FE Civil exam practice: cram pack

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

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1Formulas and methods

Beam support reactions

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

Method

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

Truss: method of joints

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

Method

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

Shear force & bending moment

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

Method

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

Beam deflection

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

Column buckling

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

Centroid & second moment of area

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

Effective stress in soil

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

Consolidation settlement

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

Hydrostatic force

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

Pipe friction & head loss

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

Open-channel flow (Manning)

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

Pumps & pump power

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

Time value of money

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

Method

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

NPV & IRR

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

Method

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

Normal distribution

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

Method

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

2Practice problems

1.Beam support reactionsMedium
P1​ = 30 kNP2​ = 40 kNABRA​ = ?RB​1.5 m2 m2.5 m

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

L = 6 mP1 = 30 kN at 1.5 mP2 = 40 kN at 3.5 m
RA = kN
2.Beam support reactionsHard
w = 10 kN/mP = 35 kNABRA​ = ?RB​7 m1 m2 m

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

L = 10 mP = 35 kN at 7 mw = 10 kN/m from 8 to 10 m
RA = kN
3.Truss: method of jointsMedium
ABBCACACB55 kN6 m5 m3 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 = 3 mB is 5 m from Avertical load = 55 kN
FAC = kN
4.Truss: method of jointsHard
ABBCACACB10 kN30 kN4 m1 m2 m

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

span = 4 mheight = 2 mB is 1 m from Avertical load = 10 kNhorizontal load = 30 kN →
FAC = kN
5.Shear force & bending momentMedium
w = 12 kN/mABsection3.5 m1.5 m

Find the bending moment Mx at the section x = 3.5 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 5 mw = 12 kN/m from 0 to 5 mx = 3.5 m
Mx = kN·m
6.Shear force & bending momentHard
12 kN/m35 kN60 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 m60 kN @ 4 m12 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
w = 5 kN/mδL = 2 m

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

w = 5 kN/mL = 2 mE = 11 GPa (timber)I = 23 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 4 kN/mABδ4.5 m

A simply supported timber beam of rectangular section, 150 mm wide, carries a uniformly distributed load w over its whole span. Its midspan deflection may not exceed span/360. Find the smallest depth hreq of the section.

w = 4 kN/mL = 4.5 mE = 11 GPa (timber)b = 150 mm
hreq = mm
9.Column bucklingMedium
PL = 4 md = 80 mmcross-section

A column of length L made of steel is fixed at the base and pinned 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 = 2 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 = 2 mE = 200 GPa (steel)d = 25 mm
σcr = MPa
11.Centroid & second moment of areaMedium
190500108xdimensions in mm

A symmetric I-section has flanges 190 mm wide and 10 mm thick, an overall depth of 500 mm and a web 8 mm thick. Find its elastic section modulus Sx for bending about the horizontal centroidal axis x.

B = 190 mmH = 500 mmtf = 10 mmtw = 8 mm
Sx = × 10³ mm³
12.Centroid & second moment of areaHard
1402514012xM = 30 kN·mdimensions in mm

The T-section is used as a beam with the flange on top and carries a sagging bending moment of 30 kN·m. Find the size of the bending stress σtop at the top edge.

bf = 140 mmtf = 25 mmtw = 12 mmhw = 140 mmM = 30 kN·m
σtop = MPa
13.Effective stress in soilMedium
sandγd​ = 16 kN/m³γsat​ = 19 kN/m³8 mwater tableXz = 8 m

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

z = 8 mzw = 4 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 19 kN/m³
u = kPa
14.Effective stress in soilHard
sandγd​ = 17 kN/m³γsat​ = 20 kN/m³6 mclayγsat​ = 17.5 kN/m³6 mwater tableXz = 9 m

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

z = 9 mzw = 2 mγw = 9.81 kN/m³sand: γd = 17 kN/m³sand: γsat = 20 kN/m³clay: γsat = 17.5 kN/m³
σ′ = kPa
15.Consolidation settlementMedium
Δσ = 20 kPasandclayCc​ = 0.3, Cr​ = 0.02e0​ = 0.95σ′0​ = 120 kPaσ′p​ = 180 kPa6 mwater table

A 6 m thick overconsolidated clay layer has Cc = 0.3, Cr = 0.02 and e₀ = 0.95. At its mid-depth the effective vertical stress is 120 kPa and the preconsolidation pressure is 180 kPa. A new building adds 20 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 6 mCc = 0.3Cr = 0.02e0 = 0.95σ′0 = 120 kPaσ′p = 180 kPaΔσ = 20 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 6 m6 mimpervious rockwater table

In a laboratory oedometer test, a clay specimen 20 mm thick, drained at the top and bottom, reaches 50% consolidation in 8 min. In the field the same clay forms a layer 6 m thick. It lies on impervious rock, with sand above it, so water drains out only at the top. How many days t does the field layer take to reach 50% consolidation?

hlab = 20 mmtlab = 8 minH = 6 mfield: single drainage
t = days
17.Hydrostatic forceMedium
gated = 1.5 mH = 1 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of water, with its top edge 1.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 1.5 mH = 1 mb = 2 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 4 mH = 1 m

A vertical rectangular gate 2 m wide sits in the wall of a tank of oil, with its top edge 4 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 4 mH = 1 mb = 2 mρ = 880 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
Q = 3 L/sD = 50 mmL = 500 mf = 0.02

Water flows at 3 L/s through a pipe 500 m long with an inside diameter of 50 mm. Use the Darcy friction factor f = 0.02 and g = 9.81 m/s². Find the friction head loss hf.

Q = 3 L/sL = 500 mD = 50 mmf = 0.02g = 9.81 m/s²
hf = m
20.Pipe friction & head lossHard
K = 10free outletH = ?L = 400 m, D = 200 mm, f = 0.0154× bend (K = 0.3)

A pipe 400 m long with an inside diameter of 200 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), 4 bends (K = 0.3 each) and a valve (K = 10). Use g = 9.81 m/s². How far H must the reservoir surface be above the pipe outlet for a flow rate of 50 L/s?

Q = 50 L/sL = 400 mD = 200 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×4)Kvalve = 10
H = m
21.Open-channel flow (Manning)Medium
D = 300 mmn = 0.013, S = 0.0015

A concrete storm sewer with an inside diameter of 300 mm flows half full. Manning n = 0.013 and the slope is S = 0.0015. Find the flow rate Q in m³/s.

D = 300 mmn = 0.013S = 0.0015
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 2.5 my = 2.2 m2 : 1n = 0.03, Q = 13 m³/s

A trapezoidal grass-lined earth channel with a bottom width of 2.5 m and side slopes of 2:1 (horizontal:vertical) must carry 13 m³/s in uniform flow at a depth of 2.2 m. Manning n = 0.03. Find the required bed slope S (in m/m).

Q = 13 m³/sb = 2.5 my = 2.2 mz = 2n = 0.03
S = m/m
23.Pumps & pump powerMedium
PQ = 30 L/sH = 74 m

A pump with an efficiency of 85% delivers 30 L/s of water (ρ = 1000 kg/m³) against a head of 74 m. Use g = 9.81 m/s². Find the shaft power Pshaft needed, in kW.

Q = 30 L/sH = 74 mη = 85%g = 9.81 m/s²
Pshaft = kW
24.Pumps & pump powerHard
250 kPa (gauge)PQ = 40 L/sΔz = 12 mL = 500 m, D = 150 mm, f = 0.015, ΣK = 8

A pump moves 40 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 12 m higher. The pipe is 500 m long with an inside diameter of 150 mm and a Darcy friction factor f = 0.015; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². The upper tank is closed and the air above its water is at a gauge pressure of 250 kPa. Find the head H the pump must add.

Q = 40 L/sΔz = 12 mL = 500 mD = 150 mmf = 0.015ΣK = 8ptank = 250 kPa
H = m
25.Time value of moneyMedium
years012€5 000FV = ?

You invest €5 000 at 8% per year with continuous compounding. Find the value FV after 2 years.

PV = €5 000r = 8%t = 2
FV = €
26.Time value of moneyHard
months0123…204€500€500€500FV = ?

You save €500 at the end of every month for 17 years. The account pays 4.2% per year, compounded monthly. How much have you saved at the end? Find FV.

A = €5004.2% / 12N = 204
FV = €
27.NPV & IRRMedium
years0123…9−500 00036 000+2%+2%…r = 11%, NPV = ?

A project costs €500 000 today. It generates €36 000 at the end of the first year, and the cash flow then grows by 2% per year forever. The cost of capital is 11%. Find the net present value NPV.

C0 = €500 000CF1 = €36 000g = 2%r = 11%
NPV = €
28.NPV & IRRHard
years012−10 0007 0005 500

A project costs €10 000 and returns €7 000, €5 500 at the end of years 1 to 2. Find its internal rate of return IRR in percent.

CF0 = −10 000CF1 = 7 000CF2 = 5 500
IRR = %
29.Normal distributionMedium
−3−2−10123zshaded area to the right of z = 0.9032

Drag z so that the shaded area under the standard normal curve, to the right of z, is 0.9032. Find z to two decimals.

A = 0.9032
z =
30.Normal distributionHard
35455565758595pointsbottom 90%

The exam scores are normally distributed with mean 65 points and standard deviation 10 points. Drag the cut-off so the shaded bottom 90% is to the left of it. Find the cut-off x.

μ = 65 pointsσ = 10 points90%
x = points

3Solutions

1.Beam support reactions

Answer: RA = 39.17 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​ = 30 kNP2​ = 40 kNABRA​RB​1.5 m2 m2.5 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·6 = 30·1.5 + 40·3.5
RB = 185/6 = 30.83 kN
ΣFy = 0: RA = 70 − 30.83 = 39.17 kN

Answer

RA = 39.17 kN
2.Beam support reactions

Answer: RA = 12.5 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 = 10 kN/mP = 35 kNABRA​RB​7 m1 m2 m

Free-body diagram

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

Equilibrium

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

UDL resultant: W = w·ℓ = 10·2 = 20 kN, acting at x̄ = 9 m
ΣMA = 0: RB·10 = 35·7 + 10·2·9
RB = 425/10 = 42.5 kN
ΣFy = 0: RA = 55 − 42.5 = 12.5 kN

Answer

RA = 12.5 kN
3.Truss: method of joints

Answer: FAC = 15.28 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.

ABBCACACB55 kNAy​Cy​

Support reactions

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

ΣMA = 0: Cy·6 = 55·5 → Cy = 45.83 kN
ΣFy = 0: Ay = 55 − 45.83 = 9.167 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 = 3/3.162 = 0.9487, cos γ = 1/3.162 = 0.3162
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −45.83/0.9487 = −48.31 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−48.31)·0.3162 = 15.28 kN

Answer

FAC = 15.28 kN (tension)
4.Truss: method of joints

Answer: FAC = 26.25 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.

ABBCACACB10 kN30 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·4 = 10·1 + 30·2 → Cy = 17.5 kN
ΣFy = 0: Ay = 10 − 17.5 = −7.5 kN
ΣFx = 0: Ax = −30 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 = 2/3.606 = 0.5547, cos γ = 3/3.606 = 0.8321
ΣFy = 0: Cy + FBC·sin γ = 0 → FBC = −17.5/0.5547 = −31.55 kN
ΣFx = 0: −FAC − FBC·cos γ = 0 → FAC = −(−31.55)·0.8321 = 26.25 kN

Answer

FAC = 26.25 kN (tension)
5.Shear force & bending moment

Answer: Mx = 31.5 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 = 12·5 = 60 kN, acting at x̄ = 2.5 m
ΣMA = 0: RB·5 = 12·5·2.5
RB = 150/5 = 30 kN
ΣFy = 0: RA = 60 − 30 = 30 kN
w = 12 kN/mABRA​ = 30RB​ = 30section3.5 m1.5 m

Cut at x = 3.5 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 = 30·3.5 − 12·3.5·1.75 = 31.5 kN·m

Answer

Mx = 31.5 kN·m
6.Shear force & bending moment

Answer: C (x = 4 m)

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

Support reactions

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

R1 = 89 kN, R2 = 126 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 = 154, MC = 260 kN·m, MD = 198, ME = 88, MF = −70, MG = 0

Answer

Mark C: MC = 260 kN·m
7.Beam deflection

Answer: δmax = 4.117 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 = 2.53 × 10¹¹ N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·5·2000⁴/(384·2.53 × 10¹¹) = 4.117 mm

Answer

δmax = 4.117 mm
8.Beam deflection

Answer: hreq = 231.6 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 = 4 N/mm, L = 4500 mm, E = 11000 N/mm²

Deflection limit

δallow = L/360 = 4500/360 = 12.5 mm

Required second moment of area

Ireq = 5wL⁴/(384·E·δallow) = 5·4·4500⁴/(384·11000·12.5) = 1.553 × 10⁸ mm⁴

Required depth

bh³/12 = Ireq → h = (12·1.553 × 10⁸/150)1/3 = 231.6 mm

Answer

hreq = 231.6 mm

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

9.Column buckling

Answer: Pcr = 506.2 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 = 0.7·4000 = 2800 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·2.011 × 10⁶/2800² = 506225 N = 506.2 kN

Answer

Pcr = 506.2 kN
10.Column buckling

Answer: σcr = 39.34 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 = 0.7·2000 = 1400 mm
KL/r = 1400/6.25 = 224

Critical stress

σcr = π²E/(KL/r)² = π²·200000/224² = 39.34 MPa

Answer

σcr = 39.34 MPa
11.Centroid & second moment of area

Answer: Sx = 1207 × 10³ mm³

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

Outer rectangle minus the two side cut-outs

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

hw = 500 − 2·10 = 480 mm
Ix = (B·H³ − (B − tw)·hw³)/12 = (190·500³ − 182·480³)/12
Ix = 3.019 × 10⁸ mm⁴

Section modulus

c = H/2 = 250 mm
Sx = I/c = 3.019 × 10⁸/250
Sx = 1.207 × 10⁶ mm³ = 1207 × 10³ mm³

Answer

Sx = 1207 × 10³ mm³
12.Centroid & second moment of area

Answer: σtop = 110.6 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 = 140·25 = 3500 mm², yf = 140 + 25/2 = 152.5 mm
web: Aw = 12·140 = 1680 mm², yw = 140/2 = 70 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (3500·152.5 + 1680·70)/5180 = 125.7 mm

Parallel-axis theorem

flange: 140·25³/12 + 3500·(152.5 − 125.7)² = 2.688 × 10⁶ mm⁴
web: 12·140³/12 + 1680·(70 − 125.7)² = 7.964 × 10⁶ mm⁴
Ix = 2.688 × 10⁶ + 7.964 × 10⁶ = 1.065 × 10⁷ mm⁴

Bending stress

The top edge is h − ȳ from the axis.

y = 165 − 125.7 = 39.26 mm
σ = M·y/I = 3 × 10⁷·39.26/1.065 × 10⁷ = 110.6 MPa

Answer

σtop = 110.6 MPa
13.Effective stress in soil

Answer: u = 39.24 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) = 9.81·4 = 39.24 kPa

Answer

u = 39.24 kPa
14.Effective stress in soil

Answer: σ′ = 97.83 kPa

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

Total stress

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

σ = γd·2 + γsat,sand·4 + γsat,clay·3
σ = 17·2 + 20·4 + 17.5·3 = 166.5 kPa

Pore water pressure

Water pressure grows with depth below the water table.

u = γw·(z − zw) = 9.81·7 = 68.67 kPa

Effective stress

σ′ = σ − u = 166.5 − 68.67 = 97.83 kPa

Answer

σ′ = 97.83 kPa
15.Consolidation settlement

Answer: S = 4.12 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 = 120 + 20 = 140 kPa ≤ 180 kPa

Settlement

The clay stays on its recompression line.

S = Cr·H/(1 + e0)·log₁₀(σ′f/σ′0) = 0.02·6/(1 + 0.95)·log₁₀(140/120) = 4.12 mm

Answer

S = 4.12 mm
16.Consolidation settlement

Answer: t = 2000 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 = 20/2 = 10 mm = 0.01 m
Hdr,field = 6 m

Scale the time

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

tfield = 8·(6/0.01)² = 2.88 × 10⁶ min
tfield = 2.88 × 10⁶/1440 = 2000 days

Answer

t = 2000 days
17.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 = 1.5 + 1/2 = 2 m
A = H·b = 1·2 = 2 m²
gated = 1.5 mH = 1 mF

Resultant force

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

Answer

F = 39.24 kN
18.Hydrostatic force

Answer: F = 77.7 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 = 4 + 1/2 = 4.5 m
A = H·b = 1·2 = 2 m²
gated = 4 mH = 1 mF

Resultant force

F = ρ·g·yc·A = 880·9.81·4.5·2 = 77.7 kN

Answer

F = 77.7 kN
19.Pipe friction & head loss

Answer: hf = 23.8 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·0.05²/4 = 0.001963 m²
V = Q/A = 0.003/0.001963 = 1.528 m/s

Velocity head

V²/(2g) = 1.528²/(2·9.81) = 0.119 m

Darcy–Weisbach

hf = f·(L/D)·V²/(2g) = 0.02·(500/0.05)·1.528²/(2·9.81) = 23.8 m

Answer

hf = 23.8 m
20.Pipe friction & head loss

Answer: H = 5.513 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 = 0.05/0.03142 = 1.592 m/s
V²/(2g) = 0.1291 m

Loss coefficients

f·L/D = 0.015·400/0.2 = 30
ΣK = 0.5 + 4·0.3 + 10 = 11.7

Energy equation

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

H = (1 + 30 + 11.7)·0.1291 = 5.513 m

Answer

H = 5.513 m
21.Open-channel flow (Manning)

Answer: Q = 0.01873 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 = 0.03534 m², R = D/4 = 0.075 m

Velocity

V = (1/0.013)·0.0752/3·0.00151/2 = 0.5298 m/s

Flow rate

Q = A·V = 0.03534·0.5298 = 0.01873 m³/s

Answer

Q = 0.01873 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.0005007 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 = (2.5 + 2·2.2)·2.2 = 15.18 m²
P = b + 2y·√(1 + z²) = 2.5 + 2·2.2·√(1 + 2²) = 12.34 m
R = A/P = 1.23 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.03·13/(15.18·1.148) = 0.02238
S = 0.02238² = 0.0005007

Answer

S = 0.0005007

That is a fall of 0.5007 m per kilometre.

23.Pumps & pump power

Answer: Pshaft = 25.62 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 = 1000·9.81·0.03·74 = 21.78 kW

Shaft power

Pshaft = Ph/η = 21.78/0.85 = 25.62 kW

Answer

Pshaft = 25.62 kW
24.Pumps & pump power

Answer: H = 52.63 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 = 0.04/0.01767 = 2.264 m/s
V²/(2g) = 0.2611 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (50 + 8)·0.2611 = 15.15 m

Pressure head

p/(ρ·g) = 250000/(1000·9.81) = 25.48 m

Pump head

Both surfaces are practically at rest, so there is no velocity head term.

H = Δz + p/(ρ·g) + hL = 12 + 25.48 + 15.15 = 52.63 m

Answer

H = 52.63 m
25.Time value of money

Answer: FV = 5868 €

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 = 0.08·2 = 0.16
e0.16 = 1.174

Future value

FV = 5 000·1.174 = €5 867.55

Answer

FV = €5 867.55
26.Time value of money

Answer: FV = 148514 €

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 = 0.042/12 = 0.0035
N = 12·17 = 204

Future value of the deposits

FV = A·((1 + i)N − 1)/i = 500·(2.04 − 1)/0.0035 = €148 514.20

Answer

FV = €148 514.20

You paid in €102 000 yourself; the rest is interest.

27.NPV & IRR

Answer: NPV = −100000 €

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.

Value of the cash flows

PV = 36 000/(0.11 − 0.02) = 400 000.00

NPV

NPV = 400 000.00 − 500 000 = −€100 000.00

Answer

NPV = −€100 000.00

NPV is negative, so the project earns less than the required return.

28.NPV & IRR

Answer: IRR = 17.01 %

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(15%) = 245.75
NPV(20%) = −347.22

Narrow down

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

IRR ≈ 15 + 5·245.75/(245.75 − (−347.22)) = 17.07%
exact: NPV(17.01%) = 0 → IRR = 17.01%

Answer

IRR = 17.01%
29.Normal distribution

Answer: z = −1.3

From an area back to z: Φ(z) is the area to the left of z. For a left-tail area A, find z with Φ(z) = A in the table. A right-tail area A means Φ(z) = 1 − A. A central area A between −z and z leaves (1 − A)/2 in each tail, so Φ(z) = (1 + A)/2. For a value x, use x = μ + zσ.

Area to the left of z

Φ(z) = 1 − 0.9032 = 0.0968

Read the z-table backwards

Find 0.0968 inside the table and read off z.

z = −1.30

Answer

z = −1.30
30.Normal distribution

Answer: x = 77.8 points

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) = 0.9

z from the table

z ≈ 1.28

Back to the original units

x = 65 + 1.28·10 = 77.8 points

Answer

x = 77.8 points

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