertical load = 25 kN
FBC = kN
4.Truss: method of jointsHard
ABCDEFGH10 kN15 kN35 kN35 kN15 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: 10 kN ↓F: 15 kN ↓F: 35 kN →G: 35 kN ↓H: 15 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
P1​ = 60 kNP2​ = 15 kNABC1 m7 m1.5 m

The beam rests on a pin at A and a roller at B and overhangs B by 1.5 m to the free end C. It carries a point load P1 between the supports and a point load P2 at C. Find the bending moment Mx under the load P1. Use sagging moments positive and upward shear on the left face positive.

L = 9.5 mP1 = 60 kN at 1 mP2 = 15 kN at 9.5 msupports at x = 0 and x = 8 m
Mx = kN·m
6.Shear force & bending momentHard
6 kN/m35 kNABCDEFG2 m2 m2 m2 m2 m2 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.

35 kN @ 12 m6 kN/m, 0–10 m
  1. 1A (x = 0 m)
  2. 2B (x = 2 m)
  3. 3C (x = 4 m)
  4. 4D (x = 6 m)
  5. 5E (x = 8 m)
  6. 6F (x = 10 m)
  7. 7G (x = 12 m)
7.Beam deflectionMedium
P = 10 kNABδ2 m0.5 m

A cantilever of length L is fixed at A and carries a point load P at a distance a = 2 m from A. Find the deflection δB at the free end B.

P = 10 kNa = 2 mL = 2.5 mE = 70 GPa (aluminium)I = 57 × 10⁶ mm⁴
δB = mm
8.Beam deflectionHard
w = 6 kN/mP = 9 kNδL = 6 m

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

P = 9 kNw = 6 kN/mL = 6 mE = 200 GPa (steel)I = 12 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 2.5 m20 × 40 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 = 2.5 mE = 200 GPa (steel)b × h = 20 × 40 mm
Pcr = kN
10.Column bucklingHard
PL = 4 md = 25 mmcross-section

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

L = 4 mE = 200 GPa (steel)d = 25 mm
σcr = MPa
11.Centroid & second moment of areaMedium
200 mm300 mm120 mmØ50xIx​ = ?

A 200 mm × 300 mm plate has a circular hole of diameter 50 mm on its vertical centre line, with its centre 120 mm above the bottom. Find the second moment of area Ix about the horizontal axis through the centroid.

b = 200 mmh = 300 mmd = 50 mmhole centre: y = 120 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
250320188xM = 100 kN·mdimensions in mm

A symmetric I-section has flanges 250 mm wide and 18 mm thick, an overall depth of 320 mm and a web 8 mm thick. It carries a bending moment of 100 kN·m about the axis x. Find the size of the bending stress σj at the junction of the web and the top flange.

B = 250 mmH = 320 mmtf = 18 mmtw = 8 mmM = 100 kN·m
σj = MPa
13.Effective stress in soilMedium
sandγd​ = 17 kN/m³γsat​ = 18.5 kN/m³14 mwater tableXz = 13 m

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

z = 13 mzw = 3 mγw = 9.81 kN/m³sand: γd = 17 kN/m³sand: γsat = 18.5 kN/m³
u = kPa
14.Effective stress in soilHard
sandγd​ = 15 kN/m³γsat​ = 20.5 kN/m³5 mclayγsat​ = 18 kN/m³4 mwater tableXz = 7 m

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

z = 7 mzw = 1 mγw = 9.81 kN/m³sand: γd = 15 kN/m³sand: γsat = 20.5 kN/m³clay: γsat = 18 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 40 kPasandclayCc​ = 0.35, Cr​ = 0.05e0​ = 1.15σ′0​ = 95 kPaσ′p​ = 145 kPa7.5 mwater table

A 7.5 m thick overconsolidated clay layer has Cc = 0.35, Cr = 0.05 and e₀ = 1.15. At its mid-depth the effective vertical stress is 95 kPa and the preconsolidation pressure is 145 kPa. A new building adds 40 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 7.5 mCc = 0.35Cr = 0.05e0 = 1.15σ′0 = 95 kPaσ′p = 145 kPaΔσ = 40 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 7 mcv​ = 1.5 m²/year7 mimpervious rockwater table

A clay layer 7 m thick has a coefficient of consolidation cv = 1.5 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 = 7 mcv = 1.5 m²/yearU = 70%Tv = 0.403single drainage
t = years
17.Hydrostatic forceMedium
gated = 1 mH = 1.5 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of water, with its top edge 1 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 1 mH = 1.5 mb = 1.5 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 1 mH = 2 m

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

d = 1 mH = 2 mb = 1 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
Q = 4 L/sD = 75 mmL = 200 mf = 0.03

Water flows at 4 L/s through a pipe 200 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 friction head loss hf.

Q = 4 L/sL = 200 mD = 75 mmf = 0.03g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 10Δz = ?L = 300 m, D = 300 mm, f = 0.0254× bend (K = 0.3)

Two open reservoirs are joined by a pipe 300 m long with an inside diameter of 300 mm and a Darcy friction factor f = 0.025. The minor losses are a square-edged entrance (K = 0.5), 4 bends (K = 0.3 each), a valve (K = 10) 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 100 L/s?

Q = 100 L/sL = 300 mD = 300 mmf = 0.025Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 10Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
b = 5 my = 2 mn = 0.03, S = 0.001

A rectangular grass-lined earth channel is 5 m wide. Water flows uniformly 2 m deep. Manning n = 0.03 and the bed slope is S = 0.001. Find the flow rate Q in m³/s.

b = 5 my = 2 mn = 0.03S = 0.001
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 6 my = 2.4 m3 : 1n = 0.015, Q = 87 m³/s

A trapezoidal brickwork channel with a bottom width of 6 m and side slopes of 3:1 (horizontal:vertical) must carry 87 m³/s in uniform flow at a depth of 2.4 m. Manning n = 0.015. Find the required bed slope S (in m/m).

Q = 87 m³/sb = 6 my = 2.4 mz = 3n = 0.015
S = m/m
23.Pumps & pump powerMedium
PQ = 15 L/sH = 32 m

A pump with an efficiency of 85% delivers 15 L/s of water (ρ = 1000 kg/m³) against a head of 32 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 15 L/sH = 32 mη = 85%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
PQ = 50 L/sΔz = 38 mL = 300 m, D = 150 mm, f = 0.025, ΣK = 8

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 38 m higher. The pipe is 300 m long with an inside diameter of 150 mm and a Darcy friction factor f = 0.025; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 65%. Find the shaft power Pshaft in kW.

Q = 50 L/sΔz = 38 mL = 300 mD = 150 mmf = 0.025ΣK = 8η = 65%
Pshaft = kW
25.Time value of moneyMedium
years0123…15€10 000FV = ?

You invest €10 000 at 2% per year with continuous compounding. Find the value FV after 15 years.

PV = €10 000r = 2%t = 15
FV = €
26.Time value of moneyHard
months0123…360€150 000A?AAA

A loan of €150 000 is repaid with equal monthly payments over 30 years. The interest rate is 2.4% per year, compounded monthly. Find the monthly payment A.

P = €150 0002.4% / 12N = 360
A = €
27.NPV & IRRMedium
years012345€30 000€2 000€2 000€2 000€2 000€2 000r = 6%, EAC = ?

A machine costs €30 000 today, lasts 5 years and costs €2 000 per year to run (paid at the end of each year). The cost of capital is 6%. Find its equivalent annual cost EAC.

C0 = €30 000M = €2 000n = 5r = 6%
EAC = €
28.NPV & IRRHard
years0123…9−50 0006 5006 5006 5006 500

An investment of €50 000 returns €6 500 at the end of each year for 9 years. Find its internal rate of return IRR in percent.

C0 = €50 000CF = €6 500n = 9
IRR = %
29.Normal distributionMedium
454572P = ?

The battery lifetimes are normally distributed with mean 500 h and standard deviation 40 h. What fraction lies between 454 and 572 h? Give P as a decimal.

μ = 500σ = 40x1 = 454x2 = 572
P =
30.Normal distributionHard
0.04 mm0D − d?

Hole diameters D are normal with mean 25.04 mm and standard deviation 0.015 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 = 25.04 mm, σ = 0.015 mmshaft: μ = 25 mm, σ = 0.02 mm
P =

3Solutions

1.Beam support reactions

Answer: RA = 9 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 = 45·1.5 + 15·4
RB = 127.5/2.5 = 51 kN

Vertical equilibrium

RA = 45 + 15 − 51 = 9 kN

Answer

RA = 9 kN
2.Beam support reactions

Answer: RA = 13.5 kN

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

w = 2 kN/mP = 25 kNABRA​RB​4 m2 m3 m1 m

Free-body diagram

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

Equilibrium

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

UDL resultant: W = w·ℓ = 2·5 = 10 kN, acting at x̄ = 6.5 m
ΣMA = 0: RB·10 = 25·6 + 2·5·6.5
RB = 215/10 = 21.5 kN
ΣFy = 0: RA = 35 − 21.5 = 13.5 kN

Answer

RA = 13.5 kN
3.Truss: method of joints

Answer: FBC = −11.18 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.

ABBCACACB25 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·5 = 25·1 → Cy = 5 kN
ΣFy = 0: Ay = 25 − 5 = 20 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 = 2/4.472 = 0.4472, cos γ = 4/4.472 = 0.8944
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −5/0.4472 = −11.18 kN

Answer

FBC = −11.18 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: 66.25 kN (T), BC: 72.5 kN (T), CD: 72.5 kN (T), DE: 43.75 kN (T), FG: 66.25 kN (C), GH: 43.75 kN (C), AF: 44.19 kN (C), HE: 61.87 kN (C), BF: 16.25 kN (T), CG: 0, DH: 28.75 kN (T), BG: 8.839 kN (C), DG: 40.66 kN (C)

Answer

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

Answer: Mx = 49.69 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. The overhang load also acts about A.

ΣMA = 0: RB·8 = 60·1 + 15·9.5
RB = 202.5/8 = 25.31 kN
ΣFy = 0: RA = 75 − 25.31 = 49.69 kN

Cut under P1 and keep the left part

Mx = RA·1 = 49.69·1 = 49.69 kN·m

Answer

Mx = 49.69 kN·m
6.Shear force & bending moment

Answer: F (x = 10 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 = 23 kN, R2 = 72 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 = 34, MC = 44, MD = 30, ME = −8, MF = −70 kN·m, MG = 0

Answer

Mark F: MF = −70 kN·m
7.Beam deflection

Answer: δB = 9.19 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 = 10000 N, a = 2000 mm, L = 2500 mm
EI = 3.99 × 10¹² N·mm²

Deflection at the free end

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

δP = Pa³/(3EI) = 6.683 mm
θP = Pa²/(2EI) = 0.005013 rad
δB = δP + θP·(L − a) = Pa²(3L − a)/(6EI) = 9.19 mm

Answer

δB = 9.19 mm
8.Beam deflection

Answer: δmax = 59.06 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 = 9000 N, w = 6 N/mm, L = 6000 mm, EI = 2.4 × 10¹² N·mm²

Each load on its own

δP = PL³/(48EI) = 9000·6000³/(48·2.4 × 10¹²) = 16.88 mm
δw = 5wL⁴/(384EI) = 5·6·6000⁴/(384·2.4 × 10¹²) = 42.19 mm

Add them

δmax = 16.88 + 42.19 = 59.06 mm

Answer

δmax = 59.06 mm
9.Column buckling

Answer: Pcr = 8.422 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 rectangle buckles about its weak axis, using the smaller dimension cubed.

Imin = h·b³/12 = 40·20³/12 = 26667 mm⁴

Effective length

KL = 1·2500 = 2500 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·26667/2500² = 8422 N = 8.422 kN

Answer

Pcr = 8.422 kN
10.Column buckling

Answer: σcr = 9.835 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·25⁴/64 = 19175 mm⁴

Radius of gyration and slenderness

A = 490.9 mm²
r = √(I/A) = √(19175/490.9) = 6.25 mm
KL = 0.7·4000 = 2800 mm
KL/r = 2800/6.25 = 448

Critical stress

σcr = π²E/(KL/r)² = π²·200000/448² = 9.835 MPa

Answer

σcr = 9.835 MPa
11.Centroid & second moment of area

Answer: Ix = 447.9 × 10⁶ mm⁴

Sections with holes: treat a hole as a negative area. The centroid is ȳ = (A₁y₁ − A₂y₂)/(A₁ − A₂), with A₁, y₁ for the full plate and A₂, y₂ for the hole. For the second moment of area about the centroidal axis, use the parallel-axis theorem for each part and subtract the hole: I = (Ic1 + A₁d₁²) − (Ic2 + A₂d₂²), where d is the distance from each part's own centroid to the axis through ȳ. A rectangle has Ic = bh³/12 and a circle Ic = πd⁴/64.

Centroid

ȳ = (60000·150 − 1963·120)/(60000 − 1963) = 151 mm

Full plate about ȳ

200·300³/12 + 60000·−1.015² = 450.1 × 10⁶ mm⁴

Hole about ȳ

π·50⁴/64 + 1963·−31.01² = 2.196 × 10⁶ mm⁴

Subtract

Ix = 447.9 × 10⁶ mm⁴

Answer

Ix = 447.9 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σj = 64.33 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 = 320 − 2·18 = 284 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (250·320³ − 242·284³)/12
Ix = 2.207 × 10⁸ mm⁴

Bending stress

y = 160 − 18 = 142 mm
σ = M·y/I = 1 × 10⁸·142/2.207 × 10⁸ = 64.33 MPa

Answer

σj = 64.33 MPa
13.Effective stress in soil

Answer: u = 98.1 kPa

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

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·10 = 98.1 kPa

Answer

u = 98.1 kPa
14.Effective stress in soil

Answer: σ′ = 74.14 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·2
σ = 15·1 + 20.5·4 + 18·2 = 133 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·6 = 58.86 kPa

Effective stress

σ′ = σ − u = 133 − 58.86 = 74.14 kPa

Answer

σ′ = 74.14 kPa
15.Consolidation settlement

Answer: S = 26.62 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 + 40 = 135 kPa ≤ 145 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.05·7.5/(1 + 1.15)·log₁₀(135/95) = 26.62 mm

Answer

S = 26.62 mm
16.Consolidation settlement

Answer: t = 13.16 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 = 7 m

Time

t = Tv·Hdr²/cv = 0.403·7²/1.5 = 13.16 years

Answer

t = 13.16 years
17.Hydrostatic force

Answer: F = 38.63 kN

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

Centroid depth and area

yc = d + H/2 = 1 + 1.5/2 = 1.75 m
A = H·b = 1.5·1.5 = 2.25 m²
gated = 1 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·1.75·2.25 = 38.63 kN

Answer

F = 38.63 kN
18.Hydrostatic force

Answer: F = 39.24 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 + 2/2 = 2 m
A = H·b = 2·1 = 2 m²
gated = 1 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·2·2 = 39.24 kN

Answer

F = 39.24 kN
19.Pipe friction & head loss

Answer: hf = 3.343 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 = 0.004/0.004418 = 0.9054 m/s

Velocity head

V²/(2g) = 0.9054²/(2·9.81) = 0.04178 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.03·(200/0.075)·0.9054²/(2·9.81) = 3.343 m

Answer

hf = 3.343 m
20.Pipe friction & head loss

Answer: Δz = 3.846 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 = 0.1/0.07069 = 1.415 m/s
V²/(2g) = 0.102 m

Loss coefficients

f·L/D = 0.025·300/0.3 = 25
ΣK = 0.5 + 4·0.3 + 10 + 1.0 = 12.7

Total head loss

hf = 25·0.102 = 2.55 m
hm = 12.7·0.102 = 1.296 m
Δz = hf + hm = 3.846 m

Answer

Δz = 3.846 m
21.Open-channel flow (Manning)

Answer: Q = 11.31 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·y = 5·2 = 10 m²
P = b + 2y = 5 + 2·2 = 9 m
R = A/P = 1.111 m

Velocity

V = (1/0.03)·1.1112/3·0.0011/2 = 1.131 m/s

Flow rate

Q = A·V = 10·1.131 = 11.31 m³/s

Answer

Q = 11.31 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.0009919 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 + z·y)·y = (6 + 3·2.4)·2.4 = 31.68 m²
P = b + 2y·√(1 + z²) = 6 + 2·2.4·√(1 + 3²) = 21.18 m
R = A/P = 1.496 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.015·87/(31.68·1.308) = 0.03149
S = 0.03149² = 0.0009919

Answer

S = 0.0009919

That is a fall of 0.9919 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 5.54 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 = 1000·9.81·0.015·32 = 4.709 kW

Shaft power

Pshaft = Ph/η = 4.709/0.85 = 5.54 kW

Answer

Pshaft = 5.54 kW
24.Pumps & pump power

Answer: Pshaft = 46.53 kW

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

Velocity

V = Q/A = 0.05/0.01767 = 2.829 m/s
V²/(2g) = 0.408 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (50 + 8)·0.408 = 23.67 m

Pump head

H = Δz + hL = 38 + 23.67 = 61.67 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.05·61.67/0.65 = 46.53 kW

Answer

Pshaft = 46.53 kW
25.Time value of money

Answer: FV = 13499 €

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.

Exponent

r·t = 0.02·15 = 0.3
e0.3 = 1.35

Future value

FV = 10 000·1.35 = €13 498.59

Answer

FV = €13 498.59
26.Time value of money

Answer: A = 584.9 €

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

Monthly rate and number of payments

i = 0.024/12 = 0.002
N = 12·30 = 360

Payment

The present value of N equal payments A is A·(1 − (1 + i)⁻ᴺ)/i. Set it equal to the loan and solve for A.

(1 + i)−N = 0.4871
A = 150 000·0.002/(1 − 0.4871) = €584.91

Answer

A = €584.91
27.NPV & IRR

Answer: EAC = 9122 €

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 − 1.06−5)/0.06 = 4.212

Annualised purchase price

30 000/4.212 = 7 121.89

EAC

EAC = 7 121.89 + 2 000 = €9 121.89

Answer

EAC = €9 121.89
28.NPV & IRR

Answer: IRR = 3.261 %

Net present value: discount every cash flow back to today with the required rate of return r, then add them up: NPV = Σ CFₜ/(1 + r)ᵗ. A project with NPV > 0 earns more than r and adds value. The internal rate of return (IRR) is the rate at which NPV = 0.

Required annuity factor

(1 − (1 + i)−9)/i = 50 000/6 500 = 7.692

Solve for the rate

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

i = 3%: 7.786
i = 4%: 7.435
IRR = 3.261%

Answer

IRR = 3.261%
29.Normal distribution

Answer: P = 0.839

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 = (454 − 500)/40 = −1.15
z₂ = (572 − 500)/40 = 1.8

Area between

P = Φ(1.8) − Φ(−1.15) = 0.9641 − 0.1251 = 0.839

Answer

P = 0.839
30.Normal distribution

Answer: P = 0.9452

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 = 25.04 − 25 = 0.04 mm, σ = 0.025 mm

Standardise

z = (0 − 0.04)/0.025 = −1.6

Probability

P = 1 − Φ(−1.6) = 0.9452

Answer

P = 0.9452

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