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​ = 55 kNP2​ = 55 kNABRA​RB​ = ?1 m1 m2 m

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

L = 4 mP1 = 55 kN at 1 mP2 = 55 kN at 2 m
RB = kN
2.Beam support reactionsHard
w = 8 kN/mP = 75 kNQ = 65 kNADCMA​ = ?2 m2 m2 m2 m

A compound beam is fixed to the wall at A, has an internal hinge at C (4 m from A) and rests on a roller at D (8 m from A). It carries a point load P at 6 m from A, a uniformly distributed load w on the whole part CD and a point load Q at 2 m from A. Find the magnitude of the reaction moment MA at the wall.

AC = 4 mAD = 8 mP = 75 kN at 6 mw = 8 kN/m from 4 to 8 mQ = 65 kN at 2 m
MA = kN·m
3.Truss: method of jointsMedium
ABCDEFGH10 kN40 kN20 kN10 kN4 × 4 m3 m

Exactly one member of this truss carries no force under these loads. Which is the zero-force member? Click it in the diagram.

B: 10 kN ↓D: 40 kN ↓F: 20 kN ↓H: 10 kN ↓
  1. 1member AB
  2. 2member BC
  3. 3member CD
  4. 4member DE
  5. 5member FG
  6. 6member GH
  7. 7member AF
  8. 8member HE
  9. 9member BF
  10. 10member CG
  11. 11member DH
  12. 12member FC
  13. 13member HC
4.Truss: method of jointsHard
ABBCACACB50 kN5 kN8 m3 m3 m

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

span = 8 mheight = 3 mB is 3 m from Avertical load = 50 kNhorizontal load = 5 kN ←
FAB = kN
5.Shear force & bending momentMedium
45 kN30 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.

45 kN @ 2 m30 kN @ 6 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)
6.Shear force & bending momentHard
w = 3 kN/mP = 25 kNABsection4 m4 m

Find the bending moment Mx at the section x = 4 m from support A. Use sagging moments positive and upward shear on the left face positive.

L = 8 mP = 25 kN at 4 mw = 3 kN/m from 0 to 8 mx = 4 m
Mx = kN·m
7.Beam deflectionMedium
w = 10 kN/mδL = 6 m

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

w = 10 kN/mL = 6 mE = 200 GPa (steel)I = 57 × 10⁶ mm⁴
δmax = mm
8.Beam deflectionHard
w = 20 kN/mP = 16 kNδL = 3 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 = 16 kNw = 20 kN/mL = 3 mE = 11 GPa (timber)I = 120 × 10⁶ mm⁴
δmax = mm
9.Column bucklingMedium
PL = 4 m30 × 60 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)b × h = 30 × 60 mm
Pcr = kN
10.Column bucklingHard
P = 115 kNL = 6 md = ?cross-section

A solid round column of length L made of steel is fixed at both ends. It must carry 115 kN with a factor of safety of 3 against buckling. Find the smallest diameter d.

P = 115 kNn = 3L = 6 mE = 200 GPa (steel)
d = mm
11.Centroid & second moment of areaMedium
1402016020xdimensions in mm

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

bf = 140 mmtf = 20 mmtw = 20 mmhw = 160 mm
Ix = × 10⁶ mm⁴
12.Centroid & second moment of areaHard
200280183802010xdimensions in mm

A welded I-section has a top flange 200 × 18 mm, a web 380 mm high and 10 mm thick, and a bottom flange 280 × 20 mm (width × thickness). Find its second moment of area Ix about the horizontal axis x through its centroid.

top flange: 200 × 18 mmweb: 10 × 380 mmbottom flange: 280 × 20 mm
Ix = × 10⁶ mm⁴
13.Effective stress in soilMedium
sandγd​ = 16 kN/m³γsat​ = 19 kN/m³10 mwater tableXz = 7 m

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

z = 7 mzw = 2 mγw = 9.81 kN/m³sand: γd = 16 kN/m³sand: γsat = 19 kN/m³
u = kPa
14.Effective stress in soilHard
sandγd​ = 15.5 kN/m³γsat​ = 19 kN/m³4 mclayγsat​ = 18 kN/m³7 mwater tableXz = 7.5 m

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

z = 7.5 mzw = 1 mγw = 9.81 kN/m³sand: γd = 15.5 kN/m³sand: γsat = 19 kN/m³clay: γsat = 18 kN/m³
σ = kPa
15.Consolidation settlementMedium
Δσ = 160 kPasandclayCc​ = 0.4, Cr​ = 0.04e0​ = 0.6σ′0​ = 55 kPaσ′p​ = 85 kPa2 mwater table

A 2 m thick overconsolidated clay layer has Cc = 0.4, Cr = 0.04 and e₀ = 0.6. At its mid-depth the effective vertical stress is 55 kPa and the preconsolidation pressure is 85 kPa. A new building adds 160 kPa of vertical stress at mid-depth. Find the primary consolidation settlement S in mm.

H = 2 mCc = 0.4Cr = 0.04e0 = 0.6σ′0 = 55 kPaσ′p = 85 kPaΔσ = 160 kPa
S = mm
16.Consolidation settlementHard
sandclayH = 3 mcv​ = 5 m²/year3 msandwater table

A clay layer 3 m thick has a coefficient of consolidation cv = 5 m²/year. It lies between two sand layers, so water drains out at the top and the bottom. For 50% average consolidation the time factor is Tv = 0.197. How many years t does the layer take to reach 50% consolidation?

H = 3 mcv = 5 m²/yearU = 50%Tv = 0.197double drainage
t = years
17.Hydrostatic forceMedium
gated = 2 mH = 2 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of water, with its top edge 2 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 2 mH = 2 mb = 3 mρ = 1000 kg/m³g = 9.81 m/s²
F = kN
18.Hydrostatic forceHard
gated = 1.5 mH = 1.5 m

A vertical rectangular gate 3 m wide sits in the wall of a tank of seawater, with its top edge 1.5 m below the surface. Find the resultant hydrostatic force F on the gate.

d = 1.5 mH = 1.5 mb = 3 mρ = 1025 kg/m³g = 9.81 m/s²
F = kN
19.Pipe friction & head lossMedium
V = 1 m/sD = 300 mmL = 300 mf = 0.02

Water (ρ = 1000 kg/m³) flows at 1 m/s through a horizontal pipe, 300 m long, with an inside diameter of 300 mm. Use the Darcy friction factor f = 0.02 and g = 9.81 m/s². Find the pressure drop Δp over the pipe in kPa.

V = 1 m/sL = 300 mD = 300 mmf = 0.02ρ = 1000 kg/m³
Δp = kPa
20.Pipe friction & head lossHard
K = 10free outletH = ?L = 200 m, D = 200 mm, f = 0.0153× bend (K = 0.3)

A pipe 200 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), 3 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 75 L/s?

Q = 75 L/sL = 200 mD = 200 mmf = 0.015Kentrance = 0.5Kbend = 0.3 (×3)Kvalve = 10
H = m
21.Open-channel flow (Manning)Medium
b = 3 my = 2 m3 : 1n = 0.014, S = 0.005

A trapezoidal unfinished concrete channel has a bottom width of 3 m and side slopes of 3:1 (horizontal:vertical). Water flows uniformly 2 m deep. Manning n = 0.014 and the bed slope is S = 0.005. Find the flow rate Q in m³/s.

b = 3 my = 2 mz = 3n = 0.014S = 0.005
Q = m³/s
22.Open-channel flow (Manning)Hard
b = 4.5 my = 1.2 m2 : 1n = 0.022, Q = 21 m³/s

A trapezoidal clean earth channel with a bottom width of 4.5 m and side slopes of 2:1 (horizontal:vertical) must carry 21 m³/s in uniform flow at a depth of 1.2 m. Manning n = 0.022. Find the required bed slope S (in m/m).

Q = 21 m³/sb = 4.5 my = 1.2 mz = 2n = 0.022
S = m/m
23.Pumps & pump powerMedium
PQ = 15 L/sH = 30 m

In a test, a pump delivers 15 L/s of water (ρ = 1000 kg/m³) against a head of 30 m while its shaft takes 5.2 kW. Use g = 9.81 m/s². Find the pump efficiency η in percent.

Q = 15 L/sH = 30 mPshaft = 5.2 kWg = 9.81 m/s²
η = %
24.Pumps & pump powerHard
PQ = 120 L/sΔz = 13 mL = 300 m, D = 250 mm, f = 0.025, ΣK = 8

A pump moves 120 L/s of water (ρ = 1000 kg/m³) from an open lower reservoir to an upper tank whose water surface is 13 m higher. The pipe is 300 m long with an inside diameter of 250 mm and a Darcy friction factor f = 0.025; the minor-loss coefficients add up to ΣK = 8 (entrance and exit included). Use g = 9.81 m/s². The pump efficiency is 78%. Find the shaft power Pshaft in kW.

Q = 120 L/sΔz = 13 mL = 300 mD = 250 mmf = 0.025ΣK = 8η = 78%
Pshaft = kW
25.Time value of moneyMedium
years0123€20 000FV = ?

You invest €20 000 at a nominal rate of 4% per year, compounded quarterly. Find the value FV of the investment after 3 years.

PV = €20 0004% / 4n = 3
FV = €
26.Time value of moneyHard
months0123…48€20 000AAAA5.4% / 12, I = ?

A loan of €20 000 is repaid with equal monthly payments over 4 years at 5.4% per year, compounded monthly. How much interest I is paid in total over the life of the loan?

P = €20 0005.4% / 12N = 48
I = €
27.NPV & IRRMedium
years01234−45 00016 00014 00018 00010 000

An investment of €45 000 gives these cash flows at the end of years 1 to 4: €16 000, €14 000, €18 000, €10 000. The cost of capital is 10%. Find the net present value NPV.

r = 10%CF0 = −45 000CF1 = 16 000CF2 = 14 000CF3 = 18 000CF4 = 10 000
NPV = €
28.NPV & IRRHard
years0123−50 00030 00036 50027 500

A project costs €50 000 and returns €30 000, €36 500, €27 500 at the end of years 1 to 3. Find its internal rate of return IRR in percent.

CF0 = −50 000CF1 = 30 000CF2 = 36 500CF3 = 27 500
IRR = %
29.Normal distributionMedium
−3−2−10123zshaded area between −z and z = 0.7580

Drag z so that the shaded area between −z and z under the standard normal curve is 0.7580. Find z to two decimals.

A = 0.7580
z =
30.Normal distributionHard
35455565758595pointstop 15%

The exam scores are normally distributed with mean 65 points and standard deviation 10 points. Drag the cut-off so the shaded top 15% is to the right of it. Find the cut-off x.

μ = 65 pointsσ = 10 points15%
x = points

3Solutions

1.Beam support reactions

Answer: RB = 41.25 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​ = 55 kNP2​ = 55 kNABRA​RB​1 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.

ΣMA = 0: RB·4 = 55·1 + 55·2
RB = 165/4 = 41.25 kN
ΣFy = 0: RA = 110 − 41.25 = 68.75 kN

Answer

RB = 41.25 kN
2.Beam support reactions

Answer: MA = 344 kN·m

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. An internal hinge cannot carry a bending moment, which gives one extra equation: the moment about the hinge of the forces on either side is zero.

Part CD

The hinge has no moment, so moments about C on CD alone must balance.

W = 8·4 = 32 kN at 2 m from C
ΣMC = 0: RD·4 = 75·2 + 32·2
RD = 53.5 kN
VC = 107 − 53.5 = 53.5 kN

Part AC

The hinge force VC acts downward on AC (equal and opposite to its action on CD).

RA = 65 + 53.5 = 118.5 kN
MA = 65·2 + 53.5·4 = 344 kN·m

Answer

MA = 344 kN·m
3.Truss: method of joints

Answer: member CG

Zero-force members: at a joint, the forces must balance in every direction. If a joint has no load and no support, and two of its three members are in line, then the balance across that line involves only the third member, so its force is zero. If only two members meet at an unloaded joint and they are not in line, both are zero.

Joint G

FG and GH lie on one straight line and the joint carries no load. Balancing forces across that line leaves only CG.

ΣF⊥ = 0 → FCG = 0

Check with the method of joints

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

AB: 46.67 kN (T), BC: 46.67 kN (T), CD: 60 kN (T), DE: 60 kN (T), FG: 53.33 kN (C), GH: 53.33 kN (C), AF: 58.33 kN (C), HE: 75 kN (C), BF: 10 kN (T), CG: 0, DH: 40 kN (T), FC: 8.333 kN (T), HC: 8.333 kN (C)

Answer

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

Answer: FAB = −46.85 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.

ABBCACACB50 kN5 kNAy​Cy​Ax​

Support reactions

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

ΣMA = 0: Cy·8 = 50·3 − 5·3 → Cy = 16.88 kN
ΣFy = 0: Ay = 50 − 16.88 = 33.13 kN
ΣFx = 0: Ax = 5 kN

Joint A

Assume every member is in tension (pulling away from the joint). Only AB has a vertical component at A.

sin α = 3/4.243 = 0.7071
ΣFy = 0: Ay + FAB·sin α = 0
FAB = −33.13/0.7071 = −46.85 kN

Answer

FAB = −46.85 kN (compression)
5.Shear force & bending moment

Answer: D (x = 6 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 = 52.5 kN, R2 = 22.5 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 = 105, MC = 120, MD = 135 kN·m, ME = 90, MF = 45, MG = 0

Answer

Mark D: MD = 135 kN·m
6.Shear force & bending moment

Answer: Mx = 74 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 = 3·8 = 24 kN, acting at x̄ = 4 m
ΣMA = 0: RB·8 = 25·4 + 3·8·4
RB = 196/8 = 24.5 kN
ΣFy = 0: RA = 49 − 24.5 = 24.5 kN
w = 3 kN/mP = 25 kNABRA​ = 24.5RB​ = 24.5section4 m4 m

Cut at x = 4 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 = 24.5·4 − 3·4·2 = 74 kN·m

Answer

Mx = 74 kN·m
7.Beam deflection

Answer: δmax = 14.8 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 = 10 N/mm, L = 6000 mm
EI = 1.14 × 10¹³ N·mm²

Deflection

δmax = 5wL⁴/(384EI) = 5·10·6000⁴/(384·1.14 × 10¹³) = 14.8 mm

Answer

δmax = 14.8 mm
8.Beam deflection

Answer: δmax = 22.8 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 = 16000 N, w = 20 N/mm, L = 3000 mm, EI = 1.32 × 10¹² N·mm²

Each load on its own

δP = PL³/(48EI) = 16000·3000³/(48·1.32 × 10¹²) = 6.818 mm
δw = 5wL⁴/(384EI) = 5·20·3000⁴/(384·1.32 × 10¹²) = 15.98 mm

Add them

δmax = 6.818 + 15.98 = 22.8 mm

Answer

δmax = 22.8 mm
9.Column buckling

Answer: Pcr = 33.99 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 = 60·30³/12 = 135000 mm⁴

Effective length

KL = 0.7·4000 = 2800 mm

Critical load

Pcr = π²EI/(KL)² = π²·200000·135000/2800² = 33990 N = 33.99 kN

Answer

Pcr = 33.99 kN
10.Column buckling

Answer: d = 75.24 mm

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.

Required critical load

Pcr = n·P = 3·115000 = 345000 N
KL = 0.5·6000 = 3000 mm

Solve for the diameter

d = (64·n·P·(KL)²/(π³E))^(1/4) = (64·345000·3000²/(π³·200000))^(1/4) = 75.24 mm

Answer

d = 75.24 mm

Check: the slenderness KL/r is 159.5, so the column is slender and Euler applies.

11.Centroid & second moment of area

Answer: Ix = 19.02 × 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 = 140·20 = 2800 mm², yf = 160 + 20/2 = 170 mm
web: Aw = 20·160 = 3200 mm², yw = 160/2 = 80 mm

Centroid

ȳ = (Afyf + Awyw)/(Af + Aw) = (2800·170 + 3200·80)/6000 = 122 mm

Parallel-axis theorem

flange: 140·20³/12 + 2800·(170 − 122)² = 6.545 × 10⁶ mm⁴
web: 20·160³/12 + 3200·(80 − 122)² = 1.247 × 10⁷ mm⁴
Ix = 6.545 × 10⁶ + 1.247 × 10⁷ = 1.902 × 10⁷ mm⁴ = 19.02 × 10⁶ mm⁴

Answer

Ix = 19.02 × 10⁶ mm⁴
12.Centroid & second moment of area

Answer: Ix = 400 × 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 three rectangles

Measure every y from the bottom edge.

top flange: A = 3600 mm², y = 409 mm
web: A = 3800 mm², y = 210 mm
bottom flange: A = 5600 mm², y = 10 mm

Centroid

ȳ = (3600·409 + 3800·210 + 5600·10)/13000 = 179 mm

Parallel-axis theorem

top flange: 200·18³/12 + 3600·230² = 1.906 × 10⁸ mm⁴
web: 10·380³/12 + 3800·31.05² = 4.939 × 10⁷ mm⁴
bottom flange: 280·20³/12 + 5600·169² = 1.6 × 10⁸ mm⁴
Ix = 1.906 × 10⁸ + 4.939 × 10⁷ + 1.6 × 10⁸
Ix = 4 × 10⁸ mm⁴ = 400 × 10⁶ mm⁴

Answer

Ix = 400 × 10⁶ mm⁴
13.Effective stress in soil

Answer: u = 49.05 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) = 9.81·5 = 49.05 kPa

Answer

u = 49.05 kPa
14.Effective stress in soil

Answer: σ = 135.5 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·3 + γsat,clay·3.5
σ = 15.5·1 + 19·3 + 18·3.5 = 135.5 kPa

Answer

σ = 135.5 kPa
15.Consolidation settlement

Answer: S = 211 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 = 55 + 160 = 215 kPa > 85 kPa

Settlement

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

S = 0.04·2/(1 + 0.6)·log₁₀(85/55) + 0.4·2/(1 + 0.6)·log₁₀(215/85)
S = 9.453 + 201.5 = 211 mm

Answer

S = 211 mm
16.Consolidation settlement

Answer: t = 0.08865 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/2 = 3/2 = 1.5 m

Time

t = Tv·Hdr²/cv = 0.197·1.5²/5 = 0.08865 years

Answer

t = 0.08865 years
17.Hydrostatic force

Answer: F = 176.6 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 + 2/2 = 3 m
A = H·b = 2·3 = 6 m²
gated = 2 mH = 2 mF

Resultant force

F = ρ·g·yc·A = 1000·9.81·3·6 = 176.6 kN

Answer

F = 176.6 kN
18.Hydrostatic force

Answer: F = 101.8 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 + 1.5/2 = 2.25 m
A = H·b = 1.5·3 = 4.5 m²
gated = 1.5 mH = 1.5 mF

Resultant force

F = ρ·g·yc·A = 1025·9.81·2.25·4.5 = 101.8 kN

Answer

F = 101.8 kN
19.Pipe friction & head loss

Answer: Δp = 10 kPa

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

Head loss

hf = f·(L/D)·V²/(2g) = 0.02·(300/0.3)·1²/(2·9.81) = 1.019 m

Pressure drop

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

Δp = ρ·g·hf = 1000·9.81·1.019 = 10000 Pa = 10 kPa

Answer

Δp = 10 kPa
20.Pipe friction & head loss

Answer: H = 7.959 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 = 0.075/0.03142 = 2.387 m/s
V²/(2g) = 0.2905 m

Loss coefficients

f·L/D = 0.015·200/0.2 = 15
ΣK = 0.5 + 3·0.3 + 10 = 11.4

Energy equation

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

H = (1 + 15 + 11.4)·0.2905 = 7.959 m

Answer

H = 7.959 m
21.Open-channel flow (Manning)

Answer: Q = 99.8 m³/s

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

Geometry

A = (b + z·y)·y = (3 + 3·2)·2 = 18 m²
P = b + 2y·√(1 + z²) = 3 + 2·2·√(1 + 3²) = 15.65 m
R = A/P = 1.15 m

Velocity

V = (1/0.014)·1.152/3·0.0051/2 = 5.545 m/s

Flow rate

Q = A·V = 18·5.545 = 99.8 m³/s

Answer

Q = 99.8 m³/s
22.Open-channel flow (Manning)

Answer: S = 0.003933 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 + 2·1.2)·1.2 = 8.28 m²
P = b + 2y·√(1 + z²) = 4.5 + 2·1.2·√(1 + 2²) = 9.867 m
R = A/P = 0.8392 m

Solve Manning for S

S1/2 = n·Q/(A·R2/3) = 0.022·21/(8.28·0.8897) = 0.06271
S = 0.06271² = 0.003933

Answer

S = 0.003933

That is a fall of 3.933 m per kilometre.

23.Pumps & pump power

Answer: η = 84.89 %

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 = 1000·9.81·0.015·30 = 4.415 kW

Efficiency

η = Ph/Pshaft = 4.415/5.2 = 84.89%

Answer

η = 84.89%
24.Pumps & pump power

Answer: Pshaft = 37.09 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 = 0.12/0.04909 = 2.445 m/s
V²/(2g) = 0.3046 m

Head losses

hL = (f·L/D + ΣK)·V²/(2g) = (30 + 8)·0.3046 = 11.57 m

Pump head

H = Δz + hL = 13 + 11.57 = 24.57 m

Shaft power

Pshaft = ρ·g·Q·H/η = 1000·9.81·0.12·24.57/0.78 = 37.09 kW

Answer

Pshaft = 37.09 kW
25.Time value of money

Answer: FV = 22537 €

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

Rate and number of periods

i = r/m = 0.04/4 = 0.01
N = m·n = 4·3 = 12

Future value

FV = 20 000·(1 + 0.01)12 = 20 000·1.127 = €22 536.50

Answer

FV = €22 536.50
26.Time value of money

Answer: I = 2282 €

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

Monthly payment

i = 0.0045, N = 48
A = 20 000·0.0045/(1 − (1 + 0.0045)−48) = €464.22

Total interest

I = N·A − P = 48·464.2 − 20 000 = €2 282.49

Answer

I = €2 282.49
27.NPV & IRR

Answer: NPV = 1470 €

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.

Present value of each cash flow

CF0 = −45 000
CF1/(1 + 0.1)1 = 16 000/1.1 = 14 545.45
CF2/(1 + 0.1)2 = 14 000/1.21 = 11 570.25
CF3/(1 + 0.1)3 = 18 000/1.331 = 13 523.67
CF4/(1 + 0.1)4 = 10 000/1.464 = 6 830.13

Add them up

NPV = €1 469.50

Answer

NPV = €1 469.50

NPV is positive, so the project earns more than the required return.

28.NPV & IRR

Answer: IRR = 40.12 %

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(40%) = 72.89
NPV(45%) = −2 929.60

Narrow down

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

IRR ≈ 40 + 5·72.89/(72.89 − (−2 929.60)) = 40.12%
exact: NPV(40.12%) = 0 → IRR = 40.12%

Answer

IRR = 40.12%
29.Normal distribution

Answer: z = 1.17

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 + 0.7580)/2 = 0.8790

Read the z-table backwards

Find 0.8790 inside the table and read off z.

z = 1.17

Answer

z = 1.17
30.Normal distribution

Answer: x = 75.4 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) = 0.85

z from the table

z ≈ 1.04

Back to the original units

x = 65 + 1.04·10 = 75.4 points

Answer

x = 75.4 points

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