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​ = 15 kNP2​ = 60 kNABRA​RB​ = ?1 m6 m3 m

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

L = 10 mP1 = 15 kN at 1 mP2 = 60 kN at 7 m
RB = kN
2.Beam support reactionsHard
P = 55 kN, 30°Q = 50 kNABα = ?2 m4 m2 m

The simply supported beam has a pin at A and a roller at B. A load P acts at 2 m from A, inclined at 30° to the horizontal, and a vertical load Q acts at 6 m from A. Find the angle α between the total reaction force at the pin A and the horizontal.

L = 8 mP = 55 kN at 2 m, θ = 30°Q = 50 kN at 6 m
α = °
3.Truss: method of jointsMedium
ABBCACACB40 kN6 m4 m3 m

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

span = 6 mheight = 3 mB is 4 m from Avertical load = 40 kN
FBC = kN
4.Truss: method of jointsHard
ABBCACACB40 kN15 kN8 m1 m4 m

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

span = 8 mheight = 4 mB is 1 m from Avertical load = 40 kNhorizontal load = 15 kN →
FAC = kN
5.Shear force & bending momentMedium
w = 3 kN/mABsection2.5 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 mw = 3 kN/m from 0 to 5 mx = 2.5 m
Mx = kN·m
6.Shear force & bending momentHard
w = 10 kN/mP = 35 kNABsection1.5 m2.5 m

Find the bending moment Mx at the section x = 1.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 4 mP = 35 kN at 1.5 mw = 10 kN/m from 0 to 4 mx = 1.5 m
Mx = kN·m
7.Beam deflectionMedium
P = 26 kNABδ2 m1 m

A simply supported beam carries a point load P at a = 2 m from support A. Find the deflection δP under the load.

P = 26 kNa = 2 mL = 3 mE = 200 GPa (steel)I = 57 × 10⁶ mm⁴
δP = mm
8.Beam deflectionHard
w = 10 kN/mδL = 2 m

A simply supported beam carries a uniformly distributed load w. Its deflection may not exceed span/360. Find the smallest second moment of area Ireq that meets this limit.

w = 10 kN/mL = 2 mE = 200 GPa (steel)
Ireq = × 10⁶ mm⁴
9.Column bucklingMedium
PL = 4 md = 80 mmcross-section

A column of length L made of steel is fixed at the base and free at the top. Using Euler’s formula, find its critical buckling load Pcr.

L = 4 mE = 200 GPa (steel)d = 80 mm
Pcr = kN
10.Column bucklingHard
PL = 6 md = 40 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 = 6 mE = 70 GPa (aluminium)d = 40 mm
σcr = MPa
11.Centroid & second moment of areaMedium
1203016010xdimensions in mm

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

bf = 120 mmtf = 30 mmtw = 10 mmhw = 160 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
180302208xM = 40 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 40 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 180 mmtf = 30 mmtw = 8 mmhw = 220 mmM = 40 kN·m
σtop = MPa
13.Effective stress in soilMedium
sandγd​ = 16.5 kN/m³γsat​ = 18.5 kN/m³6 mwater tableXz = 5 m

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

z = 5 mzw = 3 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 18.5 kN/m³
σ′ = kPa
14.Effective stress in soilHard
sandγd​ = 16.5 kN/m³γsat​ = 20.5 kN/m³3 mclayγsat​ = 18 kN/m³5 mwater tableXz = 5.5 m

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

z = 5.5 mzw = 1 mγw = 9.81 kN/m³sand: γd = 16.5 kN/m³sand: γsat = 20.5 kN/m³clay: γsat = 18 kN/m³
σ = kPa
15.Consolidation settlementMedium
Δσ = 150 kPasandclayCc​ = 0.25, Cr​ = 0.05e0​ = 0.65σ′0​ = 75 kPaOCR = 2.53.5 mwater table

A 3.5 m thick overconsolidated clay layer has Cc = 0.25, Cr = 0.05 and e₀ = 0.65. At its mid-depth the effective vertical stress is 75 kPa and the overconsolidation ratio is OCR = 2.5. A new building adds 150 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 3.5 mCc = 0.25Cr = 0.05e0 = 0.65σ′0 = 75 kPaOCR = 2.5Δσ = 150 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 4 m4 msandwater table

In a laboratory oedometer test, a clay specimen 19 mm thick, drained at the top and bottom, reaches 50% consolidation in 8 min. In the field the same clay forms a layer 4 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 = 8 minH = 4 mfield: double drainage
t = days
17.Hydrostatic forceMedium
gated = 2 mH = 3 m

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

d = 2 mH = 3 mb = 2 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 1 mH = 2.5 m

A vertical rectangular gate 1.5 m wide sits in the wall of a tank of glycerin, with its top edge 1 m below the surface. Find the depth ycp of the centre of pressure below the surface.

d = 1 mH = 2.5 mb = 1.5 mρ = 1260 kg/m³g = 9.81 m/s²
ycp = m
19.Pipe friction & head lossMedium
V = 1.4 m/sD = 75 mmL = 400 mf = 0.015

Water flows at a mean velocity of 1.4 m/s through a pipe 400 m long with an inside diameter of 75 mm. Use the Darcy friction factor f = 0.015 and g = 9.81 m/s². Find the friction head loss hf.

V = 1.4 m/sL = 400 mD = 75 mmf = 0.015g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 5Δz = ?L = 100 m, D = 300 mm, f = 0.0224× bend (K = 0.3)

Two open reservoirs are joined by a pipe 100 m long with an inside diameter of 300 mm and a Darcy friction factor f = 0.022. The minor losses are a square-edged entrance (K = 0.5), 4 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 100 L/s?

Q = 100 L/sL = 100 mD = 300 mmf = 0.022Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 5Kexit = 1.0
Δz = m
21.Open-channel flow (Manning)Medium
b = 3 my = 1.5 mn = 0.03, S = 0.001

A rectangular grass-lined earth channel is 3 m wide. Water flows uniformly 1.5 m deep. Manning n = 0.03 and the bed slope is S = 0.001. Find the flow rate Q in m³/s.

b = 3 my = 1.5 mn = 0.03S = 0.001
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 4.5 my = 2.4 m1 : 1n = 0.014, Q = 43 m³/s

A trapezoidal unfinished concrete channel with a bottom width of 4.5 m and side slopes of 1:1 (horizontal:vertical) must carry 43 m³/s in uniform flow at a depth of 2.4 m. Manning n = 0.014. Find the required bed slope S (in m/m).

Q = 43 m³/sb = 4.5 my = 2.4 mz = 1n = 0.014
S = m/m
23.Pumps & pump powerMedium
PQ = 10 L/sH = 16 m

A pump delivers 10 L/s of water (ρ = 1000 kg/m³) against a head of 16 m. The pump efficiency is 82% and the electric motor driving it has an efficiency of 90%. Use g = 9.81 m/s². Find the electrical power Pel the motor draws, in kW.

Q = 10 L/sH = 16 mηpump = 82%ηmotor = 90%g = 9.81 m/s²
Pel = kW
24.Pumps & pump powerHard
PQ = 75 L/sΔz = 21 mL = 300 m, D = 200 mm, f = 0.015, ΣK = 5

A pump moves 75 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 21 m higher. The pipe is 300 m long with an inside diameter of 200 mm and a Darcy friction factor f = 0.015; the minor-loss coefficients add up to ΣK = 5 (entrance and exit included). Use g = 9.81 m/s². Find the head H the pump must add.

Q = 75 L/sΔz = 21 mL = 300 mD = 200 mmf = 0.015ΣK = 5
H = m
25.Time value of moneyMedium
years0123456PV = ?€50 000

You need €50 000 in 6 years. An account pays 2% per year, compounded quarterly. How much must you deposit today? Find the present value PV.

FV = €50 0002% / 4n = 6
PV = €
26.Time value of moneyHard
months0123…192A?AA€100 000

You want €100 000 in 16 years. You save the same amount at the end of every month in an account paying 5.4% per year, compounded monthly. Find the monthly deposit A.

FV = €100 0005.4% / 12N = 192
A = €
27.NPV & IRRMedium
years0123…9€20 000€2 000€2 000€2 000€2 000r = 10%, EAC = ?

A machine costs €20 000 today, lasts 9 years and costs €2 000 per year to run (paid at the end of each year). The cost of capital is 10%. Find its equivalent annual cost EAC.

C0 = €20 000M = €2 000n = 9r = 10%
EAC = €
28.NPV & IRRHard
years0123−50 00031 00020 50031 000

A project costs €50 000 and returns €31 000, €20 500, €31 000 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −50 000CF1 = 31 000CF2 = 20 500CF3 = 31 000
IRR = %
29.Normal distributionMedium
49.577P = ?

The exam scores are normally distributed with mean 65 points and standard deviation 10 points. What fraction lies between 49.5 and 77 points? Give P as a decimal.

μ = 65σ = 10x1 = 49.5x2 = 77
P =
30.Normal distributionHard
157164171178185192199cmtop 95%

The heights of adult men are normally distributed with mean 178 cm and standard deviation 7 cm. Drag the cut-off so the shaded top 95% is to the right of it. Find the cut-off x.

μ = 178 cmσ = 7 cm95%
x = cm

3Solutions

1.Beam support reactions

Answer: RB = 43.5 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.

P1​ = 15 kNP2​ = 60 kNABRA​RB​1 m6 m3 m

Free-body diagram

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

Equilibrium

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

ΣMA = 0: RB·10 = 15·1 + 60·7
RB = 435/10 = 43.5 kN
ΣFy = 0: RA = 75 − 43.5 = 31.5 kN

Answer

RB = 43.5 kN
2.Beam support reactions

Answer: α = 34.82 °

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.

Components of P

Pv = 55·sin 30° = 27.5 kN
Ph = 55·cos 30° = 47.63 kN

Reactions

ΣMA = 0: RB·8 = 27.5·2 + 50·6 → RB = 44.38 kN
Ay = 27.5 + 50 − 44.38 = 33.13 kN
Ax = Ph = 47.63 kN

Direction at A

α = atan(Ay/Ax) = atan(33.13/47.63) = 34.82°

Answer

α = 34.82°
3.Truss: method of joints

Answer: FBC = −32.05 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.

ABBCACACB40 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·6 = 40·4 → Cy = 26.67 kN
ΣFy = 0: Ay = 40 − 26.67 = 13.33 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 = 3/3.606 = 0.8321, cos γ = 2/3.606 = 0.5547
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −26.67/0.8321 = −32.05 kN

Answer

FBC = −32.05 kN (compression)
4.Truss: method of joints

Answer: FAC = 21.88 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.

ABBCACACB40 kN15 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·8 = 40·1 + 15·4 → Cy = 12.5 kN
ΣFy = 0: Ay = 40 − 12.5 = 27.5 kN
ΣFx = 0: Ax = −15 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 = 4/8.062 = 0.4961, cos γ = 7/8.062 = 0.8682
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −12.5/0.4961 = −25.19 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−25.19)·0.8682 = 21.88 kN

Answer

FAC = 21.88 kN (tension)
5.Shear force & bending moment

Answer: Mx = 9.375 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 = 3·5 = 15 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 3·5·2.5
RB = 37.5/5 = 7.5 kN
ΣFy = 0: RA = 15 − 7.5 = 7.5 kN
w = 3 kN/mABRA​ = 7.5RB​ = 7.5section2.5 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 = 7.5·2.5 − 3·2.5·1.25 = 9.375 kN·m

Answer

Mx = 9.375 kN·m
6.Shear force & bending moment

Answer: Mx = 51.56 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 = 10·4 = 40 kN, acting at x̄ = 2 m
ΣMA = 0: RB·4 = 35·1.5 + 10·4·2
RB = 132.5/4 = 33.13 kN
ΣFy = 0: RA = 75 − 33.13 = 41.88 kN
w = 10 kN/mP = 35 kNABRA​ = 41.88RB​ = 33.13section1.5 m2.5 m

Cut at x = 1.5 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 = 41.88·1.5 − 10·1.5·0.75 = 51.56 kN·m

Answer

Mx = 51.56 kN·m
7.Beam deflection

Answer: δP = 1.014 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 = 26000 N, a = 2000 mm, b = 1000 mm, L = 3000 mm
EI = 1.14 × 10¹³ N·mm²

Deflection under the load

δP = Pa²b²/(3EIL) = 26000·2000²·1000²/(3·1.14 × 10¹³·3000) = 1.014 mm

Answer

δP = 1.014 mm
8.Beam deflection

Answer: Ireq = 1.875 × 10⁶ mm⁴

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).

Deflection limit

δallow = L/360 = 2000/360 = 5.556 mm

Required second moment of area

I = 5wL⁴/(384·E·δallow) = 5·10·2000⁴/(384·200000·5.556) = 1.875 × 10⁶ mm⁴
Ireq = 1.875 × 10⁶ mm⁴

Answer

Ireq = 1.875 × 10⁶ mm⁴
9.Column buckling

Answer: Pcr = 62.01 kN

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

Smallest second moment of area

A round section has the same I about every axis.

I = πd⁴/64 = π·80⁴/64 = 2.011 × 10⁶ mm⁴

Effective length

KL = 2·4000 = 8000 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·2.011 × 10⁶/8000² = 62013 N = 62.01 kN

Answer

Pcr = 62.01 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·40⁴/64 = 125664 mm⁴

Radius of gyration and slenderness

A = 1257 mm²
r = √(I/A) = √(125664/1257) = 10 mm
KL = 1·6000 = 6000 mm
KL/r = 6000/10 = 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 = 13.68 × 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 = 120·30 = 3600 mm², yf = 160 + 30/2 = 175 mm
web: Aw = 10·160 = 1600 mm², yw = 160/2 = 80 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (3600·175 + 1600·80)/5200 = 145.8 mm

Parallel-axis theorem

flange: 120·30³/12 + 3600·(175 − 145.8)² = 3.346 × 10⁶ mm⁴
web: 10·160³/12 + 1600·(80 − 145.8)² = 1.033 × 10⁷ mm⁴
Ix = 3.346 × 10⁶ + 1.033 × 10⁷ = 1.368 × 10⁷ mm⁴ = 13.68 × 10⁶ mm⁴

Answer

Ix = 13.68 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: σtop = 64.76 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 = 180·30 = 5400 mm², yf = 220 + 30/2 = 235 mm
web: Aw = 8·220 = 1760 mm², yw = 220/2 = 110 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (5400·235 + 1760·110)/7160 = 204.3 mm

Parallel-axis theorem

flange: 180·30³/12 + 5400·(235 − 204.3)² = 5.503 × 10⁶ mm⁴
web: 8·220³/12 + 1760·(110 − 204.3)² = 2.274 × 10⁷ mm⁴
Ix = 5.503 × 10⁶ + 2.274 × 10⁷ = 2.824 × 10⁷ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 250 − 204.3 = 45.73 mm
σ = M·y/I = 4 × 10⁷·45.73/2.824 × 10⁷ = 64.76 MPa

Answer

σtop = 64.76 MPa
13.Effective stress in soil

Answer: σ′ = 66.88 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) = 16.5·3 + 18.5·2 = 86.5 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·2 = 19.62 kPa

Effective stress

σ′ = σ − u = 86.5 − 19.62 = 66.88 kPa

Answer

σ′ = 66.88 kPa
14.Effective stress in soil

Answer: σ = 102.5 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·2 + γsat,clay·2.5
σ = 16.5·1 + 20.5·2 + 18·2.5 = 102.5 kPa

Answer

σ = 102.5 kPa
15.Consolidation settlement

Answer: S = 84.2 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.

Preconsolidation pressure

σ′p = OCR·σ′0 = 2.5·75 = 187.5 kPa

Compare with the preconsolidation pressure

σ′f = 75 + 150 = 225 kPa > 187.5 kPa

Settlement

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

S = 0.05·3.5/(1 + 0.65)·log₁₀(187.5/75) + 0.25·3.5/(1 + 0.65)·log₁₀(225/187.5)
S = 42.21 + 41.99 = 84.2 mm

Answer

S = 84.2 mm
16.Consolidation settlement

Answer: t = 246.2 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 = 4/2 = 2 m

Scale the time

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

tfield = 8·(2/0.0095)² = 354571 min
tfield = 354571/1440 = 246.2 days

Answer

t = 246.2 days
17.Hydrostatic force

Answer: F = 206 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 = 3·2 = 6 m²
gated = 2 mH = 3 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3.5·6 = 206 kN

Answer

F = 206 kN
18.Hydrostatic force

Answer: ycp = 2.481 m

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 + 2.5/2 = 2.25 m
A = H·b = 2.5·1.5 = 3.75 m²
gated = 1 mH = 2.5 mF

Resultant force

F = ρ·g·yc·A = 1260·9.81·2.25·3.75 = 104.3 kN

Centre of pressure

Pressure grows with depth, so the resultant acts below the centroid.

Ic = b·H³/12 = 1.5·2.5³/12 = 1.953 m⁴
ycp = yc + Ic/(yc·A) = 2.25 + 1.953/(2.25·3.75) = 2.481 m

Answer

ycp = 2.481 m
19.Pipe friction & head loss

Answer: hf = 7.992 m

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

Velocity head

V²/(2g) = 1.4²/(2·9.81) = 0.0999 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.015·(400/0.075)·1.4²/(2·9.81) = 7.992 m

Answer

hf = 7.992 m
20.Pipe friction & head loss

Answer: Δz = 1.534 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 = 0.022·100/0.3 = 7.333
ΣK = 0.5 + 4·0.3 + 5 + 1.0 = 7.7

Total head loss

hf = 7.333·0.102 = 0.7481 m
hm = 7.7·0.102 = 0.7855 m
Δz = hf + hm = 1.534 m

Answer

Δz = 1.534 m
21.Open-channel flow (Manning)

Answer: Q = 3.916 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 = 3·1.5 = 4.5 m²
P = b + 2y = 3 + 2·1.5 = 6 m
R = A/P = 0.75 m

Velocity

V = (1/0.03)·0.752/3·0.0011/2 = 0.8701 m/s

Flow rate

Q = A·V = 4.5·0.8701 = 3.916 m³/s

Answer

Q = 3.916 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.0007928 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 = (4.5 + 1·2.4)·2.4 = 16.56 m²
P = b + 2y·√(1 + z²) = 4.5 + 2·2.4·√(1 + 1²) = 11.29 m
R = A/P = 1.467 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.014·43/(16.56·1.291) = 0.02816
S = 0.02816² = 0.0007928

Answer

S = 0.0007928

That is a fall of 0.7928 m per kilometre.

23.Pumps & pump power

Answer: Pel = 2.127 kW

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

Hydraulic power

Ph = ρ·g·Q·H = 1000·9.81·0.01·16 = 1.57 kW

Shaft power

Pshaft = 1.57/0.82 = 1.914 kW

Electrical power

Pel = 1.914/0.9 = 2.127 kW

Answer

Pel = 2.127 kW
24.Pumps & pump power

Answer: H = 28.99 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 = 0.075/0.03142 = 2.387 m/s
V²/(2g) = 0.2905 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (22.5 + 5)·0.2905 = 7.988 m

Pump head

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

H = Δz + hL = 21 + 7.988 = 28.99 m

Answer

H = 28.99 m
25.Time value of money

Answer: PV = 44359 €

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

Rate and number of periods

i = 0.02/4 = 0.005
N = 4·6 = 24

Present value

PV = FV/(1 + i)N = 50 000/1.127 = €44 359.28

Answer

PV = €44 359.28
26.Time value of money

Answer: A = 328.9 €

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 deposits

i = 0.054000000000000006/12 = 0.0045
N = 12·16 = 192

Deposit

A = FV·i/((1 + i)N − 1) = 100 000·0.0045/(2.368 − 1) = €328.94

Answer

A = €328.94
27.NPV & IRR

Answer: EAC = 5473 €

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 − 1.1−9)/0.1 = 5.759

Annualised purchase price

20 000/5.759 = 3 472.81

EAC

EAC = 3 472.81 + 2 000 = €5 472.81

Answer

EAC = €5 472.81
28.NPV & IRR

Answer: IRR = 30.12 %

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(30%) = 86.48
NPV(35%) = −3 189.05

Narrow down

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

IRR ≈ 30 + 5·86.48/(86.48 − (−3 189.05)) = 30.13%
exact: NPV(30.12%) = 0 → IRR = 30.12%

Answer

IRR = 30.12%
29.Normal distribution

Answer: P = 0.8244

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 = (49.5 − 65)/10 = −1.55
z₂ = (77 − 65)/10 = 1.2

Area between

P = Φ(1.2) − Φ(−1.55) = 0.8849 − 0.06057 = 0.8244

Answer

P = 0.8244
30.Normal distribution

Answer: x = 166.5 cm

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

Φ(z) = 0.05

z from the table

z ≈ −1.64

Back to the original units

x = 178 − 1.64·7 = 166.5 cm

Answer

x = 166.5 cm

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